# SDR

REMARKS:
3 RED CABIN EMERGENCY FLOOR TRACK LIGHTS INOP.  RELAMPED FLOOR LIGHTS PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND 2 RED EMERGENCY FLOOR TRACK LIGHTS INOP.  RELAMPED BOTH LIGHTS PER BOEING M/M.


REMARKS:
DURING SCHEDULED B1 CHECK, FOUND AFT CABIN RED EMERGENCY FLOOR TRACK LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, WL 208, RBL 8.  REPAIRED PER SWA RA 1-353-421.


REMARKS:
DURING SCHEDULED D CHECK, FOUND L ANGLE CRACKED AT BS 380-400, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL TO FRAME L ANGLE CRACKED AT BS 380, STRINGER 26L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND WEB CRACKED AT BS 530,  BETWEEN STRINGER 23 AND 24 RIGHT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM TENSION STRAP CRACKED AT BS 328, RBL 30 WL 200.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, ACCOMPLISHED BS 277 FRAME REPAIR AND REINFORCEMENT PER SWA ACO 3263-53.


REMARKS:
FLIGHT 567, ON CLIMB-OUT, CREW EXPERIENCED SMOKE AND FUMES IN COCKPIT.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFULLANDING.  REPLACED GASPER FAN AND PERFORMED PRESSURIZED RUN UP PER BOEING MM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL TO FRAME L-ANGLE CRACKED AT BS 380, STR 26R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION FROM BS 1008 TO 1010, LBL 8, 8.5, AND AT LBL 6, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND FORWARD EMERGENCY EXIT LIGHT INOP.  RELAMPED LIGHT PER BOEING MAINTENANCE MANUAL.


REMARKS:
FOUND ONE RED ESCAPE PATH LIGHT INOP AND ONE LIGHT MISSING AT OVERWING EXIT.  RELAMPED LIGHTS PER BOEING MAINTENANCE  MANUAL.


REMARKS:
FOUND SECTION OF ESCAPE PATH LIGHTING WIRE OUT OF TRACK AT RIGHT AFT CABIN AREA.  RESECURED TRACK LIGHTING.


REMARKS:
DURING SCHEDULED A-CHECK, FOUND FORWARD CABIN EMERGENCY FLASHLIGHT INOP.  REPLACED FLASHLIGHT.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOP.  REPLACED BATERY PACK PER BOEING MM.


REMARKS:
FOUND FORWARD ENTRY DOOR ESCAPE SLIDE PRESSURE LOW.  REPLACED SLIDE ASSEMBLY PER BOEING MM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER 27R CORRODED AT BS 369.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 8 TO RBL 8, WL 208.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 55 TO RBL 55, WL 208.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LOWER SURFACE OF CENTER SECTION LOWER SKIN.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL TO FRAME L ANGLE CRACKED AT BS 727A, STRINGER 25L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, EXTERIOR EMERGENCY LIGHT AFT OF FORWARD GALLEY DOOR INOP.  REPLACED LIGHT ASSEMBLY  PERBOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND BULKHEAD SKIN CRACKED AT BS 178, LBL 5.5.  REPAIRED PER SWA RA 1-253-1043.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD GALLEY DOOR, FORWARD SIDE, UPPER CORNER CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM UPPER T CAP CORRODED AT BS 328, LBL34 TO RIGHT SIDE OF FUSELAGE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 344, RBL 22.  REPAIRED PER SWA RA 1-253-426.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 19L CRACKED AT BS 1088.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED AT BOTTOM OF KEEL BEAM WEB, BS 711, LBL 6.3, BELOW STANDBY HYD PUMP.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 7R CRACKED AT AFT FASTENER HOLE, BS 1106.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND 3 INCH CRACK AT INBOARD J FLANGE OF BELTFRAMES AT BS 907 AND 867, BETWEEN STRINGERS22 AND 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD CARGO BIN FLOOR BEAMS CORRODED AT BS 430, LBL 13, 8.5, 2.5 AND BS 504, LBL 18, 13, 8.5, 2.5, AND  RBL 8.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CRACKED AT BS 706, LBL 24.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 1016, LBL 8.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND VERTICAL ATTACH ANGLE CRACK AT BS 178, LBL 6.  REPAIRED PER SWA RA 1-253-1038.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT ENTRY DOOR CUTOUT CRACKED AT UPPER AFT CORNER.  REPAIRED PER SWA ACO 6134-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND UPPER WING L/E SKIN CRACKED AT NUMBER 3 SLAT ACTUATOR CUTOUT.  REPAIRED PER SWA RA 1-257-196.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SEAT TRACK CORROSION AT BS 989.5 TO 1013,  RBL 39, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD ENTRY DOOR CUTOUT, FORWARD 10 INCH AREA AT STR.7L, BS 294 WEB CRACKED AT AFT END OF RADIUS.  REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 685 STR 8L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 686.5, LBL 6 TO  RBL 49, WL 207.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND HAT CHANNEL CORRODED AT BS 993.5, LBL 14-44, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND FLOOR BEAM CRACKED AT AILERON BELLCRANK CUTOUT, BS 663.75.  REPAIRED PER SWA ACO 523-57.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND Z-ANGLE CRACKED AT BS 291 TO 296.5, STRINGER 17R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND STRINGER 24R CRACKED JUST AFT OF CARGO DOOR.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND STRINGER 10L, AT FORWARD ENTRY DOOR CUTOUT, BS 360, LOWER SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND BELT FRAME LEG CRACKED AT BS 967, ABOVE AFT ENTRY DOOR CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND BELT FRAME CRACKED AT BS 989.5, ABOVE AFT ENTRY DOOR CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND SHEARED RIVETS IN INTERCOSTAL AT HORIZONTAL FLANGE, FWD BULKHEAD BS 178, WL 195.7,RBL 23.5 AND LBL 25.5.  REPAIRED PER SWA RA 1-253-1041.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND T-EXTRUSION CRACKED  ON INBD AND OUTBD FLANGES, FORWARD BULKHEAD, BS 178. LBL 6, WL 186.2.  REPAIRED PER SWA RA 1-253-1041.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND CRACK IN THE VERTICAL LEG OF UPPER FWD CHORD ANGLE OF PRESSURE DECK AT BS 663.5  AT BL 0 AT WL 208.5.  REPAIRED PER SWA RA 1-257-195.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND CRACK IN THE VERTICAL LEG OF UPPER FWD CHORD ANGLE OF PRESSURE DECK AT BS 663.5  AT RBL 24.75  AT WL 208.5.  REPAIRED PER SWA BOEING DRAWING 691A0032.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND CRACK IN THE VERTICAL LEG OF UPPER FWD CHORD ANGLE OF PRESSURE DECK AT BS 663.5  AT LBL 24.75 AT WL 208.5.  REPAIRED PER SWA BOEING DRAWING 691A0032.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND CRACK IN RADIUS AFT SIDE OF BELTFRAME, BS 559 AT RBL 73, BELOW CREASE BEAM STR.17R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND CRACK IN RADIUS AFT SIDE OF AFT BELT FRAME OUTBD ATTACH ANGLE, RBL 73, BS 579  BELOW CREASE BEAM.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND STRINGER 22R CRACKED ON UPPER FLANGE AFT OF FWD CARGO DOOR FRAME.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND FORWARD ENTRY DOORWAY BEARSTRAP CRACK UNDER FWD UPPER STOP FITTING.  REPAIRED PER SWA RA 1-253-1039.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND SEAT TRACK SPLICE CORRODED AT BS 907, RBL 24.5.  REPAIRED PER SWA RA 1-253-1040.


REMARKS:
DURING SCHEDULED HALF D-CHECK, FOUND CRACKS AT OVAL CUTOUTS AT BS 670 RBL 24 FLOOR BEAM.  REPAIRED PER SWA RA 1-257-197.


REMARKS:
FOUND FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE LOW.  REPLACED SLIDE ASSEMBLY.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 530 BETWEEN STR 23 AND 24L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT LAV FLOOR SUPPORT BRACKET CORRODED AT BS 1013, LBL 5, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEBS AT BS 178-188 LEFT AND RIGHT SIDES CRACKED BS 178-188, WL 195, RBL 25.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL L-ANGLE CRACKED AT BS 927 TO 947, BL 0.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, RBL 56 TO 9, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 727, STR 9L, LBL 65, WL 270.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CORROSION AT BS 951, RBL 33, WL 207.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 616.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER GOUGED AT BS 559, S6L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT 19R CRACKED AT BS 727B.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CRACKED AT BS 354, S16R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOP SILL CORRODED AT  BS 940-1000.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 993, 980, AND 976, LBL 45, 46, AND LBL 47, WL 208.  REPLACEDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK,  FOUND FORWARD CARGO FLOOR BEAM WEB AT INBOARD EDGE OF THRESHOLD CRACKED IN THREE PLACES.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND AFT ENTRY DOOR ESCAPE SLIDE PRESSURE LOW.  REPLACED SLIDE ASSEMBLY PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND FORWARD ENTRY DOOR EXTERIOR ESCAPE SLIDE EMERGENCY LIGHT INOP.  REPLACED EMERGENCY LIGHT RECEPTACLE PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAMS CORRODED AT BS 1014, LBL 36, WL 208 AND AT BS 344, RBL 9 TO 30, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 530, BETWEEN STRINGERS 23-24L.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT WING L/E ILLUMINATION LIGHT SUPPORT STRINGERS CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACK AT INBOARD LOWER CORNER OF NUMBER 2 ENGINE PYLON, AFT SUPPORT FRAME AT  STA 315, AFT OF PANEL 5843R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT AILERON O/B CENTER HINGE TO UPPER SKIN ANGLE CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A CHECK, FOUND FORWARD ENTRY DOOR SLIDE PRESSURE BELOW SERVICEABLE LIMITS.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 4073, DURING MAINTENANCE FERRY FLIGHT, THRUST REVERSER ISOLATION LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO IND AND MADE AN UNEVENTFUL LANDING.  CLEANED NOSE GEAR AIR/GROUND SWITCH.


REMARKS:
FLIGHT 017, ON TAKEOFF, NUMBER 1 WHEEL ASSEMBLY SEPARATED FROM AIRCRAFT.  AIRCRAFT CONTINUED TO DAL AND MADE AN UNEVENTFUL LANDING.  INSPECTED AIRCRAFT STRUCTURE AND LANDING GEAR.  REPLACED RIGHT MAIN GEAR INNER CYLINDER, BOTH BRAKE ASSEMBLIES, AND BOTH WHEEL ASSEMBLIES.  PERFORMED GEAR RETRACTION TEST.


REMARKS:
DURING SCHEDULED QUARTER D-CHECK, FOUND A CRACK IN LEFT WING L/E SKIN WHERE NUMBER 5 SLAT O/B LOWER SKIN WEDGE SEAL CONTACTS WING L/E SKIN SURFACE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D-CHECK, FOUND A CRACK IN LEFT L/E WING SKIN CUTOUT FOR NUMBER 1 L/E SLAT AT I/B AUX TRACK.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D-CHECK, FOUND AFT EDGE OF NUMBER 5 SLAT AUX TRACK CUTOUT IN WING L/E SKIN CRACKED.  REPAIRED PER SWA RA 1-257-204.


REMARKS:
DURING SCHEDULED QUARTER D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 900L, STRINGER 26L.  REPAIRED PER SWA RA 1-253-1046.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND L/E CAVITY AT RIGHT WING STA 470 DELAMINATED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0021.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 23L CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 504, ON TAKEOFF,  LEFT OUTBOARD MAIN GEAR TIRE BLEW OUT.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  INSPECTED AIRCRAFT.  FOUND DAMAGE TO LEFT GEAR INNER DOOR, AFT FLAP, FOREFLAP, MIDFLAP AND ONE WING PANEL.  REPLACEDINNER GEAR DOOR, FOREFLAP, MIDFLAP, AND NUMBER 4 SPOILER PER BOEING M/M.  REPAIRED WING PANEL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 4318, IN CRUISE, AT 37,000 FT, LOST CABIN PRESSURE.  CREW INITIATED DESCENT TO 11,000 FT PASSENGER OXYGEN MASKS DEPLOYED AND OXYGEN GENERATORS EXPENDED.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT BWI.  REPLACED BOTH SAFETY PRESSURE RELIEF VALVES, REPLACED EXPENDED O2 GENERATORS AND REPACKED MASKS PER BOEING M/M.


REMARKS:
PHL - FLT 187 - AFTER LANDING GEAR RETRACTION ON TAKEOFF, HAD UNUSUAL NOISE AND VIBRATION.  FLIGHT RETURNED.  FOUND RT NOSE LANDING GEAR DOOR OPEN.  CLOSED AND LATCHED RT NOSE LANDING GEAR DOOR.  LANDING GEAR DOOR OPERATION NORMAL.  CHECK C-3, 4-6-93, STL.


REMARKS:
JFK - FLT 185 - DURING CLIMB, SHUT DOWN NR 3 ENGINE, SN 1528, DUE TO FUEL FLOW, N1 AND N2 FLUCTUATION AND VIBRATION.  REPLACED ENGINE FUEL PUMP, MFG PN 278200, AND ENGINE FUEL CONTROL, MFG PN 743602-3.  ENGINE OPERATION AND LEAK CHECK, CHECKED NORMAL.  CHECK C-1 10-25-93, MCI.


REMARKS:
JFK - FLT 185 - DURING CLIMB, SHUT DOWNNR 3 ENGINE, SN 1528, DUE TO FUEL FLOW, N1 AND N2 FLUCTUATION AND VIBRATION.  REPLACED ENGINE FUEL PUMP, MFG PN 278200, AND ENGINE FUEL CONTROL, MFG PN 743602-3.  ENGINE OPERATION AND LEAK CHECK, CHECKED NORMAL.  CHECK C-1 10-25-93, MCI.


REMARKS:
FLIGHT 845, FOUND AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BELOW SERVICEABLE LIMIT.  REPLACED SLIDE ASSEMBLY PER BOEING M/M.


REMARKS:
FLIGHT  078, FOUND CABIN EMERGENCY EXIT LIGHTS, AFT OF ROW 18, INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER 2R CLIP DAMAGED, BS 380.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 366, 1.5 INCH ABOVE STRINGER 10L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
JFK - PRIOR TO LANDING, NOSE GEAR DID NOT EXTEND UNTIL RECYCLED.  REPLACED RETRACT ACTUATOR, MFG P/N 65-7276235.  OP CHECKS NORMAL.


REMARKS:
CLT - NR 2389 - THE FORWARD ENTRY DOOR OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY AND LIGHT FIXTURE.  OPS CHECKS GOOD.  (Z)


REMARKS:
DURING SCHEDULED B CHECK, FOUND CABIN EMERGENCY EXIT LIGHT AT ROW 7B INOP.  REATTACHED EMERGENCY LIGHT PER BOEING M/M.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKIN GOUGED AND DENTED FROM BS 380 TO 385, ABOVE STR 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKIN CREASED FROM BS 384 TO 392, ABOVE STR 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 395.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKIN GOUGED AND DENTED AT BS 310, STR 18-19L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 1000,  BETWEEN STR 13-14R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SKIN GOUGED AT BS 1012, AT STR 18R AND AT BS 360-380, BETWEEN STR 5L AND 6L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER FLANGE DENTED AT BS 1013, STR 1.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, FROM LBL 10 TO RBL 29, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 18 TO RBL 53, WL 208.  REPAIRED PER SWA RA 1-353-542AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SEAT TRACK CORROSION FROM BS 328 TO 480, RBL 45, WL 208, AND AT BS 943, 936, RBL 45, WL208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 578, STR 11R, BS 727E, STR 4R, BS 727D, STR 5L, 6L, 7L, BS727C, STR 5 AND 7L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND UPPER CHORD L-ANGLE ON WEB AT BS 380-400 CRACKED AT BS 380-400, BL 0.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 344, BL 0, WL 207.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED ENGINE CHANGE, FOUND CRACKED CROWN STRINGER AT NUMBER 1 ENGINE PYLON.  REPAIRED PER SWA RA  1-354-068.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, AT STRINGER 24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 787, IN CRUISE, NOTED NUMBER 2 ENGINE OIL QUANTITY DROP.  AIRCRAFT DIVERTED TO ABQ AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND NUMBER 2 ENGINE OIL TANK TRANSFER TUBE LEAKING.  REMOVED AND REPLACED TUBE AND O-RINGS.  RESERVICED ENGINE OIL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP.  REPLACED EXIT LIGHT PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD LEFT, FORWARD AISLE, AND FORWARD RIGHT CABIN EMERGENCY TRACK LIGHTS  INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND HEAVY CORROSION UNDER GIRT BAR FITTING AT FORWARD ENTRY DOORWAY.  REMOVED CORROSION AND REPLACED FITTING PER BOEING STRUCTURAL REPAIR MANUAL AND BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT LIGHT INOP.  REPLACED BATTERIES PER BOEING M/M.


REMARKS:
FLIGHT 359, IN  CRUISE, NUMBER 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH ASSOCIATED OIL QUANTITY  DROP.  CREW PERFORMED NUMBER 2 ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT AT MSY.  INSPECTED AND FOUND ENGINE OIL SCAVENGE LINE B-NUT LOOSE.  RETORQUED SAME AND SERVICED OIL TO PROPER LEVEL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 328, BL 0 TO RBL 49.5, WL 207.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND Z CHANNEL CORRODED AT BS 263, BL 5R, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 27.5, WL 208.1.  REPAIRED PER SWA RA 1-353-427.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 264, BETWEEN STRINGERS 17 AND 18L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED 5 INCHES AFT AND 24 INCHES BELOW OXYGEN INDICATOR DISC.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND CABIN EMERGENCY EXIT LIGHTS AT ROW 12 INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DSM - FLT 508 - AFTER TAKEOFF NOSE LANDING GEAR WOULD NOT RETRACT.  FOUND NOSE LANDING GEAR STRUT FULLY DEFLATED.  SERVICED NOSE LANDING GEAR STRUT WITH NITROGEN AND FLUID.  LANDING GEAR OPERATION THEN NORMAL.  CHECK C-12, 8-16-93.  PHX


REMARKS:
DSM - FLT 1563 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR GREEN, DOWN AND LOCKED LIGHT DID NOTILLUMINATE.  VISUALLY VERIFIED NOSE LANDING GEAR WAS DOWN.  REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH, MFG PN H14-6.  NOSE LANDING GEAR INDICATION CHECKED NORMAL.  CHECK C-10, 7-29-93, STL.


REMARKS:
MCO - FLT 24 - AFTER TAKEOFF, UNABLE TO ADJUST PRESSURE, RETURNED TO MCO.  FOUND PRESS CONTROLLER ERRATIC, REMOVED AND REPLACED PRESSURE CONTROLLER, OPS CHECK OK AS PER MM 21-31-00.  (W)


REMARKS:
DURING Q-3 INSPECTION, FOUND 2 CRACKS .75 AND .5 INCH LT WING AFT LOWER SPAR AT NR 1 FLAP HINGE LOWER INBD ATTACH BOLT 5 O'CLOCK AND 7 O'CLOCK POSITION.  INSTALLED DOUBLER REPAIR PER EO 5788D220 AND DWG NR J060271-504.  (W)


REMARKS:
DURING Q-3 INSPECTION, FOUND A 1 INCH CRACK IN FORMER AT STA 658 LT OUTBD SIDE OF CANTED KEEL.  REPAIRED FORMER PER SRM53-03, FIGURE 12.  (W)


REMARKS:
RDU - FLT 687 - AFTER TAKEOFF, THE CREW WAS UNABLE TO RETRACT THE NOSE LANDING GEAR.  THE FLIGHT RETURNED TO RDU AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE NOSE GEAR PISTON AND AXLE ASSEMBLY PER MM 32-21-2 AND SERVICED AIR AND OIL.  EXTENSION AND RETRACTION.  OPS CHECKED OKAY.  (W)


REMARKS:
PIT - FLT 586 - THE COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED THE COCKPIT EMERGENCY LIGHTS BATTERY PACK.  OPS CHECKS NORMAL.  (W)


REMARKS:
FLL - FLT 1476 - THE FORWARD ENTRANCE DOOR EMERGENCY CHUTE DEPLOYED.  ATL MAINTENANCE REPLACED THE DOOR CHUTE PER MM 25-61-03.  (W)


REMARKS:
CLT - THE EMERGENCY EXIT LIGHTS INOPERATIVE.  MAINTENANCE REPLACED THE C-BATTERY PACKS AT SEATS 2 A AND C AND AT 14 A AND C.  OPS CHECKS OKAY.  (W)


REMARKS:
PIT - FLT 2266 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE SERVICED THE NOSE STRUT WITH AIR.  OKAY FOR SERVICE.  (W)


REMARKS:
PIT - FLT 138 - AFTER TAKEOFF, THE CREW COULD NOT PRESSURIZE AIRCRAFT.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT.  FLIGHT ATTENDANTS NOTICED A LOUD HISSING FROM THE FORWARD ENTRY DOOR.  MAINTENANCE REPLACED THE DOOR SEAL AND THE C-LATCH PLASTIC LOG COVERS.  PRESSURIZED AIRCRAFT, LEAK CHECKS OKAY.  OKAY FOR SERVICE.  (W)


REMARKS:
PHL - FLT 1501 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT.  THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT.  MAINTENANCE SERVICED THE NOSE STRUT WITH AIR AND OIL PER MM.  SWUNG NOSE GEAR SEVERAL TIMES AND OPS CHECKS GOOD.  (W)


REMARKS:
PBI - FLT 416 - AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE.  FLIGHT ATTENDANT REPORTED L2 DOOR VERY NOISY.  THE FLIGHT RETURNED TO PBI.  MAINTENANCE FOUND L2 DOOR OUT OF SEQUENCE AND RECYCLED.  INSPECTED ACM DUCTING AND CHECKS SATISFACTORY.  PRESSURIZED AIRCRAFT, SYSTEM OPS GOOD.  (W)


REMARKS:
PIT - FLT 331 - AFTER TAKEOFF, THE LT OIL STRAINER CLOGGING LIGHT ILLUMINATED.  THE CREW REDUCED THE POWER AND THE LIGHT REMAINED ON AT IDLE.  THE FLIGHT RETURNED TO PIT.  MAINTENANCE REPLACED THE LT ENGINE ASSEMBLY PER WORK CARD JD71-00-1.  (W)


REMARKS:
JAX - FLT 99 - WHILE EN ROUTE RSW-PIT, THE CREW LOST B-SYSTEM HYDRAULICS.  THE FLIGHT DIVERTED TO JAX AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, THE CONE DRAIN AND THE B-SYSTEM RETURNED FILTERS.  OPS AND LEAK CHECK GOOD.  (W)


REMARKS:
CLT - FLT 19 - THE COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE FOUND SHORTED LIGHT SOCKET ON OVERHEAD PANEL.  REPOSITIONED SOCKET AS REQUIRED.  OPS CHECK GOOD.  (W)


REMARKS:
TPA - FLT 559 - AFTER TAKEOFF, THE SMOKE DETECTORS WENT OFF IN BOTH LAVATORIES DUE TO SMOKE IN THE CABIN.  THE FLIGHT RETURNED TO TPA AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE APU ASSEMBLY PER JOB CARD JEF-49-00-1, OPSNORMAL.  (W)


REMARKS:
EWR - FLT 217 - WHILE EN ROUTE, THE NR 2 ENGINE OIL PRESSURE DROPPED TO 17 PSI.  THE CREW SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND CONTINUED TO EWR AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 2 ENGINE.  (W)


REMARKS:
PIT - FLT 1190 - THE LT AFT EMERGENCY EXIT LIGHT AT ROW 12 WAS INOPERATIVE.  MAINTENANCE REPLACED THE BULB.  OPS CHECK GOOD.  (W)


REMARKS:
CLT - FLT 1707 - THE LT EMERGENCY EXIT LIGHT BURNED OUT.  MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT.  OPS CHECK OKAY.  (W)


REMARKS:
BWI - FLT 477 - AFTER TAKEOFF, UNABLE TO RETRACT LANDING GEAR.  THE FLIGHT RETURNED TO BWI.  MAINTENANCE REMOVED ICE DEBRIS FROM LANDING GEAR CONTROL VALVE AND DEICED.  CONTROL VALVE LINKAGE OPERATIONAL, CHECKS NORMAL.  (W)


REMARKS:
CLE - FLT 1797 - AFTER TAKEOFF, UNABLE TO RETRACT LANDING GEAR.  THE FLIGHT RETURNED TO CLE.  MAINTENANCE LUBED ALL GEAR AND SERVICED THE NOSE STRUT PER MM, SWUNG GEAR SEVERAL TIMES AND OPS CHECKS OKAY.  (W)


REMARKS:
PIT - FLT 473 - AFTER TAKEOFF, THE NOSE GEAR UNSAFE LIGHT REMAINED ON WITH ALL GREEN LIGHTS OUT.  THE CREW RECYCLED THEGEAR AND THE SAME PROBLEM EXISTED.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE SERVICED NOSE STRUT WITH AIR AND OIL PER MM.  SWUNG GEAR SEVERAL TIMES AND ALL INDICATIONS AND OPS NORMAL.  (W)


REMARKS:
PIT - FLT 599 - AFTER TAKEOFF, THE RED NOSE GEAR LIGHT REMAINED ON AND THE NOSE GEAR WOULD NOT RETRACT.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPACKED THE NOSE GEAR IAW JOB CARD JD32-20-7.  SWUNG GEAR SEVERAL TIMES, OPS CHECK GOOD.  (W)


REMARKS:
BOS - FLT 908 - WHILE EN ROUTE PWM-PHL, THE CREW RECEIVED A LT GEAR UNSAFE LIGHT ON THE GEAR HANDLE UP POSITION.  THE FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE LT MLG DOWNLOCK SWITCH.  OPS CHECKSGOOD PER MM 32-60-1.  (W)


REMARKS:
CLT - FLT 2221 - AFTER TAKEOFF, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT.  THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE HIGH STAGE VALVE PER MM 36-10-00.  OPS CHECK GOOD, PRESSURIZED AIRCRAFT, NO PROBLEMS FOUND.  (W)


REMARKS:
CLT - FLT 1068 - ON APPROACH TO GSP, THE SLATS EXTENDED NORMALLY BUT NO FLAP INDICATION.  THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE PERFORMED A GROUND CHECK OF FLAPS, COULD NOT DUPLICATE.  OPS CHECK NORMAL PER MM.  (W)


REMARKS:
IND - FLT 138 - WHILE EN ROUTE PIT-ODR, THE CREW EXPERIENCED A PRESSURIZATION PROBLEM.  THE FLIGHT DIVERTED TO IND AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE AVIONICS COOLING OUTLET VALVE.  PERFORMED LEAK CHECK TO 7/75 PER MM 21-31-00.  OPS CHECK NORMAL.  (W)


REMARKS:
INT - DURING 'PCI' CHECK VISUAL INSPECTION, FOUND A 1.5 INCH BY 8 INCH CORROSION BS 1000 TO BS 1014 AT S 29L.  CORROSION TASK NR C53-113-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
FLIGHT 923, IN CRUISE, APU FIRE WARNING LIGHT ILLUMINATED, WITH APU OFF.  APU FIRE BOTTLE DISCHARGED.  AIRCRAFT LANDED AT PHX WITHOUT INCIDENT.  INSPECTED APU AREA WITH NO EVIDENCE OF FIRE.  REMOVED AND REPLACED APU FIRE LOOP SENSOR AND APU FIRE BOTTLE PER BOEING M/M.


REMARKS:
DURING SCHEDULED A CHECK, FOUND FUSELAGE SKIN CRACK AT BS 312, 2.5 INCH FROM FORWARD DOORWAY.  REPAIRED PER SWA RA 1-253-1048.


REMARKS:
LGA - FLT 208 - AT START OF DESCENT WITH POWER REDUCTION, RT AIR CONDITIONING PACK TEMPERATURE BEGAN TO RISE AND A SMOKE HAZE APPEARED IN CABIN.  OPERATED AIR CONDITIONING PACK IN MANUAL.  MANUAL AIR CONDITIONING PACK WAS NORMAL AND SMOKE DISSIPATED.  OPERATED BOTH AIR CONDITIONING PACKS THROUGH FULL CYCLE IN MANUAL AND AUTOMATIC, ALL INDICATIONS AND OPERATIONS CHECKED NORMAL.  CHECK C-1 8-27-93, MCI.


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION OF KEEL BEAM FORWARD EXTENSION, STRINGER 28R, STA 724-740.  REMOVED AND REPLACED EXTENSION PER SRM 51-10-1.  AIRCRAFT TOTAL CYCLES 43,339.


REMARKS:
STL - FLT 633 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR AND VISUALLY CHECKED RT MAIN LANDING GEAR WAS DOWN.  FOUND MASTER DIM AND TEST CARD, MFG PN 69-48272-3, MALFUNCTIONING.  REPLACED MASTER DIM AND TEST CARD AND LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL.  CHECK C-1, 11-9-93, MCI.


REMARKS:
MCI - DURING C-CHECK, FOUND CRACK APPROXIMATELY .25 INCH LONG, IN FORWARD FLANGE CASTING ABOVE STRINGER 18R, STA 940.  INSTALLED NEW CASTING PER SB 727-53-0018.  TOTAL CYCLES 41,802.


REMARKS:
JFK - FLT 393 - AFTER TAKEOFF, DURING LANDING GEAR RETRACTION, RT MAIN LANDING GEAR WOULD NOT RETRACT.  CYCLED LANDING GEAR.  FOUND RT MAIN LANDING GEAR RETRACT CYLINDER, MFG PN 65-17830-13, BYPASSING HYDRAULIC FLUID.  REPLACED RT MAIN LANDING GEAR RETRACT CYLINDER AND LANDING GEAR OPERATION CHECKED NORMAL.  CHECK C-1 10-9-93, MCI.


REMARKS:
INT - DURING PCI CHECK VISUAL INSPECTION, FOUND 5 INCH BY 5 INCHES OF CORROSION STA 660 STR 28 L TO STR 28 R.  CORROSION TASK NR C53-113-01, CORROSION LEVEL 2.  REPAIRED PER SRM 53-30-2.  (W)


REMARKS:
DURING SCHEDULED D CHECK, FOUND T ANGLE CORRODED AT BS 794.3, WL 165, RBL 45.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND WEB CRACKED AT BS 178-180, LBL 25, WL 195.  REPAIRED PER BOEING SL 737-SL-53-22-A AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND RIGHT FORWARD SERVICE DOOR ESCAPE SLIDE PRESSURE LOW.  REPLACED SLIDE ASSEMBLY PER BOEING M/M.


REMARKS:
FLIGHT 696, IN CRUISE, EXPERIENCED ELECTRICAL SMOKE AND ODOR IN AFT GALLEY.  GALLEY POWER TURNED OFF, BUT ODOR PERSISTED.  AIRCRAFT DIVERTED TO AMA AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND GALLEY WORK LIGHT BALLAST BURNED.  REPLACED BALLAST PER BOEING M/M.


REMARKS:
DURING SCHEDULED A CHECK, FOUND NUMBER 1 L/E SLAT INBOARD AUX TRACK CUTOUT CRACKED IN TWO PLACES.  REPAIRED PER DYNAIRWO 7500-02-P072.


REMARKS:
DURING SCHEDULED A CHECK, FOUND STRINGER 8A CRACKED AT FORWARD SERVICE DOOR.  REPLACED STRINGER PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 235, RBL 10.  REPAIRED PER TRAMCO EWO 94-0061.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 663 FRAME CRACKED TWO PLACES UNDER STRINGER 3L.  REPAIRED PER TRAMCO EWO 94-0045.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CHANNEL BENT AT BS 765-769, WL 155, LBL 3.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STRINGER 13L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT  INOP.  REPLACED BATTERY PACK PER BOEING MAINTENANCE.


REMARKS:
FOUND CABIN FLOOR TRACK LIGHTING WIRE COVER MISSING AND WIRE BROKEN.  REPAIRED BROKEN WIRE AND INSTALLED COVER.


REMARKS:
FOUND EXIT LIGHT AT LEFT OVERWING EXIT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
FOUND EXIT LIGHT AT OVERWING EXIT INOP.  REPAIRED BROKEN WIRES AND REPLACED ONE LIGHT LENS PER BOEING M/M..


REMARKS:
FLIGHT 1990, WHILE TAXIING OUT, A BURNING ODOR WAS DETECTED IN CABIN.  OPERATED LEFT PACK AND ODOR REMAINED IN FRONT AREA OF CABIN.  REPLACED AIR CYCLE MACHINE AND RECIRCULATING FAN PER BOEING M/M.


REMARKS:
FOUND CENTER OVERHEAD AISLE EMERGENCY LIGHT INOP.  REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER BOEING M/M.


REMARKS:
FOUND FLOOR EMERGENCY TRACK LIGHTING AT ROW 16 LOOSE FROM  FLOOR.  RESECURED TRACK LIGHTING.


REMARKS:
FOUND EMERGENCY EXIT LIGHT ON CEILING INOP.  RESECURED TERMINAL SCREW.


REMARKS:
MIA - FLT 2234 - AFTER TAKEOFF, THE RT AIR CONDITIONING PACK TRIPPED WITH THE PACK SWITCH ON.  THE CABIN FILLED WITH SMOKE.  THE FLIGHT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE TURBO FAN AIR VALVE AND CLEANED THE COCKPIT AIRFLOW SENSOR VENT LINE.  GROUND CHECK OKAY.  (W)


REMARKS:
BWI - THE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE.  MAINTENANCE REPLACED THE LT AND RT OVERWING EMERGENCY EXIT BATTERY PACKS.  OPS CHECK OKAY.  (W)


REMARKS:
STL - DURING CRUISE, NR 1 FOOD SERVING CART POSITION STARTED SMOKING.  DISCONNECTED SERVING CART.  FOUND CONTROL MODULE, MFG P/N 916583 HAD OVERHEATED.  REPLACED CONTROL MODULE AND SERVING CART OPERATION CHECKED NORMAL.  CHECK C-2A.


REMARKS:
DURING LANDING LEFT RUNWAY LIGHT SWITCH, MFG P/N A3-1219, EMITTED SPARKS AND SMOKE.  TURNED OFF SWITCH.  REPLACED RUNWAY TURNOFF LIGHT SWITCH, LIGHT OPERATION CHECKED NORMAL OP 17.


REMARKS:
AFTER TAKEOFF DURING LANDING GEAR RETRACTION, RIGHT MAIN LANDING GEAR RED LIGHT AND LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR AND LIGHTS WENT OUT.  FOUND RIGHT MAIN LANDING GEAR ACTUATOR, MFG P/N 65-72761-91, BYPASSING HYDRAULIC FLUID.  REPLACED RIGHT MAIN LANDING GEAR ACTUATOR.  LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL. CHECK C-2.


REMARKS:
AFTER TAKEOFF RIGHT MAIN LANDING GEAR WOULD NOT RETRACT.  CYCLED LANDING GEAR AND FLIGHT RETURNED.  REPLACED RIGHT MAINLANDING GEAR LOCK ACTUATOR, MFG P/N 65-17819-15, AND DOWN LOCK BUNGEE, MFG P/N 69-15364-3.  LANDING GEAR OPERATION CHECKED NORMAL.  CHECK C-2.


REMARKS:
DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR,MECHANICAL NOSE LANDING GEAR INDICATED DOWN AND LOCKED.  CLEANED NOSE LANDING GEAR LOCK SENSOR AND LOCK SENSOR CONNECTOR.  NOSE LANDING GEAR INDICATION AND OPERATION CHECKED NORMAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND 1.5 INCH CRACK ON LEFT FUSELAGE SKIN BETWEEN BS 787 AND 807.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 395,  BETWEEN STRINGERS 5 AND 6R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT  BS 727B, AT  STRINGER 6R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 987, RBL 43.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 178, RBL 25, WL 195.  REPAIRED PER BOEING SERVICE LETTER 737-SL-53-22-A AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SEAT TRACK CORROSION  AT  BS 487-491, RBL 45, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 1008, STR 19R, WL 200, AT BS 373, STR 21R, WL 178 AND AT BS 436, STR.18R, WL 192.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 520 RIGHT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK,  FOUND FLOOR TRACK LIGHTING AT ROW 2 INOP.  RELAMPED LIGHT PER BOEING MAINTENANCE MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LOWER FORWARD CORNER OF AFT ENTRY DOOR CUTOUT CRACKED.  REPAIRED PER BOEING DRAWING 65C27287.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LOWER FORWARD CORNER OF AFT SERVICE DOOR CUTOUT CRACKED.  REPAIRED PER BOEING DRAWING 65C27287.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED AT BS 1036, BETWEEN STR 19-20R, WL 196.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT FORWARD FRAME CRACKED AT FLOOR LEVEL, BS 294.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND GALLEY DOOR CUTOUT ANGLE CRACKED BELOW STR 13, FORWARD OF DOOR CUTOUT.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAMS CRACKED AT BS 520, LBL 24.74, RBL 24.75, AND 45.0.  REPAIRED PER SWA RA1-353-1049 AND ACO 3198-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, LBL 4.5.  REPAIRED PER SWA RA 1-353-1054.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 14.0, 20.0, 28 .0, 32.0 , 36.0, 40.0, 43.0,  AND 24.0.  REPAIRED PER SWA RA 1-353-1051.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 967, RBL 27.5.  REPAIRED PER SWA RA 1-353-1053.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 967, LBL 5.0.  REPAIRED PER SWA RA 1-353-1052.


REMARKS:
JFK - FLT 2010 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT.  THE FLIGHT RETURNED TO JFK AND LANDED WITHOUT FURTHERINCIDENT.  MAINTENANCE REPLACED THE LOCK ACTUATOR LINE.  OPS CHECKS GOOD.  LEAK CHECKS GOOD AND ACCOMPLISHED NOSE GEAR RETRACTION CHECK PER MM 32-33-0 PAGE 502.  OPERATED NORMAL.  (W)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, STRINGER 15L.  REPLACED CHANNEL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STRINGER 14L.  REPLACED STRINGER CLIP PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT STRINGER 10L CLIP.  REPLACED FRAME PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED AT BS 1002 TO 1016, STRINGER 27L.  REPAIRED STRINGER PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 357, BETWEEN STRINGERS 20 AND 21R, WL 185 AND AT BS 928, BETWEEN S24 AND S25L, WL 165.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND GOUGE AND DENT IN FUSELAGE SKIN OVER FRAME FROM BS 1035 TO 1045, BETWEEN STRINGERS 14 AND 15L, WL 235.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF RIGHT MAIN LANDING GEAR WOULD NOT RETRACT.  CYCLED LANDING GEAR AND FLIGHT RETURNED.  LANDING GEAR DOWN FLIGHT TO MAINTENANCE BASE.  REPLACED LANDING GEAR DOOR SEQUENCE VALVE, MFG P/N 1U1084, AND ACTUATOR, MFG P/N 7-3141-4, LOCK ACTUATOR RESTRICTOR VALVES, MFG P/N 6F1956-11 AND BACV10A504.  GROUND OPERATION OF LANDING GEAR CHECKED NORMAL.  FLIGHT TEST AND LANDING GEAR TESTS NORMAL.


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 19 INCHES BY 1 INCHES OF CORROSION, LBL 17 STA 967-986.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH AREA STA 947 FLOOR BEAM LBL 6.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER 737-300 SRM 53-00-51 FIGURE 202.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK, STR TIE CLIP AT STR 19R STA 986.5.  REPAIRED PER SRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK, STRINGER TIE CLIP AT STR 20L STA 986.5.  REPAIRED PERSRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION ON TOP SURFACE OF T-CAP.  FLOOR BEAM STA 986.5.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 53-00-51.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT WS 760.5.  REPAIRED PER EA 36668.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND HILOCK FASTENER, BS 727 E RBBL 3.00.  REPAIRED PER SRM 53-00-53, FIGURE 201.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 1 INCH CORRODED AREA, STA 956 LBL 33.  CORROSION TASK NR C33-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 51 INCHES BY 2 INCHES OF CORROSION, LT Z-ANGLE STA 998-947.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 19 INCHES BY 1 INCH AREA OF CORROSION, STA 967 TO 986 RBL 17.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 1 INCH, LBL 30 STA 958.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION FOUND 1 INCH SPOT OF CORROSION AT SCREW HOLES, Z-ANGLE AT RT FORWARD SERVICE DOOR BS 281-360 WL 208.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 20 INCHES BY 1 INCH AREA OF CORROSION STA 986 LBL 25 LBL 45.  CORROSIONTASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-05, SRM 53-00-51, SRM 51-70-12.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 51 INCHES BY 2 INCHES CORRODED AREA, RT Z-ANGLE STA 947-998.  CORROSIONTASK NR C-53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1, PAGE 4.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 19 INCHES BY 1 INCH CORRODED AREA, STA 947 TO 967 RBL 40.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 1 INCH CORROSION, STA 947 LBL 5 AND RBL 5.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 53-00-51.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND RIVET HOLES (.1250 INCH AROUND 10 HOLES EA) STA 500D FROM LBL 21.8 TO RBL 21.8.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  REPAIRED PER SRM 53-30-53. (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHES OF CORROSION BS 328 RBL 20.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 53-10-01A SRM 53-10-3.  (W)


REMARKS:
LGA - FLT 516 - AIRCRAFT WOULD NOT PRESSURIZE ON TAKEOFF.  FLIGHT ATTENDANT REPORTED LOUD AIR NOISE AROUND FORWARD ENTRY DOOR.  FLIGHT RETURNED TO LGA AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED FORWARD PASSENGER DOOR SNUBBER AND GUIDE ARM.  NO LEAKS, CHECKED GOOD.  REFERENCE CONTROL NR USAA940050.  (W)


REMARKS:
PHL - FLT 0892 - AIRCRAFT DIVERTED TO PHL DUE TO E/M 'R GEN DRIVE' ALONG WITH A DRIVE WARNING LIGHT.  MAINTENANCE FOUNDTHAT THE PRESSURE RELIEF VALVE WAS TRIPPED.  THE IDG, PRESSURE RELIEF VALVE AND THE FUEL OIL COOLER WAS REPLACED.  REFERENCE CONTROL NUMBERS USAA940052 AND 94ZZZW783.  (W)


REMARKS:
CLT - FLT 1449 - AFTER TAKEOFF, THE GEAR OR DOORS DID NOT FULLY RETRACT AND LOCK UP AND LANDING GEAR FAULT ILLUMINATED. CHECK LIST PROCEDURE WAS FOLLOWED, GEAR RECYCLED AND AGAIN RECEIVED THE ALERT.  HOWEVER, A MINUTE LATER, THE CREW HEARD AND FELT A THUD AND THE GEAR APPEARED TO PROPERLY RETRACT WITH NO ALERT.  THE FLIGHT CONTINUED WITH NO FURTHER INCIDENT.  MAINTENANCE LUBED THE MLG PER MM 32-21-07, CYCLED GEAR SEVERAL TIMES AND SYSTEM OPS CHECK GOOD.  (W)


REMARKS:
PHL - FLT 1012 - AFTER TAKEOFF, RECEIVED RT GEAR UNSAFE LIGHTS.  THE CREW RESEQUENCED GEAR UP AND ALL THREE RED LIGHTS CAME ON WITH NO OTHER LIGHTS ON.  THE FLIGHT DIVERTED TO PHL AND WITH GEAR PLACED DOWN, THE CREW RECEIVED THE NORMAL FIVE GREEN LIGHTS AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE CLEANED ICE FROM UPLOCK ON THE RT GEAR, SWUNG GEAR SEVERAL TIMES PER MM 32-00-00 AND CHECKED GOOD.  (W)


REMARKS:
CMH - FLT 1152 - WHILE EN ROUTE CVG-IAD, THE CREW SHUT DOWN THE NR 2 ENGINE DUE TO LOW OIL PRESSURE WARNING.  THE FLIGHT DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTER GASKET.  RAN NR 2 ENGINE, OPS AND LEAK CHECKS GOOD.  ALL ENGINE PARAMETERS NORMAL.  (W)


REMARKS:
LGA - FLT 1174 - AFTER TAKEOFF, UNABLE TO PRESSURIZE AIRCRAFT.  THE FLIGHT RETURNED TO LGA.  MAINTENANCE PERFORMED CHECK OF PRESSURIZATION SYSTEM PER MM 21-31-00, PAGE 201 AND ALL CHECKS GOOD.  PRESSURIZED AIRCRAFT TO 4.5 PSI AND NO LEAKS FOUND.  LUBRICATED HIGH PRESSURE AIR CONNECTION CHECK VALVE AS PRECAUTIONARY AND SYSTEM CHECKS NORMAL.  (W)


REMARKS:
CLT - WHEN AIRCRAFT WAS POWERED UP, THE EMERGENCY LIGHTS IN AIRCRAFT WOULD NOT EXTINGUISH.  MAINTENANCE FOUND CHAFED WIRE AT AFT FLIGHT ATTENDANT PANEL AND REPAIRED WIRE.  LIGHTS, OPS CHECK GOOD.  (W)


REMARKS:
BOS - FLT 17 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT.  THE FLIGHT RETURNED TO BOS AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE LOCK SENSOR CONDUIT, LUBED THE TORQUE LINKS, CHECKED STRUT SERVICING, SWUNG NOSE GEARSEVERAL TIMES AND OPS CHECK NORMAL.  (W)


REMARKS:
ROC - FLT 1871 - AFTER TAKEOFF, UNABLE TO RETRACT LANDING GEAR.  THE FLIGHT RETURNED TO ROC AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE ADJUSTED THE TELEFLEX FOR THE AIR GROUND SENSOR PER MM 32-09-200, CHECKED OKAY.  (W)


REMARKS:
PIT - FLT 8033 - AFTER TAKEOFF, THE RED RT GEAR UNSAFE LIGHT REMAINED ON WITH THREE GREEN LIGHTS OUT AND THE AMBER GEARDOOR OPEN LIGHT OUT.  THE CREW RECYCLED THE GEAR WITH SAME INDICATIONS.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE PROXIMITY HARNESS, SWUNG GEAR AND INDICATIONS CHECKED GOOD.  (W)


REMARKS:
INT - DURING PCI CHECK VISUAL INSPECTION FOUND 1.5 INCH BY 8 INCHES AREA OF CORROSION BS 1000 TO BS 1014 AT S29L.  CORROSION TASK NR C53-113-01.  CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT - DURING PCI CHECK VISUAL INSPECTION FOUND 1.25 INCHES BY 6 INCHES OF CORROSION BS 340 THROUGH BS 346.  CORROSION TASK NR C53-202-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1 ITEM 4, PAGE 5.  (W)


REMARKS:
DTW - DURING FLIGHT 1031 THE NR 2 HYDRAULIC SYSTEM QUANTITY INDICATOR WAS ERRATIC AND UNRELIABLE.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 HYDRAULIC SYSTEM QUANTITY INDICATOR TRANSMITTER.  OPERATION AND LEAK CHECK NORMAL.  (W)


REMARKS:
BDA - FLT 851 - RETURN TO FIELD DUE TO THE CABIN TEMPERATURE UNABLE TO ADJUST NEITHER MANUALLY OR AUTOMATICALLY.  MAINTENANCE REPLACED THE RT FORWARD PACK VALVE.  PACK VALVE OPS NORMAL.  (W)


REMARKS:
PHL - FLT 1778 - IN FLIGHT SHUT DOWN DUE TO E/M 'L ENG BLD OVHT' AND ASSOCIATED LIGHT M 'L ENG BLD OVHT' AND ASSOCIATEDLIGHTS.  FLIGHT CONTINUED TO PHL WITHOUT FURTHER INCIDENT.  MAINTENANCE RPLACED THE LT BLEED OVERTEMP SWITCH.  (W)


REMARKS:
BWI - FLT 1041 - RETURN TO FIELD DUE TO AIRCRAFT UNABLE TO MAINTAIN PRESSURE WITH EITHER PACK OFF.  MAINTENANCE FOUND THE OUTFLOW VALVE LEAKING EXCESSIVELY IN FULL CLOSED POSITION.  REPLACED THE CABIN PRESSURE OUTFLOW VALVE.  CABIN PRESSURIZATION NORMAL.  (W)


REMARKS:
PIT - FLT 0816 - RETURN TO FIELD DUE TO E/M 'L ENG ANTI-ICE'.  ANTI-ICE VALVE REMAINED ILLUMINATED WITH SWITCH ON.  MAINTENANCE REPLACED THE THERMAL ANTI-ICING RELAY AND CYCLED TAT VALVE MANUAL/NORM CONTROL.  OPS NORMAL.  (W)


REMARKS:
EWR - FLT 205 - EN ROUTE LGA TO CHS WHEN RT ENGINE HAD HIGH EGT AND FUEL FLOW.  CREW SHUT DOWN RT ENGINE AND DIVERTED TO EWR WHERE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED VBV MOTOR.  (W)


REMARKS:
PIT - FLT 1505 - NR 1 GENERATOR TRIPPED OFF LINE AFTER TAKEOFF, AND WOULD NOT RESET.  FLIGHT RETURNED TO PIT AND LANDEDWITHOUT INCIDENT.  MAINTENANCE RELEASED ON MEL 24-1.  REPLACED LT ENGINE GENERATOR.  OPS CHECKED GOOD, REMOVED MEL.  (W)


REMARKS:
LGA - FLT 516 - AIRCRAFT WOULD NOT PRESSURIZE ON TAKEOFF.  FLIGHT ATTENDANT REPORTED LOUD AIR NOISE AROUND FORWARD ENTRY DOOR.  FLIGHT RETURNED TO LGA AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED FORWARD PASSENGER DOOR SNUBBER AND GUIDE ARM.  NO LEAKS, CHECKED GOOD.  REFERENCE CONTROL NR 94ZZZW782.  (W)


REMARKS:
PHX - FLT 1856 - THE AFT CARGO FAN APPEARED ON THE STATUS PAGE, THEREFORE, THE AIRCRAFT DIVERTED TO PHX.  MAINTENANCE REPLACED THE AFT CARGO BIN HEATING FAN.  (W)


REMARKS:
PHL - FLT 0892 - AIRCRAFT DIVERTED TO PHL DUE TO E/M 'R GEN DRIVE' ALONG WITH A DRIVE WARNING LIGHT.  MAINTENANCE FOUNDTHAT THE PRESSURE RELIEF VALVE WAS TRIPPED.  THE IDG, PRESSURE RELIEF VALVE AND THE FUEL OIL COOLER WAS REPLACED.  REFERENCE CONTROL NUMBERS 94ZZZW783 AND 94ZZZW784.  (W)


REMARKS:
MIA - FLT 1162 - FLIGHT EN ROUTE TO LGA WHEN CREW UNABLE TO PRESSURIZE AIRCRAFT.  FLIGHT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND AIR LEAK AT LT OVERWING EMERGENCY DOOR HATCH.  REINSTALLED PLUNGER BRACKET.  ALSO, REPLACED RT ACM AND CLEARED MEL ON RT PACK.  FOUND PIN 1 ON PRESSURE CONTROLLER RACK CONNECTOR BURNED 948A.  CLEANED RACK CONNECTOR.  (W)


REMARKS:
CLT - FLT 847 - UNABLE TO PRESSURIZE AIRCRAFT ON CLIMB.  FORWARD FLIGHT ATTENDANT REPORTED LOUD NOISE AT FORWARD ENTRY DOOR.  MAINTENANCE ADJUSTED FORWARD ENTRY DOOR PROGRAMMING ARM.  OPS CHECKS GOOD.  (W)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 182 TO 188 BELOW STR 19L AND AT BS 827, BELOW S14L, WL 232.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STRINGER 10L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CORRODED ON TOP FLANGE AT SIDEWALL SUPPORT, BS 500A AND 500B, WL 156, RBL 25.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME CORRODED AT BS 500, RBL 25, WL 156.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 24L CORRODED AT  BS 876-902.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 26L SPLICE CORRODED AT  BS 907.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AT GATE, FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE ACCIDENTALLY DEPLOYED.  REPLACED SLIDE ASSEMBLY PER BOEING MAINTENANCE MANUAL.


REMARKS:
FLIGHT 1201, NUMBER 4 MAIN GEAR TIRE BLEW ON TAKEOFF.  GEAR WAS NOT RETRACTED.  AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING.  PERFORMED INSPECTION AND REPLACED NUMBER 3 AND 4 MAIN GEAR WHEEL ASSEMBLIES PER BOEING MAINTENANCE MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 360, STR. 20R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
MSP - FLT 361 - DURING DESCENT, RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED.  CYCLED LANDING GEAR AND INDICATED LOCKED.  LANDING GEAR DOWN FLIGHT TO MAINTENANCE BASE.  REPLACED RIGHT MAIN LANDING GEAR UPLOCK ASSY, MFG P/N 65-24482-94 AND SIDE BRACE, MFG. P/N 65-17657-54.  GROUND OPERATION OF LANDING GEAR AND FLIGHT TEST INDICATION NORMAL.  CHECK C-2 - 1-30-94 - MCI.


REMARKS:
JFK - FLT 26 - DURING CRUISE, SHUT DOWN NR 3 ENGINE DUE TO A AND B FIREWARNING LIGHTS ILLUMINATED.   REPLACED AFT LOWERLOOP, MFG. P/N 895899.  RESISTANCE AND MEG CHECK AND OPERATION CHECKED NORMAL.  CHECK C-71 - 1-1-94 - JFK.


REMARKS:
FOUND 2 WHITE EMERGENCY FLOOR TRACK LIGHTS INOP.  RECONNECTED LIGHT STRIP AND OPERATION CHECKED SYSTEM.


REMARKS:
AFT SERVICE DOOR EMERGENCY SLIDE ACCIDENTALLY DEPLOYED AT GATE.  REPLACED SLIDE ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 1004 TO 1013, LBL 7 TO 12, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277.  REPAIRED PER SWA ACO 644-53.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN.  REPLACED LIGHT ASSEMBLY PERBOEING M/M.


REMARKS:
FLIGHT 1452, FOUND EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT STATION INOPERATIVE.  REPLACED FLASHLIGHT BATTERY BOEING M/M.


REMARKS:
PHL - FLT 0892 - AIRCRAFT DIVERTED TO PHL DUE TO E/M 'R GEN DRIVE' ALONG WITH A DRIVE WARNING LIGHT.  MAINTENANCE FOUNDTHAT THE PRESSURE RELIEF VALVE WAS TRIPPED.  THE IDG, PRESSURE RELIEF VALVE AND THE FUEL OIL COOLER WAS REPLACED.  REFERENCE CONTROL NUMBERS USAA940052 AND 94ZZZW784.  (W)


REMARKS:
RDU - FLT 796 - AFTER TAKEOFF WITH THE GEAR HANDLE RAISED THE CREW RECEIVED AMBER ALERT, BUT THE LT AND RT MAINS ILLUMINATED GREEN.  RECYCLED GEAR.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE MAIN GEAR SELECTOR VALVE.  OPS CHECKS NORMAL.  (W)


REMARKS:
DURING SCHEDULED MAINTENANCE CHECK, FOUND LEFT WING TRAILING EDGE BEAM SEAL CRACKED.  REPAIRED PER SWA RA 1-357-212.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD SKIN GOUGED AT BS 1156, WL 268.  REPAIRED PER TRAMCO EWO 94-0114.


REMARKS:
DURING SCHEDULED MAINTENANCE CHECK, FOUND FLOORBEAMS CRACKED AT BS 520 AT LBL 45.5, 24.75, RBL 45.5 AND 24.75.  REPAIRED PER SWA RA 1-353-1066.


REMARKS:
MCI - DURING SPECIAL CHECK FOUND CRACK IN RT WING UPPER REAR SPAR CAP, FORWARD OF NR 8 JACKSCREW.  REPAIRED PER SRM 57-10-6.  AIRCRAFT TOTAL CYCLES 38,164.


REMARKS:
TPA - FLT 545 - DURING CRUISE AND SINGLE AIR CONDITIONING PACK OPERATION, LOST CABIN PRESSURIZATION.  RAPID DESCENT PERFORMED.  CLEANED RT AIR CONDITIONING PACK TEMPERATURE SENSOR AND REPLACED LT AIR CONDITIONING PACK AIR CYCLE MACHINE, MFG PN 204950-5-4.  OPERATION OF AIR CONDITIONING SYSTEMS CHECKED NORMAL.  CHECK C-6, 4-8-93, STL.


REMARKS:
MCI - DURNG OP-17 FOUND 3 INCH CRACK IN STRINGER 29R RADIUS, STA 990.  INSTALLED NEW STRINGER CHORD SECTION PER DWG C03440.  AIRCRAFT TOTAL CYCLES 23,959.


REMARKS:
STL - DURNG C-CHECK FOUND CRACK IN LONGERON 6 LT UPPER FASTENER HOLE AT BELT RING ATTACH, STA 639.  REPAIRED LONGERON PER SRM 53-02, PAGE 2A.  AIRCRAFT TOTAL CYCLES 74,997.


REMARKS:
EWR - FLT 9 - UNABLE TO CONTROL CABIN PRESSURE IN BOTH AUTO AND MANUAL WHEN CABIN AIR MIX VALVES MOVED TO WARM CABIN.  CLIMBS DUCT PRESS NORMAL.  FOUND RT OUTFLOW VALVE DIAPHRAM RUPTURED.  REMOVED AND REPLACED RT OUTFLOW VALVE PER MM 21-30-00.  OPS CHECK OK.  (W)


REMARKS:
FLIGHT 351, DURING TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND ENGINE FAN BLADES  8 THROUGH 14 DAMAGED.  REPLACED ENGINE FAN BLADE ASSEMBLY AND PERFORMED ENGINE POWER ASSURANCE RUN.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND UPPER EMERGENCY FLASHLIGHT INOP.  REPLACED FLASHLIGHT PER BOEING M/M.


REMARKS:
ATH - FLT 881 - DURING CRUISE, NR 1 AND NR 4 ENGINES SPOOLED DOWN.  NR 1 AND NR 4 ENGINE RESTART WAS NORMAL.  CHECKED OPERATION OF FUEL VALVE, FUEL BOOST PUMPS.  DRAINED ENGINE FUEL FILTERS, BLED FUEL CONTROLS AND INSPECTED PS4 LINES, ALL CHECKED NORMAL.  PERFORMED GROUND OPERATIONAL RUNUP AND ENGINES CHECKED NORMAL.  CHECK C-4B, 2-1-94, JFK.


REMARKS:
STL - FLT 648 - DURING DESCENT WHEN POWER WAS REDUCED, NR 1 ENGINE VIBRATION INCREASED TO 4.0 AVM.  SHUT DOWN ENGINE SN1553.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED NR 1 ENGINE.  ENGINE TOTAL TIME 32,630 HOURS, 20,843 CYCLES.  GROUND RUN UP OPERATIONS NORMAL.  CHECK C-2, 2-13-94, MCI.


REMARKS:
FOUND CABIN FLOOR EMERGENCY TRACK LIGHT SECTION INOP.  REPAIRED WIRE PER BOEING M/M.


REMARKS:
FOUND CABIN FLOOR EMERGENCY TRACK WHITE LIGHT BROKEN.  REPLACED LIGHT SECTION PER BOEING M/M.


REMARKS:
FOUND FORWARD AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
FOUND CABIN EMERGENCY EXIT LIGHT AT ROW 12 INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
FOUND CABIN EMERGENCY ESCAPE PATH LIGHT SECTION INOP.  REPAIRED BROKEN WIRES PER BOEING M/M.


REMARKS:
DURING Q-4 INSPECTION, ACCOMPLISHED SID CARD NR 9-58-53702 PSE 53.09.16.  FOUND 2.5 INCH CRACK AT STATION 680 FLOOR BEAM 6 INCHES INBOARD OF RT FUSELAGE SKIN.  REPLACED STATION 680 FLOOR BEAM PER STANDARD PRACTICE.  (Z)


REMARKS:
DURING Q-4 INSPECTION ACCOMPLISHED SID PSE 53-09-030, FOUND .1650 INCH CRACK STATION 83, BETWEEN LONGERON 2 AND 3 RIGHTAT RIVET HEADS (SKIN).  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 38.  (Z)


REMARKS:
DURING Q-4 INSPECTION, ACCOMPLISHED SID PSE 53-09-16 AND FOUND 5 .1650 INCH CRACKS AT STATION 658 RT MAIN FRAME, CRACKSAT RIVETS AND 1 CRACK .5 INCH AT LOWER OUTBOARD END.  ALL CRACKS BELOW FLOOR LEVEL.  REPLACED MAIN FRAME PER STANDARD PRACTICE.  (Z)


REMARKS:
DURING Q-4 INSPECTION ACCOMPLISHED SID PSE 53-09-16, FOUND 3 .1650 INCH CRACKS AT STATION 639 RT MAIN FRAME AT RIVETS BELOW FLOOR.  REPLACED MAIN FRAME PER STANDARD PRACTICE.  (Z)


REMARKS:
DURING Q-4 INSPECTION ACCOMPLISHING SID PSE NR 53-09-029, FOUND 3 CRACKS APPROXIMATELY .3750 INCH LONG AT RIVET HEADS STATION 69 LONGERON L2 AND L3 (SKIN).  INSTALLED FLUSH TYPE REPAIR PER SRM 53-04 FIG 38.  (Z)


REMARKS:
DURING Q-4 INSPECTION ACCOMPLISHING CORROSION CARD NR 9-46-25700-C TASK NR C46-53303, FOUND LEVEL 2 CORROSION STATION 160-200, 6 INCHES INBOARD OF MED THRESHOLD FLOOR ANGLE.  REPLACED FLOOR SUPPORT ANGLE PER STANDARD PRACTICE.  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND 1 INCH CRACK STATION 37 BULKHEAD SKIN AT UPPER RT GUIDE PIN EXTENDING THROUGH RIVET JUST BELOW PIN.  VISUAL INSPECTION.  INSTALLED DOUBLER TYPE REPAIR PER SRM 53-01, FIG 2 SHT 3.  (Z)


REMARKS:
CLT - FLT 1016 - THE 04 DOOR EVACUATION SLIDE ARMING LEVER WAS DIFFICULT TO ENGAGE IN POSITION.  MAINTENANCE REPOSITIONED THE GIRT BAR.  THE LEVER ENGAGED PROPERLY AND THE LIGHT WORKS GOOD.  (Z)


REMARKS:
SEA - FLIGHT 566 - ON PRE-FLIGHT CHECK, FOUND FLOOR PROXIMITY LIGHTS AT ROWS 12 THROUGH 16 LEFT SIDE INOPERATIVE.  MAINTENANCE REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK.  OPS CHECK GOOD.  (Z)


REMARKS:
BWI - FLT 1729 - FLIGHT EN ROUTE BWI TO CLT WHEN NR 2 ENGINE FAILED TO RESPOND TO POWER LEVER MOVEMENTS.  NORMAL ENGINESHUT DOWN WAS ACCOMPLISHED.  FLIGHT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND INBOARD CROSS SHAFTLOOSE.  REASSEMBLED, SECURED AND SAFETIED.  RAN NR 2 ENGINE TO TAKEOFF POWER, ALL ENGINE INDICATIONS CHECK NORMAL.  (Z)


REMARKS:
DAB - FLIGHT 1543 - FLIGHT EN ROUTE CLT TO DAB WHEN HAZE OR FOG DEVELOPED FROM MID-CABIN TO REAR OF AIRCRAFT.  FLIGHT LANDED DAB WITHOUT INCIDENT.  MAINTENANCE CHECKED ACM OIL LEVELS.  RAN AIRCRAFT WITH FULL AIRCRAFT PACKING HOT AND FULL ELECTRICAL LOAD.  UNABLE TO DUPLICATE PROBLEMS.  (Z)


REMARKS:
CLT - FLT 916 - ELECTRICAL SMELL IN CABIN AFTER TAKEOFF.  CABIN AIRFLOW FAN AND TR UNIT NR 1 CIRCUIT BREAKERS POPPED.  FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT.  MAINTNENANCE FOUND WIRES TO NR 1 BUS TRANSFER RELAY BURNED.  REPLACED R3 RELAY.  RESET CIRCUIT BREAKERS AND OPS CHECK NORMAL.  (Z)


REMARKS:
PIT - FLIGHT 1462 - AFTER TAKEOFF NR 1 ENGINE 'A' SYSTEM HYDRAULIC LIGHT CAME ON.  FLUID LEVEL DROPPED TO 1.5 GALLONS.FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR WITH FLAPS RETRACTED AND EXTENDED.  ALL CHECKED NORMAL.  (Z)


REMARKS:
CLT - FLT 1568 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RIGHT ACM.  OPS CHECK NORMAL.  (Z)


REMARKS:
CLE - FLIGHT 263 - FORWARD DOOR EMERGENCY EXIT LIGHTS ON BOTH SIDES INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK ANDREPAIRED WIRES.  OPS CHECKS GOOD.  (Z)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORROSION 10 INCH AFT OF FS 727 E BUTT LINE '0'.  REPAIRED PER SRM 7370300 51-10-02.  (Z)


REMARKS:
PIT - FLT 409 - AFTER TAKEOFF GRN/FLT CONTROL, TAKEOFF CONFIGURATION STAB AND STALL COMPUTER WARNING INDICATED ON THE MFDU.  AIRCRAFT RETURNED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE PROX SWITCH ELECTRONIC UNIT.  OPS AND BITE CHECK NORMAL PER MM 31-41-01D, PAGE 403.  (W)


REMARKS:
PIT - FLT 225 - DURING FLIGHT CABIN ALTITUDE WARNING ANNUNCIATED AT FL 310.  THERE WAS NO EFFECT WITH EITHER AUTO OR MANUAL CABIN CONTROLLER UNTIL DESCENT THROUGH FL210 WHEN BOTH MODES THEN FUNCTIONED OK.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 1 CABIN PRESSURE CONTROLLER.  OPS CHECKS NORMAL.  (W)


REMARKS:
GSO - DURING PCI 797 CHECK VISUAL INSPECTION FOUND A .3750 INCH CRACK, WINDOW POST 'C', OUTER SKIN LOWER END STA 203.8,WL 246.1.  REPAIRED PER EA 25051.  (W)


REMARKS:
INT- DURING Q-4 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 60 INCH CORRODED AREA STA 927-987 RBL 45.  REPAIRED PER SRM 51-10-2 PARAGRAPH 8.  (W)


REMARKS:
INT- DURING Q-4 CHECK VISUAL INSPECTION FOUND SEVERAL AREA 1 INCH BY 2 INCHES (3 EA) (OUT OF LIMITS) CORROSION BS 294.5TO BS 44 LBBL 58.  REPAIRED PER SRM 51-10-02, PAGE 16.  (W)


REMARKS:
INT- DURING Q-4 CHECK VISUAL INSPECTION FOUND 58 INCHES CORRODED AREA BS 294.5-344 RBBL 58.  REPAIRED PER SRM 51-10-02/51-20-2.  (W)


REMARKS:
INT- DURING Q-4 CHECK VISUAL INSPECTION FOUND 1 INCH CORROSION TOP SILL ANGLE 100 PERCENT GONE.  Z-ANGLE LT ENTRY DOOR BS 312-BS 340.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT- DURING Q-4 CHECK VISUAL INSPECTION FOUND 1 INCH BY 3 INCHES OF CORROSION BS 767- BS 795 RT SIDE RT BL24.  REPAIREDPER SRM 51-10-02.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH AREA CORRODED, SCREW HOLES CORRODED AT FLOOR SUPPORT, BS 991 36 INCHES LBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 5 INCH CORROSION BS 520 BETWEEN S 27R AND 28R.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.   REPAIRED PER SRM 51-30-1.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 4 INCH CORRODED AREA, BS 787 BETWEEN S 27L AND S 27R.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 6 INCH CORROSION, BS 360 BETWEEN S 28L AND S 27R.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-4, FIGURE 11.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 7 INCH CORRODED AREA S 27L FORE AND AFT OF BS 947.5.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.   REPAIRED PER SRM 53-10-3, FIGURE 1.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 4 INCH CORROSION AREA, S 21L APPROXIMATELY STA 905.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-01.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 5 INCH CORRODED AREA S 27R FORE AND AFT OF BS 907.  CORROSIONTASK NR C53-208-01, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-01.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A .5 INCH BY 1 INCH CORRODED AREA, TOP OF FLOOR BEAM BS 986.5 4 INCHES LBL.  CORROSION TASK NR C53-207-02, CORROSION LEVEL 2.   REPAIRED PER TR 53-10-5B.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH CORRODED AREA, SCREW HOLE CORRODED ON FLOOR BEAM BS 986.5 14 INCHES RBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER TP 53-10-05B.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH SCREW HOLES AS CORROSION.  INTERCOSTAL BETWEEN BS 967-986.5 17 INCHES RBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A .5 INCH BY 1 INCH AREA CORRODED, FLOOR BEAM BS 1006 9 INCHES LBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER TR 53-10-05B.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH AREA 2 PLACES CORRODED, FLOOR SUPPORT BS 994-1006 14 INCHES LBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER SRM 51-30-2.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH AREA CORRODED, SCREW HOLE CORRODED FLOOR BEAM BS 1016 6 INCHES LBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 2 INCH AREA CORRODED, FLOOR SUPPORT SB 1016 28 INCHES LBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-06.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 2 INCH AREA CORRODED, FLOOR SUPPORT SCREW HOLES ON BOTTOM SIDE OF FLOOR SUPPORT BS 1006-1016 17 INCHES LBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-06.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH AREA CORRODED, SCREW HOLE, FLOOR BEAM SCREW HOLE BS 1016 5 INCHES RBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-09.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 1 INCH SEVERAL AREAS OF Z-ANGLE HAS CORROSION TOP OF Z-ANGLE SCREW HOLES AND EDGES AFT ENTRY.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A .5 INCH BY 3 INCH AREA CORRODED, FORWARD WALL SUPPORT FOR LAVATORY BS 994 14 INCHES LBL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-30-2.  (W)


REMARKS:
INT- DURING Q-6 CHECK VISUAL INSPECTION FOUND A 1 INCH BY 3 INCH AREA CORRODED, STA 727 A BETWEEN S 26R AND S 27R.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
GSO - FLT 389 - FLT EN ROUTE IAH TO CLT WHEN FIRST OFFICER'S WINDSHIELD CRACKED FLIGHT DIVERTED TO GSO AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED R1 WINDOW, OPS CHECK GOOD.  (W)


REMARKS:
CLT - FLT 334 - THE AFT AISLE EMERGENCY LIGHTS REMAINED ON AT THE GATE.  MAINTENANCE REPAIRED THE WIRE LEADING TO THE BATTERY PACK IN THE AFT LAVATORY.  (W)


REMARKS:
MSY - FLT 55 - THE AFT SERVICE DOOR EMERGENCY CHUTE DEPLOYED.  MAINTENANCE FERRIED MSY TO LGA.  MAINTENANCE REPLACED THE L-2 DOOR EMERGENCY ESCAPE SLIDE.  (X)


REMARKS:
CLT - FLT 1256 - AFTER TAKEOFF, NOSE GEAR WOULD NOT TOTALLY RETRACT.  THE CREW RECYCLED THE GEAR AND NEVER COULD GET THE UNSAFE LIGHT TO EXTINGUISH.  THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NLGUPLOCK SENSOR AND ADJUSTED PER MM., LUBED HINGE FITTINGS AND TORQUE LINKS, PERFORMED GEAR SWING SEVERAL TIMES AND OPS NORMAL.  OKAY FOR SERVICE.  (X)


REMARKS:
CLT - FLT 905 - ON TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT.  THE CREW RECYCLED THE GEAR AND STILL WOULD NOT RETRACT.  THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE SERVICED NOSE STRUT WITH AIR AND OIL AND REPLACED THE SCHRADER VALVE.  OPERATION NORMAL AND LEAK CHECKED GOOD.  (X)


REMARKS:
PIT - FLT 1488 - ON TAKEOFF, THE NR 2 GYRO FLAG CAME IN VIEW AND AUTOPILOT WOULD NOT ENGAGE.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 2 VERTICAL GYRO.  SYSTEM OPERATION TEST NORMAL.  (X)


REMARKS:
PIT - FLT 505 - AFTER TAKEOFF, CREW NOTICED AN AIRFRAME VIBRATION AND ALSO ENCOUNTERED A PRESSURIZATION PROBLEM.  THE FLIGHT RETURNED TO JAX AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND FORWARD CARGO DOOR OPEN.  CHECKED OPERATION OF THE DOOR AND OPS CHECK NORMAL.  CHECKED MASTER CAUTION PANEL AND FOUND FORWARD CARGO DOOR LIGHT INOPERATIVE.  MAINTENANCE RELAMPED LIGHT AND OPS CHECK GOOD.  (X)


REMARKS:
PHL - FLT 572 - ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT.  THE CREW RECYCLED THE GEAR AND STILL WOULD NOT RETRACT.  THE FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPACKED THE NOSE STRUT.  WITH THE AIRCRAFT JACKED, NOSE GEAR OPERATED NORMALLY AND ALL INDICATIONS NORMAL.   OKAY FOR SERVICE.  (X)


REMARKS:
MCO - FLT 460 - AFTER TAKEOFF, UNABLE TO PRESSURIZE AIRCRAFT PROPERLY.  THE FLIGHT RETURNED TO MCO AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND BLOWN DUCT-A, THE RIGHT AIR CYCLE MACHINE, AND INSTALLED THE DUCT WITH NEW CLAMPS.  PRESSURIZED IN AUTO AND MANUAL TO 6 PSI.  OPS CHECK OKAY.  (X).


REMARKS:
MIA - FLT 1996 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT.  MAINTENANCE OPS CHECKED PRESSURIZATION SYSTEM.  LEAK CHECKED DOORS AND SLIDING WINDOWS.  NO DEFECTS FOUND.  (X)


REMARKS:
CLT - FLT 1008 - RIGHT WING BODY OVERHEAT LIGHT CAME ON AFTER TAKEOFF.  LIGHT STAYED ON AFTER ISOLATING RIGHT SIDE BLEED AIR.  FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED OVERHEAT MODULE.  (X)


REMARKS:
DCA - FLT 527 - AFTER TAKEOFF UPON GEAR RETRACTION, MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED SIMULTANEOUSLY.  RECYCLED HANDLE SEVERAL TIMES AND ALL LIGHTS EXTINGUISHED.  FLIGHT RETURNED TO DCA AND LANDED WITOUT INCIDENT.  MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR, NO DEFECTS NOTED.  REPLACED INDICATION LOGIC CARD AS A PRECAUTION.  AIRCRAFT OKAY FOR SERVICE.  (X)


REMARKS:
AIRCRAFT TAIL CONE DAMAGED BY GROUND EQUIPMENT.  REPLACED TAIL CONE AND REPAIRED DAMAGED AREA PER SWA RA 1-253-1073.


REMARKS:
AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED A CHECK, FOUND RIGHT WING LEADING EDGE SKIN TORN AT NUMBER 5 L/E SLAT INBOARD AUX TRACK CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 459-471, ABOVE STRINGER 16L.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 360-371, BETWEEN STRINGERS 4 AND 5L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAMS CORRODED AT FASTENER HOLES, BS 986.5, LBL 14.5, RBL 19.5, 39, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND SWA RA 1-353-542.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 791, STRINGER 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500A, STRINGER 22L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 996, 1002, AND 1008, ABOVE STRINGER 14L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING STRUCTURAL INTEGRITY PROGRAM VISIT ACCOMPLISHED SIP 55-30-01 AND DISCOVERED 2 INCH CRACK LT SIDE VERTICAL STABILIZER TO EMPENNAGE CONNECTION ANGLE.  VISUAL INSPECTION.  REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 55-31-00.  (W)


REMARKS:
CLT - FLT 1928 - GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO.  CYCLED GEAR, FLIGHT CONTINUED TO CLT AND LANDED WITH 3GREEN LIGHTS.  MAINTENANCE FOUND NOSE GEAR LOCK PIN INSTALLED IN NOSE GEAR.  REMOVED PIN.  (W)


REMARKS:
BWI - FLT 1660 - AIRCRAFT LOST RT MAIN OUTBD WHEEL ASSEMBLY ON TAKEOFF.  FLIGHT RETURNED TO BWI AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 3 AND NR 4 MAIN WHEEL, NR 4 BRAKE ASSEMBLY, ANTI-SKID TRANSDUCER, AND LOWER GEAR WIRE HARNESS.  (W)


REMARKS:
IND - FLT 164 - AFTER TAKEOFF, THE RT MAIN GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH.  THE CREW RECYCLED THE GEAR.  THE FLIGHT RETURNED TO IND AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE CLEANED AND LUBED THE RT MAIN GEAR DOOR LATCH.  RECHECKED GEAR RETRACTION AND OPS CHECK NORMAL PER MM 32-60-0, PAGE 201.  (W)


REMARKS:
PHL - THE FIRST 4-5 ROWS OF FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE.  MAINTENANCE REPLACED THE FUSE.  OPS CHECK GOOD.  (W)


REMARKS:
ALB - DURING MAINTENANCE INSPECTION, LT WING ILLUMINATION EMERGENCY EXIT LIGHT ASSEMBLY HAS AN INTERNAL SHORT WHICH CAUSED THE BATTERY TO DRAIN.  MAINTENANCE REPLACED THE LIGHT ASSEMBLY.  (W)


REMARKS:
CLT - FLT 1419 - AFTER FLAP EXTENSION, A-HYDRAULIC SYSTEM FLUID QUANTITY DROPPED INTO THE RED.  CAPTAIN RETURNED TO CLTAND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND A SYSTEM PRESSURE LINE LEAKING.  REPLACED LINE.  RAN ENGINE, OPS AND LEAK CHECK GOOD.  (W)


REMARKS:
CLT - FLT 0196 - THE SQUIB FOR THE RT SLIDE ON TEST ONE AND THE SPOILER FOR THE LT SLIDE ON TEST TWO WOULD NOT TEST.  MAINTENANCE REPLACED BOTH OVERWING BATTERY PACKS, OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
PIT - FLT 2920 - DURING FLIGHT, THE RT GENERATOR DROPPED OFF LINE AND AC CROSSTIE LOCKOUT OCCURRED.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE RESET CROSS-TIE, RAN BOTH ENGINES AND DID CROSS-TIE CHECK SEVERAL TIMES.  VOLTS AND FREQUENCY NORMAL.  OPS CHECK NORMAL.  (W)


REMARKS:
IND - FLT 131 - AFTER TAKEOFF, THE CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AND NOTICED THE E/E COMPARTMENT DOOR LIGHT ILLUMINATED.  MAINTENANCE CLEANED AND LUBRICATED THE E/E COMPARTMENT DOOR SWITCH.  OPS CHECK NORMAL AND RETURNED AIRCRAFT TO SERVICE.  (W)


REMARKS:
PIT - FLT 1500 - ON THREE CONSECUTIVE APPROACHES INTO DCA, THE CREW LOST ALL NAV SIGNALS ON THE CAPTAIN'S INSTRUMENTS AND INTERMITTENT ON THE FIRST OFFICER'S.  THE FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE FIRST OFFICER'S VOR/ILS RECEIVER.  GROUND OPS TEST NORMAL.  (W)


REMARKS:
PIT - FLT 0023 - AT DEPARTURE TIME, CATERING FOUND THE EMERGENCY SLIDE AT DOOR R4 OUT OF THE HOUSING.  MAINTENANCE FOUND THE BAR LOCK MECHANISM TO BE MISSING.  THE BAR LOCK WAS INSTALLED AND THE SLIDE ASSEMBLY SECURED.  OPERATION OF THE GIRT BAR CHECKED NORMAL.  (W)


REMARKS:
PHL - FLT 214 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT ATTENDANT'S ADVISED CREW OF A LOUD AIR NOISE FROM L1 DOOR.  FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND FORWARD ENTRY DOOR NOT CLOSED PROPERLY. RECLOSED DOOR.  OPERATED SEVERAL TIMES, OK FOR SERVICE.  (W)


REMARKS:
PIT - FLT 577 - FLIGHT EN ROUTE LGA TO MCI WHEN LOST ALL PRESSURE IN THE FLIGHT DECK OXYGEN SYSTEM.  FLIGHT DIVERTED TOPIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED CAPTAIN'S AND FIRST OFFICER'S OXYGEN MASK AS PRECAUTIONARY.  REPLACED CREW OXYGEN BOTTLE.  (W)


REMARKS:
TPA - DURING INSPECTION, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN CENTER SECTION.  MAINTENANCE FOUND SHORTED WIRE IN FLOOR TRACK.  REPAIRED BAD PIN AT BATTERY PACK.  (W)


REMARKS:
PIT - FLT 281 - ON APPROACH PIT, NO GEAR TRANSIT LIGHTS OR DOWN INDICATIONS.  CYCLED GEAR AND USED EMERGENCY EXTENSION HANDLE.  VISUALLY VERIFIED GEAR DOWN AND LOCKED.  LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND GEAR INDICATION LIGHTS CIRCUIT BREAKER POPPED.  RESET CIRCUIT BREAKER, CHECKED OK.  (W)


REMARKS:
BWI - FLT 1440 - AIRCRAFT DEPARTED WITH NR 2 ENGINE B-LOOP AND NR 1 ENGINE A-LOOP ON MEL.  ON CLIMB-OUT, FAULT LIGHT ONFIRE CONTROL PANEL CAME ON INTERMITTENTLY.  FLIGHT RETURNED TO BWI AND LANDED WITHOUT INCIDENT.  MAINTENANCE TESTED SYSTEM NUMEROUS TIMES, COULD NOT DUPLICATE PROBLEM.  SYSTEM OK FOR SERVICE.  (W)


REMARKS:
DEN - FLT 3 - FLIGHT EN ROUTE LAX TO MCI WHEN OUTER PANE ON CAPTAIN'S WINDSHIELD CRACKED.  FLIGHT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED CAPTAIN'S WINDSHIELD PER MM 56-11-11.  (W)


REMARKS:
BOS - FLT 1446 - AFTER TAKEOFF, THE NOSE WHEEL RED LIGHT REMAINED ON.  THE CREW RECYCLED THE GEAR AND GOT THE SAME INDICATION.  THE FLIGHT RETURNED TO BOS AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE TIGHTENED THE LOOSE SPRAY DEFLECTOR BOLTS.  JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES SUCCESSFULLY.  OPS CHECK OKAY.  (W)


REMARKS:
EWR - FLT 7024 - AFTER TAKEOFF, LOST THE RT GENERATOR AND ALSO HAD AC CROSS-TIE RELAY LOCK-OUT.  THE APU WAS ON MEL.  THE FLIGHT DIVERTED TO EWR AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE RT AC GENERATOR.  SYSTEM CHECKSGOOD.  (W)


REMARKS:
INT - DURING 'DROP-IN' CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK BS 178 RBL 5.7 AND WL 220.  REPAIRED PER EA 36537. (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND A 1 INCH CRACK AT STA 160 LONGERON 2L.  REPLACED LONGERON AND SPLICED PER SRM 53-02, FIGURE 2.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND A .75 INCH CRACK AT STA 160 LONGERON 4L.  REPLACED LONGERON AND SPLICED PER SRM 53-02, FIGURE 2.  (W)


REMARKS:
DURING Q-1 INSPECTION FOUND .5 INCH CRACK STA 718 LONGERON 5R.  REPLACED LONGERON AND SPLICED PER SRM 53-02 FIGURE 2.  (W)


REMARKS:
DURING Q-1 INSPECTION FOUND 2 CRACKS 2 INCHES AT STA 996 AFT PRESSURE BULKHEAD UPPER LT CORNER.  INSTALLED REPAIR KIT 503 PER EO 5390 D152 CONDITION IV.  (W)


REMARKS:
DURING Q-1 INSPECTION ACCOMPLISHING CARD J9-46-25700-C CORROSION TASK C46-53302 FOUND LEVEL 2 CORROSION AT CUSP MEMBRANE OF SERVICE DOOR STA 160-207.  REMOVED CORRODED AREA AND INSTALLED DOUBLER AND SPLICES PER SRM 53-05 FIGURE 55.  (W)


REMARKS:
DURING Q-1 INSPECTION ACCOMPLISHING CARD J9-48-52701-C CORROSION TASK C58-5330, FOUND LEVEL 2 CORROSION TO STA 996 LONGERON 18L CUSP ANGLE.  MFG REPAIR AND SPLICED PER SRM 53-05 FIGURE 25, EA 25111.  (W)


REMARKS:
DURING Q-1 INSPECTION ACCOMPLISHING CARD J9-58-38701-C CORROSION TASK C58-53300, FOUND LEVEL 2 CORROSION AT STA 980 FLOOR BEAM SCREW HOLES AND NUT PLATES.  TRIMMED OUT CORRODED AREA AND INSTALLED REPAIR ANGLES AND STRAPS PER TYPICAL REPAIR53-10-19.  (W)


REMARKS:
DURING Q-1 INSPECTION, 1.25 INCH CRACK AT RT PYLON STA 1019 ANGLE VISUAL INSPECTION.  INSTALLED REPAIR ANGLE PER SRM 54-04, FIGURE 10 AND EA 25100.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND 2 INCH CRACK AT STA 965 BULKHEAD LOWER OUTBD CORNER VISUAL INSPECTION.  MFG NEW REPAIR WEBAND INSTALLED PER SRM 53-03, FIGURE 21.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND 3 INCH CRACK AT AFT FUSELAGE STA 1038 BULKHEAD IN WEB LT SIDE NEAR LONGERON 9L, VISUAL INSPECTION.  INSTALLED DOUBLER AND SHIMMED PER SRM 53-01, FIGURE 2, SHEET 3.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND .5 INCH CRACK ON HORIZ FORMER Z=34.0 BULKHEAD STA 996 LONGERON 14L AND 15L.  VISUAL INSPECTION.  REPLACED FORMER AND INSTALLED CLIPS PER EA 25218.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND A 2.3 INCH CRACK IN CANTED FRAME STA 1074 AT LONGERON 6L.  INSTALLED TEMPORARY REPAIR PER SRM 53-03, FIGURE 30 SECT K-K SHT-4.  (W)


REMARKS:
DURING STRUCTURAL INTEGRITY INSPECTION ACCOMPLISHED SIP 53-10-03 DISCOVERED A .5 INCH CRACK REAR PRESSURE BULKHEAD AT BL 1050 BEAM 1.  EDDY CURRENT INSPECTION.  REMOVED CRACKED BEAM AND REPLACED PER EA25022A.  (W)


REMARKS:
DURING STRUCTURAL INTEGRITY INSPECTION, ACCOMPLISHED SIP 53-10-05 DISCOVERED 3 INCH CRACK IN FORWARD PRESSURE BULKHEAD AT HORIZONTAL BEAM NR 7, VERIFIED WITH HFEC INSPECTION.  STOP DRILLED CRACK ENDS AND INSTALLED A DOUBLER PER EA NR 25147A.  (W)


REMARKS:
DURING STRUCTURAL INTEGRITY INSPECTION VISIT ACCOMPLISHED SIP 53-10-05 DISCOVERED A 4 INCH CRACK FORWARD PRESSURE BULKHEAD BELOW FLOOR RT SIDE BEAMNR 3.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER EA25164.  (W)


REMARKS:
DURING STRUCTUAL INTEGRITY INSPECTION, ACCOMPLISHED SIP 53-10-19 AND 2 EACH 3 INCH CRACKS ON THE AUX FRAME INSIDE THE NLF WHEEL WELL AT STA 2650 ABOVE NOSE TIRE BRAKE PAD MOUNTS.  VISUAL INSPECTION.  REMOVED DAMAGED AREA AND INSTALLED FILLERS AND DOUBLER PER EA 25233.  (W)


REMARKS:
DURING STRUCTURAL INTEGRITY INSPECTION VISIT, ACCOMPLISHED SIP 53-10-18 DISCOVERED A 1 INCH CRACK IN THE LT NR 3 WINDOWPOST AFT HORIZONTAL FLANGE.  HFEC INSPECTION.  REMOVED AND REPLACED FITTING AT CRACK LOCATION PER EA 25135.  (W)


REMARKS:
DURING STRUCTUAL INTEGRITY PROGRAM VISIT ACCOMPLISHED SIP 55-30-01 AND DISCOVERED A 2 INCH CRACK IN THE RT VERTICAL INSPECTION VERIFIED BY DYE PENETRANT.  REMOVED THE DAMAGED AREA AND INSTALLED A FILLER AND DOUBLER PER SRM 55-31-00.  (W)


REMARKS:
DURING Q-4 INSPECTION ACCOMPLISHED SID CARD NR 9-58-53702 FOUND LT SIDE FLOOR BEAM BROKEN APPROXIMATELY 6 INCHES INBD OF FUSELAGE SKIN AT STA 680.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIGURE 47.  (W)


REMARKS:
DURING Q-4 INSPECTION, FOUND A .25 INCH HOLE IN FUSELAGE SKIN CHAFED THROUGH BY AFT END OF RT PYLON TRAILING EDGE AT STA 1087.  INSTALLED DOUBLER TYPE REPAIR PER SRM 53-04 FIGURE2.  (W)


REMARKS:
DURING Q-4 INSPECTION, FOUND A .1875 INCH CRACK IN SKIN AT FASTENER, AFT LOWER CORNER OF FORWARD STAIR DOOR CUTOUT.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIGURE 57A.  (W)


REMARKS:
DURING Q-4 INSPECTION, FOUND NOSE WHEEL WELL CEILING PANEL 2 INCH CRACK INBD OF NOSE GEAR ACTUATOR ATTACH BRACKET.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIGURE 19.  (W)


REMARKS:
DURING Q-4 INSPECTION, DISCOVERED A 1 INCH CRACK IN THE LT NOSE GEAR TRUNNION A-FRAME AT AFT LOWER SIDE.  REPLACED TRUNNION A-FRAME ASSEMBLY PER STANDARD PRACTICE.  (W)


REMARKS:
DURING Q-4 INSPECTION, ACCOMPLISHING SID PSE 53-09-029 FOUND 2 EA .25 INCH CRACKS AT STA 83 BETWEEN LONGERON L2 AND L3 AT RIVET HEADS (SKIN).  INSTALLED DOUBLER REPAIR PER SRM 53-04, FIGURE 38.  (W)


REMARKS:
EMERGENCY FLOOR TRACK LIGHTS INOP AT ROWS 10 TO 12 AND 15 TO 16.  REPLACED AND TESTED LIGHTS PER BOEING M/M.


REMARKS:
AFT GALLEY EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
IN CRUISE, CAPTAIN'S NUMBER 1 WINDSHIELD CRACKED.  AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND REPLACED WINDOW ASSEMBLY PER BOEING M/M.


REMARKS:
FLIGHT 646, FOUND CABIN EMERGENCY TRACK LIGHTING INOPERATIVE AT FORWARD AND MID CABIN AREAS.  REMOVED AND REPLACED BATTERY PACKS PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION CORNER FITTING CRACKED.  REMOVED AND REPLACED FITTING PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 320, BETWEEN STRINGERS 20R AND 21R.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 992, RBL 45-59, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT GALLEY FLOOR TRACK CORRODED FROM BS 947 TO 1016, RBL 40, WL 208.  REPLACED TRACK PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT FUSELAGE SKIN DENTS AT BS 484, BETWEEN S24L AND S25L, BS 328, BETWEEN STRINGERS 24AND 25L AND AT BS 811 ABOVE S17R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 312, LBL 17 AND 12.  REPAIRED PER TRAMCO EWO 94-0166 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CRACKED AT BS 1136, STRINGER 13L.  REPLACED STRINGER TIE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD SERVICE DOOR, LOWER CORNER CLIP ANGLE CRACKED AT FLOOR LEVEL.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD SERVICE DOOR FRAME WEB ATTACH ANGLE CRACKED, BS 294, WL 240.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD SERVICE DOOR FRAME CRACKED AT UPPER FORWARD STOP.  REPLACED FRAME PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND MLG WHEEL WELL STRINGER 18A SHEAR BEAM CRACKED.  REPLACED FRAME PER BOEING SERVICE BULLETIN 737-53-1066R2.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD ENTRY DOORWAY STRINGER FLANGE CRACKED AT BS 296, S10L.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD ENTRY DOORWAY WEB CRACKED AT BS 296, S12L.  REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND L ANGLE CRACKED AT FLOOR BEAM BELT FRAME AREA AT BS 294, BBL 53R.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND Z ANGLE DOUBLER STRAP CORRODED AT BS 294.5, BBL 52R.  REPLACED DOUBLER STRAP PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 328, BBL 21R.  REPAIRED PER SWA RA 1-353-1059.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, BBL 21L.  REPAIRED PER SWA RA 1-353-1056.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, BBL 8L.  REPAIRED PER SWA RA 1-353-1057.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 294.5, BBL 43R.  REPAIRED PER SWA RA 1-353-1058.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND INTERCOSTAL WEB UPPER ANGLE NUTPLATE HOLES CRACKED AT BS 927 AND 947.5.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD ENTRY DOORWAY SHEAR TIE WEB ATTACH ANGLE VERTICAL FLANGE CRACKED.  REPLACEDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM T-CAP CORROSION AT BS 986, LBL 3.0, 25 35, RBL 5, 14, 28, 30, 32, 34, 36, 38, 40, AND 43.  REPLACED T-CAP PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 664, S10R AND S10L.  REPLACED CLIP PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 918, AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO SAT AND MADE AN UNEVENTFUL LANDING.  ADJUSTED AIR/GROUND SENSOR TARGET AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
PIT - FLT 89 - DURING FLIGHT, THE NR 1 BLEED DUCT LEAK WOULD NOT RESET.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE RESET BAY OVERTEMP INDICATOR.  BLEED AND OPS CHECKS NORMAL.  (W)


REMARKS:
PIT - FLT 1786 - DURING CLIMB-OUT CREW GOT 'GND/FLT CONTROL' AND 'STALL CMPTR WARNING' ON MFDU.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED AIR/GND RELAYS.  ALL CHECKS NORMAL.  (W)


REMARKS:
PIT - FLT 1441 - ON TAKEOFF 'GND/FLT CONTROL' AND 'STALL CMPTR WARNING' ANNUNCIATED WHEN STAB TRIM WENT OUT OF GREEN BAND.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED LT NR 1 AND NR 3 PROX SENSORS ON LT MLG.  AIRCRAFT INDICATION NORMAL.  (W)


REMARKS:
PIT - FLT 1139 - AFTER GEAR RETRACTION THE 'GRD/FLT CONTROL' ALERT CAME ON INTERMITTENTLY.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE ADJUSTED RT NR 2 GND FLT PROX SENSOR PER MM.  OPERATION CHECKS GOOD.  (W)


REMARKS:
PIT - FLT 512 - RT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE ON EXTENSION.  CYCLED GEAR.  ON SECOND EXTENSION, GREEN LIGHT ILLUMINATED.  MAINTENANCE REPLACED RT GEAR DOWNLOCK ACTUATOR PER MM 32-32-16.  OPS CHECKS GOOD.  (W)


REMARKS:
SYR - FLT 409 - CREW GOT THREE GEAR GREEN LIGHTS BUT 'LDG DOWNLOCK SW' ON MFDU.  GEAR UNSAFE WARNING APPEARED.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE CLEANED AND INSPECTED PRIMARY DOWNLOCK SWITCH.  OPS CHECKS GOOD.  (W)


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND NUMBER 1 ENGINE PYLON PANEL CUTOUT CRACKED OUTBOARD AFT SIDE.  REPAIRED PER SWA ACO6135-54.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND LEFT WHEEL WELL STRINGER 18A CRACKED.  REPAIRED PER SWA RA 1-353-1074.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, 10R AND 10L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CRACKED IN UPPER FLANGE RADIUS AT BS 520.  REPAIRED PER SWA ACO 3198-53.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER UPPER FLANGE CRACKED FWD OF FWD ENTRY DOORWAY CUTOUT BS 296.  REPAIRED  PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOORWAY Z-ANGLE CRACKED AT BS 294.  REPLACED ANGLE PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOORWAY BELTFRAME ANGLE CRACKED AT LOWER INBOARD CORNER, BS 294.5.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOORWAY ANGLE CRACKED BELOW S12R, FWD OF NUMBER 4 DOORSTOP, BS 291.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOORWAY, FORWARD FRAME CRACKED AT UPPER DOORSTOP FITTING, BS 294.5.  REPLACED FRAME PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT FRAME INBOARD CHORD LEG CRACKED AT BS 616.  REPAIRED PER SWA RA 1-353-1072.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND LEFT FRAME INBOARD CHORD LEG CRACKED AT BS 616.  REPAIRED PER SWA RA 1-353-1071.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM Z ANGLE CORRODED AT BS 294.5.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM T-CAP CORROSION AT BS 328, RBL 15, 21.5, 28.75, 35.5, 42.5, 49.5, AND 58.25.  REPLACED PER SWA RA 1-353-424 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND RIGHT SIDE BULKHEAD CRACKED FOUR PLACES, AT BS 178, WL 234.  REPAIRED PER SWA RA 1-253-1077.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND STRINGER 26L CORRODED AT BS 967.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND STRINGER 18R CRACKED AT BS 727A.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CABIN EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 12 TO 14.  RECONNECTED WIRE AT ROW 14 PER BOEING M/M.


REMARKS:
ROA - FLT 319 - NR 2 GENERATOR DROPPED OFF LINE AND CREW DETECTED SMOKE IN COCKPIT.  CREW DECLARED AN EMERGENCY AND RETURNED TO ROA WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED RIGHT GCU.  (Z)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 3 INCH AREA OF SURFACE CORROSION.  STRINGER 28R(KEEL BEAM) OUTBOARD FLANGE AT STATION 500D.  REPAIRED PER EA 36823A.  (Z)


REMARKS:
DURING CX-1 INSPECTION, FOUND MULTIPLE WIRES ON 6 STRANDS OF CONTROL CABLE BROKEN ON LT AILERON RETURN CONTROL CABLE OUTBRD OF AILERON SECTOR MECHANISM.  FURTHER INSPECTION REVEALED CABLE ROUTED OVER PULLEY GUIDE PIN.  REMOVED AND REPLACEDCONTROL CABLE, RIGGED PER DC-9 MM 27-10-10, TEMP REV. 27-437, PARA 3D, OPERATIONAL CHECK OKAY.  (X)


REMARKS:
CLT - FLT 2705 - ON APPROACH, LT THROTTLE BECAME NONFUNCTIONAL.  THE CREW SHUT DOWN LT ENGINE FOR LANDING.  MAINTENANCEREPLACED ROD END ON THE PUSH/PULL CABLE.  RIGGED AND OPS CHECK OKAY PER MM.  (X)


REMARKS:
PIT - FLT 1505 - APU SHUT DOWN AND WOULD NOT RESTART.  FLIGHT RETURNED TO PIT DUE TO THE GENERATOR BEING ON MEL AND LANDED WITHOUT INCIDENT.  (W)


REMARKS:
PHL - FLT 731 - A LOUD BANG OCCURRED IN CLIMB-OUT OF PHL.  PASSENGER REPORTED A FLAME SHOT OUT OF THE NR 2 ENGINE.  FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT.  MAINTENANCE RAN RT ENGINE AND COULD NOT DUPLICATE PROBLEM.  INSPECTED AND RAN RT PACK, ALL CHECKED OK.  SUSPECT MINUTE ICE INGESTION IN RT PACK WHICH MIGHT CAUSE THE NOISE.  (W)


REMARKS:
IND - FLT 1732 - ON APPROACH TO SBN, THE CREW WAS UNABLE TO EXTEND THE LANDING GEAR AND UNABLE TO EXTEND OR RETRACT THEFLAPS.  THE FLIGHT DIVERTED TO IND AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND LOWEST POTABLE WATER LINES OVER CENTER SECTION AND REAR BIN BROKEN.  REPLACED BROKEN LINES.  REMOVED ALL ICE AND WATER, REPLACED RT MAIN LANDING GEAR DOOR AND CHECKED GEAR OPERATION.  OPS CHECKED SLATS, FLAPS, ENGINE REVERSE AND BRAKES FOR NORMAL OPERATION.  OPS CHECKED OKAY AND RETURNED THE AIRCRAFT TO SERVICE.  (W)


REMARKS:
CLT - DURING SHOP FUNCTIONAL TEST OF A 727 LIFE RAFT, MPN R0202A203, THE TWO AIR CYLINDERS TESTED FAILED TO PRODUCE SUFFICIENT AIR FLOW TO OPERATE THE RAFT ASPERATORS.  SHOP TEST OF ELEVEN ADDITIONAL CYLINDERS FOUND NINE ADDITIONAL FAILURES.  CYLINDER FAILURES WERE TRACED TO THE BOTTLE REGULATOR.  ALL UNITS WERE RETURNED TO VENDOR FOR REWORK.


REMARKS:
MCI - FLT 608 - WHILE EN ROUTE LAS-PIT, THE 'A' SYSTEM HYDRAULICS FAILED.  THE FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE TIGHTENED A LEAKING PRESSURE RELIEF VALVE IN THE RIGHT MAIN GEAR.  REPLACED 'A' SYSTEM FILTERS AND NO LEAKS NOTED, CHECKED OK.  (Z)


REMARKS:
MSP - FLT 136 - EN ROUTE PIT TO MSP WHEN RIGHT ENGINE OIL PRESSURE DROPPED TO 20 PSI AND OIL QUANTITY READS ZERO GALLONS.  CREW SHUT DOWN RIGHT ENGINE AND DIVERTED TO MSP WHERE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND AFT BEARINGOIL LINE LEAKING.  RESECURED LINE.  LINE CHECKED OK.  (Z)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM TOP CHORD CRACKED AT BS 663, BL 0, WL 208.  REPAIRED PER TRAMCO EWO 94-0161.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD SERVICE DOOR FORMED ANGLE CORRODED FROM BS 299 TO 335, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A CHECK, FOUND FORWARD ENTRY EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD  AISLE EMERGENCY LIGHT INOP.  REPLACED BATTERY PACK PER BOEINGM/M.


REMARKS:
FOUND MID CABIN OVERHEAD EMERGENCY LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
ON APPROACH ATL, SLAT LIGHT CAME ON THEN OFF ACCOMPANIED BY STICK SHAKER.  SPEED WAS 180 KTS, 5 DEGREE FLAP.  SLAT DISAGREEMENT LIGHT ALSO BLINKED ON AND OFF.  CONDITION REPEATED ITSELF NUMEROUS TIMES.  ACCOMPLISHED ABNORMAL PROCEDURES ANDLANDED WITHOUT INCIDENT.  REMOVED AND REPLACED RT AOA VANE, OPS CHECKED AND CALIBRATED PER MM 34-14-0, CHECKED OK.


REMARKS:
RIC - FLT 464 - ON TAKEOFF AND CLIMB THE LT ENGINE SURGED FROM 100 PERCENT TO 85 PERCENT ON TRUST INDEX.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 1 ENGINE MAIN BLEED VALVE PER MM 36-10.  FUNCTIONAL AND LEAK CHECK SATISFACTORY.  (W)


REMARKS:
STL - FLT 123 - DURING CRUISE RIGHT GALLEY SERVICE DOOR ESCAPE SLIDE LANYARD INADVERTENTLY BECAME ENTANGLED WITH A FOODSERVICE CART AND INFLATED.  THE SLIDE, MFG P/N 7A1274-8, WAS DEFLATED WITH A SHARP OBJECT AND REPLACED.  CHECK C-24 - 1-8-94 - MCI.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND LT WING IWS 555.00 RIB-TO-STRINGER LOWER TIE CLIP BROKEN AT 5 STRINGERS AFT AT TANK ACCESS OPENING.  REPLACED CLIP PER SRM 51-10-01.  AIRCRAFT TT, 54,909 HOURS.  CYCLES, 21,036.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A 2 INCH CRACK IN RADIUS OF LOWER RIB CAP, WS 555, BETWEEN STRINGERS 9 AND 10.  REPLACE CHORD PER EMLR 64313.  AIRCRAFT TT, 62,336 HOURS.  CYCLES, 17,629.


REMARKS:
DURING OP-9, FOUND CRACK IN DOUBLER AT AFT LOWER CORNER OF FORWARD STAIRWELL DOOR.  REPAIRED PER SRM 53-04 FIGURE 57A, 53-05 FIGURE 57A, AND ARA 3208.  AIRCRAFT TT, 63,061 HOURS.  CYCLES, 71,310.


REMARKS:
DURING OP-9 FOUND .50 INCH LONG CRACK IN FUSELAGE SKIN RIGHT OF CENTERLINE, FORWARD OF RIGHT WINDSHIELD WIPER MOTOR, STA 76.55.  INSTALLED REPAIR DOUBLER PER SRM 53-04, FIGURE 12B, PAGE 60G.  AIRCRAFT TT, 60,732 HOURS.  CYCLES, 74,566.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACK APPROXIMATELY .75 INCH LONG IN RT WING LOWER IWS 555 RIB T-CHORD CASTELLATION, AT STRINGERS 9 AND 14.  REPLACED LOWER CORD PER SRM 51-10-01.  AIRCRAFT TT, 60,879 HOURS.  CYCLES 17,100.


REMARKS:
DURING SPECIAL CHECK, FOUND CRACK APPROXIMATELY .75 NCH LONG IN RT WING UPPER IWS 555 RIB T-CHORD CASTELLATION, AT STRINGERS 13, 14, AND 19.  REPLACED UPPER CORD PER SRM 51-10-01.  AIRCRAFT TT,60,879 HOURS.  CYCLES, 17,100.


REMARKS:
MCI - DURING SPECIAL CHECK FOUND .75 INCH CRACK IN LT WING FORWARD FALSE SPAR INBOARD ATTACH ANGLE AT IWS 503.7.  REMOVED AND REPLACED ANGLE PER SRM 51-01-01.  AIRCRAFT TOTAL TIME, 60,879 HOURS.  CYCLES, 17,100.


REMARKS:
DURING SPECIAL CHECK, FOUND A .3750 INCH CRACK IN RT WING UPPER IWS 529.4 RIB T-CHORD, STRINGER 18.  STOP DRILLED CRACKAND REPAIRED PER ARA 7999.  AIRCRAFT TOTAL TIME, 60,879 HOURS.  CYCLES, 17,100.


REMARKS:
DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IIN RT WING UPPER IWS 529.4 RIB T-CHORD, STRINGER 19.  STOP DRILLED CRACKAND REPAIR PER ARA 7999. AIRCRAFT TT, 60,879 HOURS.  CYCLES, 17,100.


REMARKS:
DURING APPROACH, NOSE LANDING GEAR DID NOT INDICATE DOWN UNTIL CYCLED THREE TIMES.  CHECKED PROXIMITY SWITCH CLEARANCES.  JACKED NOSE GEAR, OP CHECKS NORMAL.  CHECK C-1A - 11-26-93 - MCI.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 360-380, ABOVE STRINGER 22R, BS 480, STRINGER 5R, BS 957, STRINGER 19L, BS 467, BETWEEN STRINGERS 16 AND 17R AND AT BS 914 BETWEEN 22 AND 23L.  REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 5R CRACKED AT BS 480, STRINGER.  REPAIRED STRINGER PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND CRACK IN WEB OF NOSE GEAR RETRACT CYLINDER SUPPORT BEAM.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT BS 907, 3 FOOT AFT OF AFT CARGO DOOR.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING CLIMB-OUT, EXPERIENCED BIRDSTRIKE TO FIRST OFFICER'S NUMBER 1 WINDOW, OBSCURING FIRST OFFICER'S VISIBILITY.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  ACCOMPLISHED BIRD STRIKE INSPECTION.  REPLACED DAMAGED WINDSHIELDWIPER ARM AND CLEANED WINDOW, NO OTHER DAMAGE NOTED.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CRACK IN CLIPS ON STRINGER WEB ON BELTFRAME AT BS 294.5, S12L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS  344, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND MID CABIN OVERHEAD EMERGENCY LIGHT BLINKING.  REPLACED BATTERY PACK PER BOEING MAINTENANCE MANUAL.


REMARKS:
DURING AN EMERGENCY EVACUATION, CREW ATTEMPTED TO DEPLOY L-1 EVACUATION SLIDE, SLIDE WOULD NOT DEPLOY AUTOMATICALLY OR MANUALLY.  PASSENGERS EVACUATED VIA R-1 SLIDE.  REMOVED AND REPLACED SLIDE WITH SERVICEABLE SLIDE.  SLIDE WAS REPACKED ON 11/01/93 AND WAS DUE FOR REPACK ON 11/01/96.  SLIDE RETAINED IN VALUJET MAINTENANCE SHOP PENDING DISPOSITION FROM FAA.


REMARKS:
FLT 26 - CRUISE ALTITUDE BETWEEN FLL AND ATL IN THE VACINITY OF MACON, GA.  WITH NO PRIOR INDICATION, THE ENGINE COMPRESSOR STALLED APPROXIMATELY 6 TIMES IN RAPID SUCCESSION.  THROTTLE WAS RETARDED TO IDLE AND THE IDLE ENGIE INDICATION STABILIZED IN THE NORMAL ZONE AND REMAINED STABLE UNTIL AFTER LANDING IN ATL.  THE ENGINE WAS SHUT DOWN WHILE TAXING TO THEGATE.  REPLACED NR 1 ENGINE IAW PRATT AND WHITNEY MM SECTION 71-00 AND VJ WORK CARD SN P657465.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND SEVERAL PLACES CORRODED MORE THAN 15 PERCENT DEEP 1 INCH BY 1 INCH, 1.25INCH BY 1 INCH, 1 INCH BY .5 INCH SUPPORT BEAM FOR CARGO FLOOR BS 727 TO BS 787, LBBL 17.20 INCH.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-70-12, FIGURE 1 AND SRM 53-00-53 PAGE 205.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND SEVERAL PLACES .5 INCH BY 2.5 INCH BY 1 INCH BY .75 INCH CORRODED MORE THAN 15 PERCENT DEEP.  SUPPORT BEAM FOR CARGO FLOOR STA 727 TO STA 880 RBBL 13.80 INCH.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  REPAIRED PER SRM 55-00-53 PAGE 205.  (W)


REMARKS:
GSO - DURING TRANSIT CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 384 BBL ZERO AT EQUIPMENT COOL OUTLET DUCT.  REPAIRED PER EA 25454.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION (APPROXIMATELY 2 INCH BY 40 INCH AREA) AT STA 947 FLOOR BEAM.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-05.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY .050 INCH CORROSION (3 EA) LBL 12 STA 294.5 TO STA 312.  CORROSION TASK NR C-53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 2 INCH BY 12 INCH AREA SURFACE, INTERCOSTAL BS 986.5 LBBL 20 INCHES AND BS 1006 LBBL 9 INCHES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 3 INCHES BY .75 INCH BY .030 INCH, STA 294.5 TO STA 312 RBL 27.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND T-CAP CORROSION 1.25 INCH BY 1.5 INCH BY .018, STA 294.5 LBL 20-28.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-01A.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH AREA CORRODED AROUND FASTENER HOLES, Z-ANGLE BETWEEN BS 294.5 AND BS 313 FORWARD SERVICE DOOR.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG BY 2 INCH WIDE MORE THAN 15 PERCENT DEEP LT AFT ENTRY DOOR S 17L.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH LONG BY 30 INCH CORROSION Z-ANGLE AT RT AFT SERVICE DOOR BS 947 TO BS 986.5.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER 737-300 SRM 51-10-02, PAGE 15.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION .5 INCH BY 8 INCHES AND .5 INCH BY 9 INCHES AT STA 951, LBL 18 AND LBL 42.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL AT LBL 18 STA 967-986.5 .5 INCH BY 6 INCHES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL AT RBL 18 STA 967-986.5 .5 INCH BY 6 INCHES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 8 INCH AREA SURFACE CORRODED, AT BS 947 THROUGHBS 967 LBBL 18 INCHES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
MCO - FLT 322 - ON CLIMB-OUT FROM MIA, RT BLEED TRIPPED AND WOULD NOT RESET.  CLIMBING THROUGH FL 290, CABIN ALT WARNING SOUNDED.  FLIGHT DESCENDED TO FL 250 AND CABIN ALT STABILIZED AT 8500.  FLIGHT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT.  MAINTENANCE PRESSURIZED AIRCRAFT, ALL INDICATIONS NORMAL.  REPLACED LT AIR CYCLE MACHINE.  NO LEAKS NOTED.  (W)


REMARKS:
CLT - FLT 1679 - AFTER TAKEOFF RT PACK TRIPPED.  CREW RESET AND IT TRIPPED AGAIN.  LT PACK WAS ON MEL.  UNABLE TO MAINTAIN PRESSURIZATION.  FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND BOTH HEAT EXCHANGERS DIRTY.PERFORMED HEAT EXCHANGER WASH.  RT PACK OPS NORMAL AFTER WASH.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND APPROXIMATELY 2 INCH BY 10 INCH AREA SURFACE CORROSION.  BS 947 THROUGH BS 967 AT LBBL 42 INCHES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND APPROXIMATELY 2 INCH BY 8 INCH AREA SURFACE CORROSION.  BS 986 RBBL 20 INCHES AND BS 1006 RBBL 9 INCHES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND CORROSION APPROXIMATELY 2 INCH BY 50 INCH AREA SURFACE.  FLOOR BEAM AT STATION 986.5.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-05.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND .5 INCH AREA CORRODED AROUND FASTENERS.  FLOOR BEAM BS 328 RBL 0 THROUGHRBL 58.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-01, REV A.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND CORROSION 1.5 INCHES BY 3 INCHES BY .031 INCH (20 PLACES) STA 967 LBL 6 TO LBL 50.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 53-60-51, FIC 202.  (W)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FORWARD SERVICE DOOR CUTOUT, LOWER AFT CORNER, BS 328, WL 210. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND DENT IN TOP FLANGE OF FRAME AT  BS 787, RBL 27, WL 159.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727, S24R.  REPAIRED PER SWA RA 1-353-890 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED STRUCTURE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727, S24R.  REPAIRED PER SWA RA 1-353-890 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND Z ANGLE CORRODED AT AFT SERVICE DOOR ENTRYWAY FLOOR LEVEL.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND ANGLE ABOVE STRINGER 10L CRACKED AT BS 300.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND ATTACH ANGLE CRACKED AT FLOOR LEVEL, OUTBOARD OF Z CHORD AND BETWEEN BS 294.5 AND FORWARD OF DOOR FRAME WL 200.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE WEB SUPPORT SKIN ATTACH ANGLE CRACKED AT BS 292, S9R.  REPLACED ANGLE PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND OUTBOARD SHEAR TIE WEB TO SKIN ATTACH ANGLE CRACKED AT BS 292, S13R.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM UPPER T-CAP CRACKS AT BS 520, RBL 45.5, 24.75, LBL 45.5, AND 24.75 .  REPAIRED PER SWA ACO 3198-53 AND RA 1-353-1078.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT BS 294.5, S23L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM STABILIZER STRAP CRACKED AT BS 312, RBL 32.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM T-CAP CORROSION AT BS 328, BETWEEN LBL 34 AND RBL 60.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY FLOOR BEAM CORRODED AT BS 967, RBL 5.  REPAIRED PER SWA RA 1-353-1080.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY FLOOR BEAM CORRODED AT BS 986.5, RBL 20.  REPAIRED PER SWA RA 1-353-1085.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND AFT GALLEY FLOOR BEAM CORRODED AT BS 986.5, RBL 21.5, 26.5, AND 30.0.  REPAIRED PERSWA RA 1-353-1084.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND AFT GALLEY FLOOR BEAM CORRODED AT BS 986.5, RBL 23.5, 27.5, 31.5.  REPAIRED PER SWARA 1-353-1085.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY FLOOR BEAM CORRODED AT BS 986.5, LBL 35, 40, AND RBL 31.0.  REPAIRED PERSWA RA 1-353-1083.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, RBL .75.  REPAIRED PER SWA RA 1-353-1086.


REMARKS:
JFK - FLT 185 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, LANDING GEAR RED AND GREEN LIGHTS REMAINED ON.  CYCLED LANDING GEAR AND RED LIGHTS REMAINED ON.  FOUND NOSE LANDING GEAR POSITION SWITCH MFG NR 1HA11 BAD.  REPLACED SWITCH.  LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL.  CHECK C-2 - 1-28-94 - MCI.


REMARKS:
DURING CHECK C-1, FOUND CRACKED NOSE WHEEL WELL AT BS 285.8.  REPAIRED PER SSRM 53-10-211, PAGE 201 USING STANDARD PRACTICES.  AIRCRAFT TT 62,774 HOURS.  CYCLES, 42,874 CYCLES.


REMARKS:
MCI - DURING CHECK C-1 FOUND CRACK AT BS 278.3 AND CENT LINE OF CEILING OF NOSE WHEEL WELL.  REPAIRED PER SSRM 53-10-211, PAGE 201 USING STANDARD PRACTICES.  AIRCRAFT TT 62,774 HOURS.  CYCLES, 42,874.


REMARKS:
DURING CHECK C-1 FOUND 2 CRACKS NG WHEEL WELL APPROXIMATELY 2 INCHES AT BS 245.8, LT SIDE.  REPAIRED PER SSRM 53-10-211, PAGE 201 AND FIGURE 201.  AIRCRAFT TT, 62,774 HOURS.  CYCLES, 42,874.


REMARKS:
DURING CHECK C-1, FOUND 2 CRACKS NG WHEEL WELL APPROXIMATELY 2 INCHES AT BS 243.3, LT SIDE.  REPAIRED PER SSRM 53-10-211, PAGE 201.  AIRCRAFT TT, 62,774.  CYCLES, 42,874.


REMARKS:
PIT - FLT 820 - AFTER TAKEOFF, THE CREW UNABLE TO PRESSURIZE THE AIRCRAFT.  THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND BLOWN DUCT AT RIGHT PACK COOLING TURBINE AND REPLACED THE DUCT AND PRESSURIZED THE AIRCRAFT.  OPS NORMAL.  (Z)


REMARKS:
EWR - FLT 17 - ON PUSH BACK, FOUND BROKEN WIRES ON NOSE GEAR.  ASSIGNED MEL 32-06 030035D AND MEL 33-11 030036-C FOR NOSE GEAR AND TAXI LIGHTS.  REFERENCE CONTROL NR IXKA9400005.  (W)


REMARKS:
ATL - BEFORE TAKEOFF, FLT 48, NR 3 ENGINE EPR GAUGE WENT FULL SCALE.  REMOVED AND REPLACED EPR TRANSMITTER PER MM 77-11-11.  PERFORMED TAKEOFF POWER RUN.  OPS CHECK OK.  (W)


REMARKS:
AT EWR, FLT NR 17, ON PUSH BACK FOUND BROKEN WIRES ON NOSE GEAR BRAKES AND TAXI LIGHTS.  REMOVED AND REPLACED NOSE GEARELECTRICAL HARNESS, OPS CHECK OF NOSE GEAR ANTI-SKID PER 32-42-01.  OPS CHECK OK.  (Z)


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND INTERCOSTAL AND STRINGER  CRACKED AFT SIDE OF FORWARD ENTRY DOOR.  REPLACED STRINGER AND INTERCOSTAL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND A 2 INCH CRACK ON FORGING AT AFT SIDE OF FRAME, BS 727, WL 231.6, LBL 72.  REPAIRED PERTRAMCO EWO 94-0154.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 827, STRINGER 28L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 320, STRINGER 21R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT.  CREW USED OVERRIDE AND GEAR RETRACTED.  AIRCRAFT DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACED LANDING GEAR HANDLE  LATCH SOLENOID AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
RIGHT OVERWING EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
FORWARD CABIN EMERGENCY LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
FOUND BOTH FORWARD ENTRY DOORS EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SPECIAL CHECK, FOUND CRACK INDICATION APPROXIMATELY .5 INCH IN REAR SPAR UPPER CHORD RT WING BAY 8, HOLE 6A, OF HORIZONTAL CHORD FLANGE ZONE 600.  REPAIRED PER ARA 7280.  TOTAL CYCLES 15,885.


REMARKS:
DURING SPECIAL CHECK, FOUND LEFT WING UPPER CHORD AT IWS 555 HAS 8 CRACKS.  REPLACED UPPER CHORD PER ELMR 64314 REV A.TOTAL CYCLES 18,876.


REMARKS:
DURING SPECIAL CHECK, FOUND LEFT WING IWS 555 HAS CRACKED LOWER STRINGER NR 7 TO LOWER T-CHORD ATACH ANGLE.  REPLACED CLIP PER SRM 51-10-05.  TOTAL CYCLES 18,876.


REMARKS:
DURING SPECIAL CHECK, FOUND RT WING IWS 555 UPPER WING T-CHORD HAS 6 CRACKS.  REMOVED AND REPLACED UPPER CHORD PER EMLR64314 REV A.  TOTAL CYCLES 18,876.


REMARKS:
DURING SPECIAL CHECK, FOUND RT WING IWS555 HAS CRACK IN LOWER T-CHORD BETWEEN STRINGERS NR 14 AND NR 15 APPROXIMATELY .6250 INCHES LONG FROM STRINGER 14 CUTOUT INTO RADIUS.  REMOVED AND REPLACED FWD SECTION OF LOWER RIB CHORD PER EMLR 64214 REV A.  TOTAL CYCLES 18,876.


REMARKS:
DURING SPECIAL CHECK, FOUND LEFT WING IWS 55 HAS 2 CRACKS IN LOWER T-CHORD BETWEEN STRINGERS 09 AND 10.  ONE CRACK APPROX 2 INCHES LONG FROM STRINGER 9 CUTOUT THROUGH FASTENER INTO CHORD RADIUS AND 1 FROM CUTOUT APPROX 1 INCH LONG INTO RADIUS CHORD.  INSTALLED LOWER CHORD PER EMLR 64314 REV A.  TOTAL CYCLES 18,876.


REMARKS:
PIT - FLT 0675 - RETURN TO FIELD DUE TO THE EICAS MESSAGE 'FWD CARGO DOOR' AND THE FORWARD CARGO DOOR LIGHT WHICH CAME ON AFTER TAKEOFF.  MAINTENANCE CLEANED THE TARGET AND SENSOR AND CHECKED THE TARGET TO SENSOR ADJUSTMENT.  A PSEU BIT WAS ALSO PERFORMED.  ALL CHECKS WERE FOUND TO BE SATISFACTORY.  (W)


REMARKS:
PIT - FLT 0816 - THE EVACUATION SLIDE SQUIB TEST FAILED.  THE SQUIB DOES NOT TEST WHEN THE PUSH TO TEST BUTTON IS PUSHED.  MAINTENANCE REPLACED THE BATTERY PACK.  OPS CHECKED NORMAL.  (W)


REMARKS:
SDF - FLT 544 - AFTER TAKEOFF, THE NOSE GEAR DOOR LIGHT ILLUMINATED AND UNUSUAL VIBRATION.  THE FLIGHT RETURNED TO SDF AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE LUBED THE NOSE GEAR DOOR AND LATCHES AND DOORS CHECKED NORMAL.  (W)


REMARKS:
CVG - FLT 936 - AFTER TAKEOFF AND UPON GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED.  THE FLIGHT RETURNED TOCVG AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND THE RT NOSE GEAR SPRAY DEFLECTOR'S BOLTS MISSING AND REINSTALLED THE SPRAY DEFLECTORS.  (W)


REMARKS:
CLT - FLT 1175 - DURING SQUIB TEST, THE 2R EMERGENCY ESCAPE SPOILER INDICATOR LIGHT REMAINED EXTINGUISHED.  MAINTENANCEREPLACED THE BATTERY CHARGER AND BATTERY PACK ASSEMBLIES.  OPERATIONS CHECKED GOOD.  REFERENCE USAA940303.


REMARKS:
PIT - FLT 77 - AFTER TAKEOFF CREW GOT A GROUND FLIGHT CONTROL WARNING AND THE GEAR WOULD NOT RETRACT.  CREW HAD TO OVERRIDE THE GEAR.  ALSO, DURING GEAR RETRACTION CREW GOT LIFT DUMPER MESSAGE AND CAUTION LIGHT.  DURING CLIMB, THE STAB TRIM FAULTED AND DURING DESCENT THE CABIN PRESSURE CONTROL FAULTED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE ADJUSTED LT MLG FLT/GRND SWITCHES PER MM.  JACKED AIRCRAFT, ALL INDICATIONS NORMAL.  (Z)


REMARKS:
MSP - FLIGHT 1089 - DURING FLIGHT, FLIGHT ATTENDANT ADVISED CAPTAIN THAT AIR WAS COMING THROUGH PAX MAIN ENTRY DOOR.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPAIRED AND INSPECTED MAIN ENTRY DOOR AND PRESSURIZED AIRCRAFT.  ALL CHECKS NORMAL  (Z)


REMARKS:
GSO - FLT 186 - DURING FLIGHT, THE NR 2 ENGINE ANTI-ICE FAULTED AND WOULD NOT RESET.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE ANTI-ICE VALVE.  OPERATION CHECK NORMAL.  (Z)


REMARKS:
LGA - FLT 1267 - DURING FLIGHT, HYD SYSTEM 2 OVERHEAT ALERTED.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 2 HYD FLUID OVERHEAT TEMP SENSOR.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLT 1159 - LEFT GEAR LIGHT CAME ON IN FLIGHT, NO OTHER ABNORMAL INDICATIONS.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND SOCKET PIN FOR LT GEAR LIGHT BEING SHORTED TO GROUND.  STRAIGHTENED PIN, SWUNG GEAR SEVERAL TIMES.  OPERATIONS CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLT 1294 - AFTER TAKEOFF, RT AFT SMOKE ALARM SOUNDED WHEN SMOKE APPEARED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED LT/RT WATER SEPARATOR BAGS.  OK FOR SERVICE.  (Z)


REMARKS:
PIT - FLT 77 - DURING FLIGHT THE ENGINE NR 1 HYDRAULIC SYSTEM NR 1 ENGINE PUMP FAILED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE ENGINE NR 1 SYSTEM NR 1 HYD PUMP.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
MIA - FLT 302 - AFTER TAKEOFF LEFT PACK TURBINE STARTED SPINNING WITH SEVERE VIBRATION AS AIRCRAFT ACCELERATED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED TURBINE.  OPERATION AND LEAK CHECK OK.  (Z)


REMARKS:
CLT - FLT 1167 - AFTER GEAR RETRACTION, INDICATION SHOWED LT AND RT MAIN GEAR DOWN BUT NOSE GEAR UP.  CYCLED GEAR.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED LT MLG DOOR UP SEQUENCE VALVE PER MM.  OPERATION CHECKS GOOD.  (Z)


REMARKS:
GRR - FLT 225 - DURING FLIGHT, CREW GOT A HIGH ALTITUDE WARNING INDICATION.  OXYGEN MASKS WERE DEPLOYED FOR PASSENGERS AND CREW.  NO EMERGENCY DECLARED.  AIRCRAFT LANDED WITHOUT INCIDENT AT DESTINATION.  MAINTENANCE FOUND TORN MAIN SEAL TOBE THE PROBLEM.  REPLACED THE SAME.  CLEANED AND STOWED OXYGEN MASKS PER MM 35-11 AND PRESSURIZED AIRCRAFT PER MM 21-31.  ALL CHECKS NORMAL.  (Z)


REMARKS:
DURNG Q-4 INSPECTION, FOUND .8750 INCH AND 1 INCH CRACK IN THE AFT RT EMERGENCY EXIT DOOR BENEATH TOP TWO DOOR STOPS.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03.  (Z)


REMARKS:
DURING CX-2 INSPECTION, FOUND TWO EACH .5 INCH CRACKS IN LONGERON NR 5 RIGHT AT FS 756.  LOW FREQUENCY EDDY CURRENT.  SPLICE REPAIR INSTALLED PER SRM 53-02.  (Z)


REMARKS:
DURING Q-CHECK INSPECTION, WHILE ACCOMPLISHING CORROSION CONTROL AND J9-57-53701-C TASK NRC57-53300, FOUND LEVEL 2 CORROSION AT STATION 996 TEE CAP LOWER CENTER JACK PAD AREA.  NO PREVIOUS REWORK ACCOMPLISHED.  INSTALLED REPAIR ANGLE PER USAIR TYPICAL REPAIR 53-30-10.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT, INSPECTION FOUND .3750 INCH CRACK IN RIGHT SIDE LOWER AFT CORNER OF SERVICE DOOR JAMB, FUSELAGE SKIN.  INSTALLED DOUBLER AS PER SRM 53-05, FIG 35.  (Z)


REMARKS:
DURING AGING VISIT, INSPECTION FOUND 5 CRACKS .1250 INCH TO .3750 INCH IN LEFT SIDE NOSE SKIN STATION 69, LONGERON NR 2AND NR 3.  INSTALLED FLUSH TYPE DOUBLER AS PER SR0950239 AND EA 25347.  (Z)


REMARKS:
DUIRNG Q-CHECK INSPECTION, FOUND .75 INCH AND 1 INCH CRACK IN THE VERTICAL STAB 4TH RIB AND 6TH RIB VISUAL WITH LEADINGEDGE REMOVED.  INSTALLED REPAIR ANGLES PER SRM 55-02 FIG 27 AND USAIR EA 25536.  (Z)


REMARKS:
WHILE PERFORMING C-10 CHECK, INSPECTION FOUND CRACK 1 INCH LONG AT STATION 897 LONGERON 29R.  DAMAGED SKIN WAS REMOVED AND FLUSH REPAIR INSTALLED AS PER EA 25764.  (Z)


REMARKS:
WHILE PERFORMING C-10 CHECK, INSPECTION FOUND 2 CRACKS APPROXIMATELY .5 INCH EACH AT STATION 736 BETWEEN L29R AND 29L.DOUBLER WAS INSTALLED AS PER SRM 53-04, FIG 12B, SHEET 11.  (Z)


REMARKS:
IND - FLT 1925 - DURING FLIGHT, THE CAPTAINS FWD WINDOW CRACKED.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE CAPTAINS FWD WINDOW PER MM 56-11-00 AND PER EA 25638.  ALL CHECKS NORMAL.  (Z)


REMARKS:
SFO - FLT 1776 - AT DEPARTURE, CREW REPORTED R1 DOOR SLIDE COULD NOT BE ENGAGED.  MAINTENANCE RERIGGED THE GIRT BAR ANDENGAGE MECHANISM.  THE SYSTEM RETURNED TO NORMAL FUNCTION.  (Z)


REMARKS:
IND - FLT 272 - WHILE EN ROUTE PIT TO MCI, THE RIGHT ENGINE WOULD NOT SPOOL UP WHILE AT CRUISE ALTITUDE.  ENGINE LOST POWER AND WOULD NOT RESPOND TO THROTTLES.  THE CREW SHUTDOWN THE RIGHT ENGINE AND DIVERTED TO IND AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE FUEL CONTROL UNIT PER MM 73-20-01, TRIMMED UNIT TO ENGINE PER JOB CARD JD901, NOLEAKS NOTED AND ALL CHECKED GOOD.  (Z)


REMARKS:
EWR - FLT NR 1740 - AFTER TAKEOFF, THE LANDING GEAR OVERRIDE BOTTOM JAMMED ALL THE WAY IN, MAKING IT UNABLE TO RAISE THE LANDING GEAR.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE INSPECTED LINKAGE AND OPERATING MECHANISM AT GEAR EXTENSION LEVER.  PERFORMED TEST OF OVERRIDE CONTROL SYSTEM.  FOUND NO DEFECTS NOTED AS PER MM 32-31-01. (Z)


REMARKS:
BUF - CENTER CABIN EMERGENCY EXIT LIGHT FELL OFF CEILING.  MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSEMBLY.  (Z)


REMARKS:
PHL - THE EMERGENCY PATHWAY LIGHTS WOULD NOT TEST.  MAINTENANCE REPLACED NINE OUT OF TEN BATTERIES IN THE FLOOR LIGHTING.  (Z)


REMARKS:
P0HL - FLT 1159 - AFTER TAKEOFF, THE TAIL CONE UNSAFE LIGHT ILLUMINATED.  THE FLIGHT RETURNED TO PHL AND LANDED WITHOUTFURTHER INCIDENT.  MAINTENANCE FOUND BALL END OF CABLE NO INSERTED INTO SWITCH ASSEMBLY.  REINSERTED CABLE.  OPS CHECK OF SWITCH AND LIGHT ASSEMBLY NORMAL.  (Z)


REMARKS:
MSY - FLT 1400 - ON TAKEOFF, THE CREW FELT SEVERE VIBRATION IN THE RIGHT MAIN LANDING GEAR.  THE FLIGHT CONTINUED TO CLT.  AT CLT, THE CREW DROPPED THE GEAR AND DID NOT GET THREE GREEN LIGHTS.  THEY DID A FLY-BY THE TOWER AND CONFIRMED GEAR DOWN AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND THE NR 3 MAIN TIRE BLOWN AND REPLACED.  (Z)


REMARKS:
YUL - FLT 954 - ON APPROACH, THE RIGHT MAIN GEAR WOULD NOT GIVE EITHER A RED OR GREEN INDICATION.  THE CREW ATTEMPTED TO CHANGE THE BULBS BUT WERE UNSUCCESSFUL.  THE CREW THEN VISUALLY SIGHTED THE GEAR AND FOUND IT LOCKED AS WELL AS A PRECAUTIONARY FLY-BY THE TOWER.  THE FLIGHT THEN LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND THE RIGHT GEAR INDICATOR LAMPS BURNED OUT.  RELAMPED AND RESET RIGHT GEAR INDICATOR MODULE.  GEAR INDICATION CHECKS NORMAL.  (Z)


REMARKS:
DCA - FLT 56 - ON APPROACH, NO RED OR GREEN LIGHTS ON THE NOSE GEAR.  BOTH INDICATOR LIGHTS WERE CHANGED, HOWEVER, STILL NO GREEN NOSE LANDING LIGHT DURING GEAR WARNING TEST AND LIGHT ILLUMINATION.  UPON FLY-BY, THE GPWS GEAR WARNING SOUNDED.  THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH.  GROUND OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLT 0816 - RETURN TO FIELD DUE TO E/M 'LE SLAT ASYM'.  THE LEADING EDGE LIGHT ILLUMINATED WITH THE FLAP LEVER IN 1.  MAINTENANCE PERFORMED BITE CHECK PER FIM.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
CLT - FLT 1175 - DURING SQUIB TEST, THE 2R EMERGENCY ESCAPE SPOILER INDICATOR LIGHT REMAINED EXTINGUISHED.  MAINTENANCEREPLACED THE BATTERY CHARGER AND BATTERY PACK ASSEMBLIES.  OPERATIONS CHECKED GOOD.  REFERENCE 94ZZZZ580.


REMARKS:
FLOOR BEAM TOP SURFACE CORRODED 20 INCHES IN LENGTH BETWEEN LBL 24.75, LBL 24.75, LBL 45.50, STATION 377.5.  INSTALLED T-CAP AND REPAIR ANGLES.  REPAIR DOC EA 36926.  (Z)


REMARKS:
CENTER LINE OF FLOOR BEAM TOP SURFACE CORRODED 1 INCH BY 3 INCH AND 1 INCH BY 6 INCH AT BODY STATION 324, RBL 55 AND RBL 45 (G 1A GALLEY).  INSTALLED T-CAP REPAIR ANGLES.  REP DOC EA 36935.  (Z)


REMARKS:
YYZ - FLT 1230 - WHILE EN ROUTE ROC-YYZ, THE RIGHT LOW OIL PRESSURE LIGHT ILLUMINATED THE RIGHT OIL QUANTITY GAUGE DROPPED TO ZERO AND THE RIGHT OIL PRESSURE GAUGE 10-15 PSI.  THE CREW DECIDED TO SHUTDOWN THE RIGHT ENGINE AND CONTINUED TO YYZ AND LANDED WITHOUT FURTHER INCIDENT.  FOUND UPPER AFT STUD ON OIL FILTER HOUSING STRIPPED.  MAINTENANCE REPLACED THEHELICOILS AND SEALS.  ENGINE GROUND RUN LEAKED CHECKS OKAY AND MAG PLUG CHECKS OK FOR CONTINUED SERVICE.


REMARKS:
PIT - FLT NR 8005 - AFTER TAKEOFF, CREW GOT RED WARNING FOR TAKEOFF CONFIGURATION FLAP, AMBER WARNING FOR L/D INOP AND ANTI-SKID INOP.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE ADJUSTED RT FLT/GRD SWITCH PER MM. OPERATION CHECKS GOOD.  (Z)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT FOUND CORROSION IN THE AREA OF THE LOWER CARGO DOOR FRAME STATION 370-427.  CUTOUT AND SPLICED IN NEW SECTION OF FRAME PER SRM 53-05 FIG 44.  (Z)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT ACCOMPLISHED SSID PSE 53.09.029 FOUND 3 CRACKS RANGING FROM .1250 INCH TO .6250INCH AT FUSELAGE STATION 76 LONGERON 26 COMING FROM RIVET HEADS.  EDDY CURRENT INSPECTION.  INSTALLED DOUBLER REPAIR PER SR09530239 AND EA 25347.  (Z)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT ACCOMPLISHED SSID PSE INSPECTION 53.09.029 FOUND 5 CRACKS RANGING FROM .1250 INCH TO .5 INCH AT STATION 69 LONGERON 2L COMING FROM RIVET HEADS.  EDDY CURRENT INSPECTION.  INSTALLED DOUBLER REPAIR PERDWG NR SR09530239 AND EA 25347.  (Z)


REMARKS:
BOS - FLT NR 1899 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT.  RECYCLED GEAR.  PER PILOT HANDBOOK ABNORMAL OPERATIONS 1-312-9, GEAR WAS NORMAL FOR LANDING.  FLIGHT RETURNED TO BOS AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE ADJUSTED NOSE GEAR DOOR RIGGING PER MM 32-22-01, PAGES 204-206.  CYCLED GEAR SEVERAL TIMES, OPS CHECKS NORMAL, ALL INDICATIONS NORMAL AND RECERTIFIED ALL WORK ADJUSTMENTS AND OPS CHECK OK.  (Z)


REMARKS:
ATL - FLT 833 - DURING FLIGHT, THE CABIN PERSSURE WENT TO 10,000 FEET WITH MULTI FUNCTION DISPLAY UNIT WARNING.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE PRIMARY AND SECONDARY OUTFLOW VALVES PER MM.  FUNCTIONAL CHECK SATISFACTORY.  (Z)


REMARKS:
CLT - FLT NR 1458 - AFTER TAKEOFF LEAVING 400 FEET, CREW RECEIVED FLT/GND SWITCH WARNING.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LT GEAR HARNESS AND NR 3 LEFT GEAR AIR/GND SENSOR.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
CLT - FLT 553 - DURING FLIGHT, THE NR 2 PITOT HEAT FAULT LIGHT ILLUMINATED AND WOULD NOT RESET.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 PITOT HEAT TUBE.  OPERATION CHECKS NORMAL PER MM.  (Z)


REMARKS:
PIT - FLT 164 - FLIGHT EN ROUTE DTW TO PHL WHEN FIRST OFFICERS FORWARD WINDSHIELD CRACKED.  FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED FIRST OFFICERS WINDSHIELD.  (Z)


REMARKS:
PHL - FORWARD SERVICE AND ENTRY DOOR EXTERIOR EMERGENCY LIGHTS WILL NOT ILLUMINATE.  MAINTENANCE REPLACED BATTERY PACK. (Z)


REMARKS:
AUS - FLT 1157 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO AUS AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND FORWARD ENTRY DOOR FALSE LOCKED.  RE-CLOSED DOOR.  (Z)


REMARKS:
PHL FLT - 560 - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF.  FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR LOCK ACTUATOR INOPERATIVE.  REPLACED ACTUATOR.  (Z)


REMARKS:
FOUND FORWARD CABIN EMERGENCY EXIT LIGHT OVER FORWARD SERVICE DOOR INOP.   REPLACED LIGHT AND BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND BELTFRAME SHEAR TIE CLIP CORRODED AT BS 987.7, RBL 8.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 27L INSIDE SURFACE CORRODED AT BELTFRAME, BS 986.5.  REPAIRED STRINGER PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR BEAM UPPER T-CAP CORROSION AT BS 986.5, LBL 50 AROUND NUTPLATE.  REPAIRED PERSWA RA 1-253-1091.


REMARKS:
UNABLE TO RAISE GEAR OR PRESSURIZE DUE TO GROUND SHIFT MALFUNCTION.  DE-ICED NLG DISCO LINK, GROUND OPS CHECKED GOOD.


REMARKS:
NO FLIGHT INVOLVED, NO PERSONNEL ON BOARD AIRCRAFT.  AIRCRAFT PARKED AT FORT LAUDERDALE JET CENTER.  BETWEEN 2200 AND 2215 EST A G-2 AIRCRAFT OWNED BY AMERICAN ENVIROMENT WAS TAXIING INTO THE JET CENTER/CUSTOMS AREA WHEN THE LEFT ELEVATOR OF THE G-2 AIRCRAFT STRUCK THE TOP RUDDER AND FAIRING OF VALUJET AIRCRAFT.  AIRCRAFT TERMINATING FLIGHT NR 93 ARRIVED AT8:25 PM 16 MAR 1994.  REPLACED RUDDER WITH LOANER FROM DC-9 FROM COMMODORE IN MIAMI.


REMARKS:
DURING THE PERFORMANCE OF AN 'N' CHECK, TECHNICIAN NOTICED NR 1 ENGINE C-1 AND C-2 FODED.  AIRCRAFT ATL, TERMINATING FLIGHT NR 56 AT 2143 LOCAL.  REPLACED C-2 DISC AND BLENDED C-1 PER MM71-00, PERFORMED ENGINE RUNUP, AIRCRAFT CHECKED GOOD.


REMARKS:
AIRCRAFT ON ROLLOUT, ACCELERATED TO 60 KNOTS, NR 1 ENGINE QUIT, AIRCRAFT RETURNED TO RAMP.  TROUBLESHOT NR 1 ENGINE, FOUND FUEL PUMP SHAFT SHEARED.  CHANGED FUEL PUMP AND FUEL CONTROL (TURN AROUND TIME FASTER BY CHANGING TOGETHER), BLED SYSTEM, RAN ENGINE, TRIMMED, GROUND CHECKED IAW M 71-00.


REMARKS:
NR 1 ENGINE OIL PRESSURE WENT TO 80 PSI AFTER TAKEOFF, AIRCRAFT LANDED AND RETURNED TO RAMP.  ADJUSTED OIL PRESSURE PERMM 71-00, OPERATIONAL CHECKED GOOD.  (Z)


REMARKS:
PHL - THE R4 DOOR EMERGENCY EXIT LIGHT FAILED TEST.  MAINTENANCE REPLACED THE LIGHT ASSEMBLY.  OPERATIONS CHECKED GOOD. (Z)


REMARKS:
BWI - FLT 8081 - RETURN TO FIELD DUE TO CAPTAIN'S AIRSPEED INDICATOR STUCK AT 10 KNOTS.  THE MACH SPEED TRIM LIGHT ALSOCAME ON.  MAINTENANCE REPLACED THE MACH AIRSPEED INDICATOR.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR WEB ANGLE DAMAGED AT BS 927-947, BL 0, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB SUPPORT ANGLE, AT AFT SIDE OF WEB CRACKED AT BS 597, WL 208, RBL 65.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 188, WL 148, RBL 18, AT BS 498, BETWEEN STRINGERS 21 AND 22L, AT BS 727D, BETWEEN STRINGERS 2 AND 3R, AT BS 500B, BETWEEN STRINGERS 24 AND 25 R, AT BS 282, BETWEEN STRINGERS 23 AND24R, AND AT BS 390, BETWEEN STRINGERS 21 AND 22R.  REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 360-370, STRINGER 4 TO 6L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 640, LBL 65.5, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, LBL 14.5, WL 208, AND AT BS 967, LBL 6, RBL 6TO 45.  REPAIRED PER TRAMCO EWO 94-0236.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 947.5, RBL 10 - LBL 14, WL 208.  REPAIRED PER TRAMCOEWO 94-0238.


REMARKS:
DURING SCHEDULED TRANSITION  CHECK, FOUND FLOOR BEAM CORRODED AT BS 328, LBL 328 AND AT RBL 35.5, WL 208.  REPAIRED PERSWA ACO 1-353-424.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CRACKED AT BS 328, RBL 21.5.  REPAIRED PER SWA RA 1-353-424.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, LBL 49.25 TO RBL 7.75, WL 208.  REPAIRED PER SWA RA 1-353-427.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 312, LBL 7.75, BL 0, RBL 7.75, 10.5, 11.5, WL 208.  REPAIREDPER SWA RA 1-353-421R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SEAT TRACK CORRODED FROM BS 334 TO 338, WL 208, RBL 45, AND AT BS 277, RBL 45. REPLACED TRACK PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SEAT TRACK CORROSION AT BS 335, RBL 45.  REPLACED TRACK PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 559-663.75.  REPAIRED PER SWA ACO 3315-53 R1.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 500A BETWEEN STRINGERS 21R AND 23R AND AT BS 988-1000, STRINGER 11L TO 14L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STRINGER 27R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 10R DAMAGED AT BS 336.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT CLIP NUT HOLES, BS 294, RBL 14.5, 20.5, 32, WL 208.  REPLACED PER SWA RA 1-353-418.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT CLIP NUT HOLES, BS 328, LBL 49.5, 28.5, RBL 13.5, 35.0, 49.0, 56.0, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, WL 208, RBL 29.5 AND AT BS 294.5, LBL 55.0, WL208.  REPLACED PER EA 1-353-41B AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 054, IN CRUISE, RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  FOUND AIR LEAKS AT AIR START VALVE CONNECTION AND AT PRIMARY HEAT EXCHANGER CLAMP.  REPLACED START VALVE AND PRIMARY HEAT CHANGER CLAMP PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, STRINGER 10R AND 10L.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
INT - DURING 'PCI PLUS STABILIZER MOD' CHECK VISUAL INSPECTION FOUND (10) .25 INCH CRACKS AT FASTENER HOLES AT STATION 211, STATION 235, STATION 243 FRAMES WL 212 TO WL 219 LEFT SIDE.  REPAIRED PER EA 25314, EO 5394G012.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION STATION 947.5 LBL 9, LBL 5, RBL 5, AND RBL 47-54.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 53-00-51.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 3 INCH BS 947 .5 INCH BY 4 INCH BS 967 CORROSION AT LBL 43 INTERCOSTAL BETWEEN CABIN FLOOR BEAMS.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-02.  (Z)


REMARKS:
INT - DURING 'PCI' CHECK VISUAL INSPECTION FOUND 2 INCH CRACK (TOP AFT OF SERVICE DOOR).  REPAIRED PER SRM 52-00-3 FIG 5.  (Z)


REMARKS:
INT - DURING 'PCI' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK PRESS WEB STATION 663 LBL 34 WL 196.5.  REPAIRED PER BOEING DRAWING 65C16935.  (Z)


REMARKS:
INT - DURING 'PCI' CHECK VISUAL INSPECTION EDDY CURRENT, FOUND .25 INCH CRACK STR 18A, LEFT HAND AT STATION 727 PART STRINGER.  REPAIRED PER EA 36958.  (Z)


REMARKS:
CLT - FLT 1209 - UNABLE TO PRESSURIZE AIRCRAFT ON TAKEOFF.  HEAR LOUD RUMBLE NEAR NOSE WHEEL.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND E/E DOOR COCKED IN HOLE AND SEAL HANGING OUT.  SECURED DOOR.  (Z)


REMARKS:
MCO - FLT 1212 - AFTER TAKEOFF RSW, FLIGHT CREW WAS UNABLE TO PRESSURIZE AIRCRAFT.  FLIGHT DIVERTED TO MCO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND APU PRESSURE SEAL ON BLEED AIR DUCT AT AFT BULKHEAD OFF.  SECURED SEAL.  PRESSURIZED AIRCRAFT.  OPS CHECK NORMAL.  (Z)


REMARKS:
SJU - FLT 1042 - RETURN TO FIELD DUE TO THE RIGHT AFT SERVICE DOOR BIENG LATCHED INCORRECTLY.  MAINTENANCE CHECKED THE RIGGING OF THE DOOR BEING LATCHED INCORRECTLY.  MAINTENANCE CHECKED THE RIGGING OF THE DOOR.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
INT - DURING 'PCI PLUS STATION MOD' CHECK VISUAL INSPECTION, FOUND SEVEN .25 INCH CRACKS AT FASTENER HOLES AT STATION 211, STATION 235, STATION 243 FRAMES WL 212 TO WL 219 RIGHT SIDE.  REPAIR PER EA 25314, EO 5394G012.  (Z)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND 53 INCH DISBONDED AREA, BS 767 TO BS 820 S20 R TO 25R.  DETECTED BYSONIC, REPAIRED PER EA 37007.  (Z)


REMARKS:
TPA - FLT 1632 - AFTER TAKEOFF UPON RAISING GEAR HANDLE, 'A' HYDRAULIC SYSTEM FAILED.  QUANTITY AND PRESSURE WENT TO ZERO.  FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED RIGHT MAIN GEAR ACTUATOR UP LINE.AIRCRAFT OK FOR SERVICE.  (Z)


REMARKS:
MCO - FLT 1164 - AFTER TAKEOFF AT APPROXIMATELY 5000 FEET, RIGHT PACK TRIPPED ON AND OFF AND NR 1 BLEED VALVE STUCK CLOSED.  FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED AIR CONDITIONING CONTROL MODULE.SYSTEM GROUND CHECKS OK.  (Z)


REMARKS:
BWI - FLT 0484 - RETURN TO FIELD DUE TO THE L-1 OUTER WINDOW PANE BEING CRACKED.  MAINTENANCE REPLACED THE L-1 WINDOW.OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
PHL - FLT 695 - FLIGHT EN ROUTE BDL TO CLT WHEN NR 2 ENGINE OIL PRESSURE INDICATOR WENT INTO THE YELLOW BAND, FLIGHT DIVERTED TO PHL WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND .1250 INCH OIL LINE TO THE TRANSFER CASE SHEARED ATTHE 90 DEGREE FITTING.  REPLACED OIL LINE AND 90 DEGEE FITTING.  (Z)


REMARKS:
MIA - FLIGHT 1814 - WHEN GEAR WAS RETRACTED, AIRCRAFT LOST THE 'A' HYDRAULIC SYSTEM.  FLIGHT RETURNED TO MIA WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED HYDRAULIC LINE AT LEFT MAIN GEAR ACTUATOR.  PINNED GEAR AND OPERATED GEAR HANDLE UP.  LEAK CHECKS OK.  (Z)


REMARKS:
EWR - FLT 165 - AFTER TAKEOFF CABIN FILLED WITH SMOKE.  FLIGHT RETURNED TO EWR WHERE LANDING WAS WITHOUT INCIDENT.  APUHAD BEEN PLACED ON MEL PRIOR TO FLIGHT DUE TO SMOKE IN CABIN.  MAINTENANCE REPLACED LEFT AND RIGHT WATER SEPARATOR BAGS.  CLEARED SYSTEM, AIRCRAFT OK FOR SERVICE.  (Z)


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION IN AFT OUTBD CORNER OF LT AFT LAV, FS 1176, RBL 64.  INSTALLED REPAIR PER SRM 51-10-1, 51-30-02 AND 51-30-03.  AIRCRAFT TOTAL TIME 48,500 HOURS, TOTAL CYCLES 31,993.


REMARKS:
STL - FLT 341 - DURING CLIMB, HAD UNCONTROLLABLE INCREASE IN CABIN ALTITUDE.  CABIN OXYGEN MASKS DEPLOYED.  CYCLED LT AIR CONDITIONING PACK SWITCH AND REGAINED CONTROL OF CABIN PRESSURIZATION.  REPLACED AUTO PRESSURIZATION CONTROLLER, MFG PN 763810-2.  PERFORMED AIR CONDITIONING PACK HEALTH CHECK, REPACKED CABIN OXYGEN MASKS.  PRESSURIZATION SYSTEM OPERATION CHECKED NORMAL.  CHECK C-1, 11-19-93, MCI.


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION IN AFT OUTBD CORNER OF RT AFT LAV, FS 1176, RBL 64.  REMOVED CORROSION PER SRM 57-10-06 AND REPAIRED PER SRM 51-10-1, 53-30-0 AND 51-30-03.  AIRCRAFT TOTAL TIME 48,500, AIRCRAFT TOTAL CYCLES 31,993.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACK IN INBD STRINGER 27L, STA 1183.  REPAIRED SRM 51-10-1 AND STANDARD PRACTICES.  AIRCRAFT TOTAL TIME 64,047, TOTAL CYCLES 43,268.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CORROSION IN E/E COMPARTMENT, INTERIOR SURFACE OF FUSELAGE SKIN, STRINGER 19R, STA 440 TO 480.  INSTALLED REPAIR PER DRAWING 69-61 AND SRM 53-10-3, FIGURE 1.  AIRCRAFT TOTAL TIME 64,047, AIRCRAFT TOTAL CYCLES 43,268.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CORROSION ON FLOOR BEAM SUPPORT, FS 1137, LBL 15, IN AFT CABIN.  REPLACED PART PER SRM 51-01-01 AND REMOVED CORROSION PER SRM 51-10-06 AND STANDARD PRACTICES.  AIRCRAFT TOTAL TIME 48,500, TOTAL CYCLES 31,993.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CORROSION ON STRINGER 29R, STA 1183.  REPAIRED PER SRM 5-10-1 AND STANDARD PRACTICES. AIRCRAFT TOTAL TIME 64,047, TOTAL CYCLES 43,268.


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION IN E/E COMPARTMENT ON FUSELAGE SKIN BETWEEN LONGERON 29L AND 29R, FS 170.  REMOVED CORROSION PER SRM 51-10-03 AND REPAIRED PER ARA 5234 AND SRM 53-04, FIGURE 12R.  AIRCRAFT TOTAL TIME 62,395, TOTAL CYCLES 69,448.


REMARKS:
ATL - FLT 534 - ON LANDING TOUCHDOWN, TAIL CONE DEPARTED THE AIRCRAFT.  TAIL CONE LOCK LIGHT DID NOT ILLUMINATE.  FOUNDBROKEN WIRE IN LOCK LIGHT CIRCUIT.  REPAIRED BROKEN WIRE, REPLACED TAIL CONE.  LIGHT OPERATION CHECKED NORMAL.  CHECK C-2B, 4-7-94, MCI.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A .75 INCH CRACK IN LT WING UPPER IWS 555 RIB T-CHORD, STRINGER 19.  REPAIRED PER DRAWING 1647070 AND SRM 51-10-01.  AIRCRAFT TOTAL TIME 17,100, TOTAL CYCLES 17,100.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A .6250 INCH CRACK IN LT WING UPPER IWS 555 RIB T-CHORD, STRINGER 12.  REPAIRED PER DRAWING 1647070 AND SRM 51-10-01.  AIRCRAFT TOTAL TIME 60,589, TOTAL CYCLES 17,100.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A .6250 INCH CRACK IN LT WING UPPER IWS 555 RIB T-CHORD, STRINGER 13.  REPAIRED PER DRAWING 1647070 AND SRM 51-10-01.  AIRCRAFT TOTAL TIME 60,589, TOTAL CYCLES 17,100.


REMARKS:
INT - DURING CX-4 CHECK VISUAL INSPECTION FOUND APPROXIMATELY 7 INCH CRACK, 727 BS LT SIDE PRIMARY CHORD WEB FLANGE CRACK STARTS AT S 23 AND FOLLOWS CHORD WEB FLANGE TO NR 4 FLAP TRACK SUPPORT FITTING.  VISUAL, EDDY CURRENT CONFIRMED.  REPAIRED PER BOEING DRAWING 65C33722, EA 36957 AND SB 737-53-1088.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORRODED SCREW HOLES ON FLOOR BEAM BS 294.5 8 INCHES LBL.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-04B.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORRODED SCREW HOLES ON INTERCOSTAL BETWEEN BS 294.5 BS 312 11 INCHES LBL.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER TR 51-10-01.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORRODED AREA 2 PLACES FLOOR BEAM BS 312 7 INCHES RBLAND 11 INCHES LBL.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-13.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORRODED AREA AT SCREW HOLES ON FLOOR BEAM BS 328 28 INCHES LBL AND 51 INCHES LB.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-13.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 2 INCH BY 4 INCH CORROSION STA 967 STR 26R.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  REPAIRED PER SRM 53-10-3.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 1 INCH BY 2 INCH CORRODED AREA Z-ANGLE STA 312 DOOR SILL AREA.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION FOUND 2 INCHES BY 34 INCHES CORRODED AREA Z-ANGLE STA 294.5 TO 334.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH AREA CORRODED PRECISE LOCATION BS 328 RBBL 12.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-13.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 22 INCH CORRODED AREA FLOOR BEAM STATION 259 11 INCHES LBL TO11 INCHES RBL.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-16.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 28 INCH CORRODED AREA FLOOR BEAM STATION 294.5 RBL 12 TO RBL 40.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER TR 53-10-04B.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 11 INCHES CORRODED AREA FLOOR PANEL ATTACH POINT STATION 259-270 11 INCHES LBL.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1, DRAWING 65-45833.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH SCREW HOLES CORRODED BS 270-284 11 INCHES LBL AND 1 INCH BY 1 INCH TOP AFT CORNER OF SAME ANGLE.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.(Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 1 INCH CORRODED AREA FORWARD ENTRANCE GIRT BAR ATTACH POINTS.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCHES LONG STATION 178 LBL 6 INCHES.  REPAIRED PER TR 53-10-17.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK RBL 6 178 BULKHEAD AFT SIDE.  REPAIRED PER TR 53-10-11.(Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 LBL 6 INCH 10 INCH BELOW FLOOR LEVEL.  REPAIRED PERTR 53-10-11.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 4 INCH CORRODED AREA BS 270 RBL 11 INCH AND LBL 11 INCH.  CORROSION TASK MR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-40-04.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 20 INCH CORRODED AREA BS 947-997, S 17 L (AFT ENTRY DOOR SILLCHORD 'Z' ANGLE).  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSEPCITON, FOUND 5 INCH BY 30 INCH CORRODED AREA BS 947-997 AT S 17 R (AFT SERVICE DOOR SILL 'Z' ANGLE).  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 500 C PLUS 4.5 INCH AND S 16L.  REPAIRED PER SB 737-53-1145 EA 36824.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL, FOUND CORROSION 2 INCH BY 1 INCH CORRODED AREA BETWEEN 947 AND 967 LBL 24.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER 51-10-1.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION BS 986.5.  REPAIRED PER TR 53-10-05. CORROSION TASK NR C53-107--02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION FOUND 2 INCH DIAMETER SPOTS OF CORROSION.  AFT LAVATORY MOUNTS JUST AFT OF BS 946.5 APPROXIMATELY LBL 50.  REPAIRED PER SRM 51-10-2, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA FITTINGS AT BS 277 AND 303 LBL 11.10.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER 51-10-1.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE 1 INCH DIAMETER SPOTS OF CORROSION APPROXIMATELY .030 INCH DEEP ON BS 967 BEAM AT LBL 5.37 AND 43.  SHEAR WEB AT AFT ENTRANCE DOOR CORRODED LEVEL 1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 53-00-51 FIG 202.  (Z)


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LEFT FUSELAGE SKIN CRACKED, APPROX 5 INCHES AFT OF LEFT WING BODY  FAIRING.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 'A' CHECK, FOUND CABIN FLOOR TRACK LIGHTS  REMAIN ILLUMINATED WITH SWITCH IN OFF POSITION.  REPLACED AFT BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT OVERHEAD LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD CABIN FLOOR TRACK LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ON CEILING AT AFT CABIN INOP.  REPLACED BATTERY CHARGER PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 720.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FRAME CRACKED AT BS 277, LBL 7, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 14L CRACKED AT BS 992.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND CORROSION ON TOP OF FLOORBEAM, BS 312, RBL 12.5, WL 208.  REPAIRED PER SWA RA 1-353-421 R2.


REMARKS:
DURING SCHEDULED D CHECK, FOUND BULKHEAD CRACKED TWO PLACES AT BS 178, WL 235, RBL 105.  REPAIRED PER TRAMCO EWO 94-0249.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND 2 GOUGES ON FUSELAGE SKIN, UNDER FORWARD ENTRY DOOR, ABOVE STRINGER 18R BETWEEN BS 307 AND 310.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK,  FOUND SHEAR TIE CORRODED AT BS 727A, RBL 6 TO LBL 6, WL 149.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED CHECK, FOUND CABIN FLOOR SUPPORT HAT CHANNEL CRACKED AT BS 540, LBL 2.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
AT FL350, APU FIRE WARNING LIGHT ILLUMINATED, WITH APU IN OFF POSITION.  APU FIRE BOTTLE WAS DISCHARGED AND LIGHT EXTINGUISHED.  INSPECTED APU AREA WITH NO EVIDENCE OF FIRE.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CABIN EMERGENCY FLOOR TRACK LIGHTING INOP AT OVERWING EXIT.  REPLACED EMERGENCY LIGHT BATTERY AND BASE.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CHORD CRACKED AT BS 616, WL 200, RBL 65.  REPAIRED PER TRAMCO EWO 94-0240 AND 94-0241.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT FORWARD SERVICE DOORWAY LOWER AFT CORNER CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FRAME CRACKED AT BS 663, STR. 3L.  REPAIRED PER TRAMCO EWO 94-0248.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT CARGO TIE DOWN TRACK CORRODED FROM BS 794.3 TO 847 AND AT 927 TO 947.5.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE CORRODED  AT BS 727A, RBL 6.5 TO 10, WL 149.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1050 AND 1044, BETWEEN S19 AND 20R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DENTED AT BS 830 TO 835, BETWEEN S26 AND 27R, AT BS 1028, BETWEEN S26R AND S27R AND AT BS 976, BETWEEN S23 AND 24L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
STL - DURING OP-9 FOUND BELTRING, STA 1104, CRACKED .1250 INCH AT LONGERONS 3L, 4L, 5L AND 6L.  REPLACED SECTION OF BELTRING PER SRM CHAPTER 51.  AIRCRAFT TOTAL CYCLES 76,188.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A 1.25 INCH AND A ONE-INCH SKIN CRACK AT STA 718, LONGERON 5R.  REPAIRED PER SRM 53-02, FIGURE 2.  TOTAL CYCLES 71,386.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND CRACK APPROXIMATELY 1.25 INCH LONG IN NR 1 HORIZONTAL BEAM FORWARD END, RADIUS OUTBD SIDE.  REPLACED BEAM PER DRAWING 911579.  TOTAL CYCLES 74,615.


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION ON FUSELAGE SKIN IN E/E COMPARTMENT, BETWEEN LONGERON 29L AND 29R, FS 170.  REMOVED CORROSION PER SRM 51-10-03 AND REPAIRED PER ARA 5234 AND SRM 53-04, FIGURE 12B.  TOTAL CYCLES 69,448.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN LONGERON L7, STA 680.  REPAIRED PER SRM 5302, FIGURE 2.  TOTAL CYCLES 70,304.


REMARKS:
STL - FLT 517 - INVESTIGATION OF ENGINE OIL FILTER WARNING LIGHT ILLUMINATION AND VIBRATION REVEALED NR 3 BEARING FAILED, PN 804059.  ENGINE SN 2150 WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
JFK - DURING C-CHECK, FOUND CORROSION ON OUTBD SIDE OF RT MLG TORQUE BOX AT LANDING GEAR ACTUATOR UPPER ATTACH FITTING MOUNT BOLTS, AND SECTION FORWARD OF BOLTS.  REMOVED CORROSION PER SRM 51-21-01, PAGE 1, TREATED CORROSION AREA AND PAINTED.  TOTAL CYCLES 22,350.


REMARKS:
JFK - DURING C-CHECK, FOUND THREE CRACKS AT FORWARD FITTING FOR L-1 DOOR SAFETY STRAP.  INSTALLED REPAIR DOUBLER PER SRM 51-50-01, PAGES 3, 4 AND 5.  AIRCRAFT TOTAL CYCLES 22,350.


REMARKS:
STL - FLT 433 - DURING CRUISE, NR 3 OVEN EMITTED SMOKE DURING OPERATION.  TURNED OFF OVEN, MFG PN 50381.  REPLACED OVEN, OPS CHECKED NORMAL.  CHECK C-1A, 3-26-94, MCI.


REMARKS:
MCI - DURING OP-15 FOUND CORROSION IN AFT CARGO COMPARTENT, LONGERON 22R INTERCOSTAL, STA 945-965.  INSTALLED NEW INTERCOSTAL PER STANDARD PRACTICES.  AIRCRAFT TOTAL CYCLES 71,936.


REMARKS:
LGA - FLT 1129 - CLIMBING OUT OF 6000 FEET, CAPTAIN'S NR 2 WINDOW STARTED TO ARC AND CRACK.  FLIGHT RETURNED TO LGA ANDLANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED LT SLIDING WINDOW.  SYSTEM OPS CHECKS NORMAL.  (W)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 312, RBL 12-5, WL 208.  REPAIRED PER SWA RA 1-363-421 REV.2


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 294.5, LBL 35 TO 52, WL 208.  REPAIRED PER SWA RA 1-353-418.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 344, RBL 10, WL 208.  REPAIRED PER SWA RA  1-353-427.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND HORIZONTAL STABILIZER T-CHORD AND REAR SPAR WEB DAMAGE AT STA 166 LEFT.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT OVER AFT SERVICE DOOR WILL NOT TEST.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
DURING PREFLIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS INOP.  REPLACED FORWARD BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD CABIN EMERGENCY TRACK LIGHTS DIM.  REPLACED FORWARD BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND CHORD CRACKED AT BS 178 BULKHEAD RIGHT SIDE IN RADIUS, WL 194 TO 196.5.  REPAIRED PER TRAMCO EWO 94-0244.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND DOOR FRAME THRESHOLD SUPPORT WEB DAMAGED AT BS 794.3 TO 847, RBL 23-30, WL 161.5.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
CLT - DURING SHOP FUNCTIONAL TEST OF A 727 LIFE RAFT, MPN R0202A203, THE TWO AIR CYLINDERS TESTED FAILED TO PRODUCE SUFFICIENT AIRFLOW TO OPERATE THE RAFT ASPERATORS.  SHOP TEST OF 28 ADDITIONAL CYLINDERS FOUND 21 ADDITIONAL FAILURES.  CYLINDER FAILURES WERE TRACED TO THE BOTTLE REGULATOR, PN 524 GPS-2.  ALL UNITS WERE RETURNED TO THE VENDOR FOR REWORK.  (X)


REMARKS:
NUMBER 1 ENGINE FUEL FILTER DIFFERENTIAL LIGHT ILLUMINATED IN FLIGHT.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED FUEL FILTER AND FUEL PRESSURE SWITCH PER BOEING M/M.


REMARKS:
WEATHER RADAR DISPLAYED ANTENNA AND ATTITUDE FAULT.  AIRCRAFT DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACEDRADAR R/T UNIT PER BOEING M/M.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND NUMBER 2 ENGINE PYLON SKIN CRACKED AT TOP FORWARD CORNER OF ACCESS PANEL 5724L OPENING. REPAIRED PER SWA RA 6053-54.


REMARKS:
NUMBER 4 MAIN GEAR TIRE BLEW ON TAKEOFF, CAUSING DAMAGE TO  RIGHT WING INBOARD T/E  MID FLAP AND FOREFLAP.  AIRCRAFT RETURNED TO AUS AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 3 AND 4 MAIN GEAR WHEEL ASSEMBLIES, RIGHT GEAR INBOARD DOOR AND GEAR STRUT DOOR, RIGHT WING T/E MID FLAP AND FOREFLAP, AND RIGHT GEAR ANTI-SKID HARNESS PER BOEING M/M.


REMARKS:
SLC - FLT 177 - INVESTIGATION OF STALL AND INCREASING EGT ON ENGINE SN 3258 REVEALED INTERMEDIATE CASE REAR SKIRT, PN 804127, EIGTH STAGE SUPPORT FLANGE CRACKED WITH HPC AND HPT DAMAGE.  INCORPORATED PRATT AND WHITNEY SB 6117.  ENGINE SN 3258 REPAIRED AND RETURNED TO SERVICE.


REMARKS:
DEN - FLT 410 - INVESTIGATION OF STALLS IN ENGINE SN 3243 REVEALED 7TH STAGE COMPRESSOR BLADE, PN 809407, BROKE CAUSINGHPC DAMAGE.  ENGINE SN 3243 REPAIRED AND RETURNED TO SERVICE.


REMARKS:
SGF - INVESTIGATION OF ENGINE SN 1211 STALL AND SPOOL DOWN REVEALED SECOND STAGE LPT BLADE, PN 800002, FRACTURED CAUSING TURBINE DAMAGE.  ENGINE SN 1211 WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
INT - DURING Q-1 VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 294.5-312 28 INCHES LBL.  CORROSION TASK NRC53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 53-10-3, SRM 51-10-1.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECITON, FOUND .25 INCH CRACK BS 500 C PLUS 4.5 INCH AND S 16 R.  REPAIRED PER SB 737-53-1145 EA 36824.  (Z)


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND A 4.125 INCH CRACK IN LEFT FUSELAGE SKIN FROM BS 394 TO BS 398, 2.25 INCH ABOVE S24L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND SHEAR STRAPS CRACKED AT BS 314, LBL 1 AND RBL 30.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FLOORBEAMS CRACKED AT BS 520, RBL 45.5, 24.75, AND AT LBL 24.75.  REPAIRED PER SWAACO 3198-53 AND RA 1-353-1095.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND STRINGER CLIPS  CRACKED AT BS 663, S10R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND STRINGER TIE CLIPS  CRACKED AT BS 663, S10R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FORWARD CARGO BIN FORWARD FRAME CRACKED AT LOWER UPPER CORNER OF BOTTOM STOP FITTING.  REPAIRED FRAME CRACKED PER SWA RA 1-353-1094.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND SEAT TRACK SUPPORT CHANNELS CRACKED AT UPPER CORNERS AT BS 520, RBL 45.5 AND 24.75.  REPLACED CHANNEL PER SWA ACO 3198-53.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND LEFT SIDEWALL BELTFRAME INBOARD CHORD CRACKED AT LOWER END. REPAIRED PER SWA RA 1-353-1096.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FLOORBEAM CORROSION AT BS 1016, RBL 10 TO 16.  REPAIRED PER SWA RA 1-353-1102.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FLOORBEAM CORROSION AT BS 968, RBL 28.5.  REPAIRED PER SWA RA 1-353-1099.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 10.75. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FLOORBEAM CORROSION AT BS 947 AT FORWARD FLANGE, RBL 2.  REPAIRED PER SWA RA 1-353-1097.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND LEFT RAM AIR INLET UPPER INBOARD CHORD ANGLE CRACKED AT BS 540, S23L. REPLACED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND KEEL BEAM SKIN PANEL CRACK AT BS 680, 18 INCHES FROM END OF PANEL AND AT BS 700, 36 INCHES FROM END OF PANEL.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
STL - DURING C-CHECK, FOUND ONE-INCH CRACK ON 24R RUDDER RIB.  REPLACED RIB PER SRM 51-30 AND SRM 55-03, FIGURE 11.  AIRCRAFT TOTAL CYCLES 71,420.


REMARKS:
STL - DURING C-CHECK, FOUND .75 INCH CRACK IN LONGERON 4L, STA 160.  REPAIRED LONGERON PER SRM 53-02, FIGURE 2 AND DRAWING SRO 9530128.  TOTAL CYCLES 71,420.


REMARKS:
STL - DURING C-CHECK, FOUND .75 INCH CRACK IN LONGERON 2L, STA 160.  REPAIRED LONGERON PER SRM 53-02, FIGURE 2 AND DRAWING SRO 9530128.  TOTAL CYCLES 71,420.


REMARKS:
STL - FLT 324 - DURING CLIMB EXPERIENCED SMOKE IN COCKPIT.  COMPLETED ELECTRICAL ISOLATION CHECK LIST AND FLIGHT RETURNED.  FOUND FORWARD LT LAVATORY MULTIPLEX DECODER, MFG PN 275D499, FAULTY.  REPLACED DECODER AND OPERATION CHECKED NORMAL.  CHECK C-8A, 12-22-93, JFK.


REMARKS:
STL - DURING C-CHECK, FOUND A .1250 INCH LONG CRACK IN LONGERON 7L, STA 639.  REPAIRED LONGERON PER SRM 53-02, FIGURE 2.  TOTAL CYCLES 71,420.


REMARKS:
AT EWR, FLT NR 48, INBOARD FR PBI, NR 4 LE SLAT DID NOT ILLUMINATE GREEN ON APPROACH TO LANDING UNTIL GO AROUND INITIATED.  REMOVED AND REPLACED NR 4 LE ACTUATOR AND NR 4 LE FLAP SW PER MM 27-81.  OPS CHECK AND LEAK CHECK OK.  (Z)


REMARKS:
AT EWR, FLT NR 5, EWR TO MDW ON CLIMB-OUT CO-PILOT R1 OUTER PANE WINDSHIELD CRACKED.  REMOVED AND REPLACED CO-PILOT WINDSHIELD R1 PER MM 56-11-11.  REMOVED AND REPLACED NR 1 WINDOW HEAT CONTROL PRECAUTIONARY.  OPS AND LEAK CHECKED OK.  (Z)


REMARKS:
AT EWR, FLT NR 39 ON TAXI OUT, NR 4 LE FLAP LIGHT IS AMBER WITH 15 DEGREES.  REMOVED AND REPLACED NR 4 LE FLAP SWITCH PER MM 27-82-1 PG 401.  OPS CHECK OK.  (Z)


REMARKS:
DURING FC-5 INSPECTION, FOUND 1 INCH CRACK IN PLATE UNDER ELEVATOR GUST LOCK VERTICAL STABILIZER.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR EA NR 25498.  (Z)


REMARKS:
CLT - FLT 833 - AFTER TAKEOFF, BLEED NR 1 AND NR 2 WILL NOT REMAIN, RESET INFLIGHT EVEN AT LOW POWER SETTINGS.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE PRSOV.  OPERATION AND LEAK CHECK NORMAL.  (Z)


REMARKS:
CLT - FLT 429 - DURING FLIGHT THE PRESSURIZATION WAS COMPLETELY ERRATIC.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 2 DIGITAL AIR DATA COMPUTER.  CHECK NORMAL.  (Z)


REMARKS:
EWR - FLIGHT NR 456 - AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR DOOR LOCK SWITCH ANNUNCIATED IN AMBER ON MULTI FUNCTION DISPLAY UNIT.  CYCLED GEAR.  AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT.  MAINTENANCE LUBED DOOR LOCK AND RESET PSEU.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLIGHT NR 1733 - AIRCRAFT ARRIVED WITH THE EMERGENCY LIGHTS INOP.  MAINTENANCE SECURED WIRE ON DIODE.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLT 8006 - ABOUT 10 MINUTES AFTER TAKEOFF THE NR 1 ENGINE FAIL LIGHT ILLUMINATED IN HANDLE.  ALSO, THE NR 1 EMUX MESSAGE ALERTED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE PERFORMED BITE CHECK, NO FAULTS NOTED.  REPLACED NR 1 EMUX COMPUTER, ALL CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLIGHT NR 294 - THE DC BUS NR 1 FAILED IN FLIGHT, DC BUS NR 1 LIGHT ON MULTI FUNCTION DISPLAY TRU NR 1 SHOWS 0 VOLTS.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE INSTALLED NR 1 TRU.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
ORF - FLIGHT NR 1267 - DURING FLIGHT, CABIN PRESSURE EXCEEDED 10,000 FEET AT FL 310.  CABIN CONTINUED CLIMBING TO 15,000 FEET WHERE THE PAX 02 MASKS DEPLOYED NORMALLY.  UNABLE TO CONTROL PRESSURE MANUALLY.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE RAN BITE CHECK ON PRESSURE CONTROLLERS.  ALL CHECKS OK.  PRESSURIZED AIRCRAFT AND FOUND FWD ENTRY DOOR SEAL LEAKING.  REPLACED FWD ENTRY DOOR SEAL AND STOWED ALL MASKS.  ALL CHECKS NORMAL.  (Z)


REMARKS:
CLT - FLIGHT 1126 - FLIGHT EN ROUTE MCO TO ISP, WHEN IN CRUISE AT FL 330, LOST INSTRUMENT LIGHTING, CAPTAINS INSTRUMENTATION, AND CABIN PRESSURE BECAME UNCONTROLLABLE.  FLIGHT DESCENDED TO 10,000, RESET NR 1 MAIN DISTRIBUTION CIRCUIT BREAKER.  DIVERTED TO CLT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND LEFT GENERATOR 'A' PHASE OPEN.  REPLACED GENERATOR.  OPS CHECK NORMAL.  (Z)


REMARKS:
PIT - FLT NR 285 - DURING CRUISE, THE CREW EXPERIENCED A UTILITY SYSTEM FAILURE LIGHT.  AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED.  AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED AN O-RING AT THE LANDING GEAR SELECTOR VALVE.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
CLT - FLIGHT 1232 - DURING FLIGHT, THE RADAR BECAME USELESS FOR 5 TO 10 MINUTES AFTER IT WAS TURNED ON.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED RADAR TRANSCEIVER.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
CLT - FLT 1062 - AFTER TAKEOFF, THE CREW FELT SEVERE VIBRATION.  THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND THE NOSE GEAR DOORS OPEN.  CLOSED DOORS, OK FOR SERVICE.  (Z)


REMARKS:
PIT - FLT 1574 - WHILE EN ROUTE CRW-PIT, THE LEFT ENGINE OIL STRAINER LIGHT ILLUMINATED.  THE CREW SHUT DOWN THE LEFT ENGINE AND LANDED IN PIT WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT ENGINE ASSEMBLY PER WORK CARDS J371-00-1.  (Z)


REMARKS:
CLT - FLT NR 776 - WHILE EN ROUTE CMH-CLT, THE LEFT ENGINE OIL STRAINER LIGHT ILLUMINATED.  THE CREW SHUT DOWN THE LEFTENGINE AND LANDED IN CLT WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH.  OPS AND LEAK CHECK GOOD.  ACCOMPLISHED NR 1 ENGINE WINDMILLING INSPECTION, OIL STRAINER AND CHIP DETECTORS OK.  AIRCRAFTOK FOR SERVICE.  (Z)


REMARKS:
ATL - FLT 551 - FLIGHT EN ROUTE IND TO TPA WHEN FIRST OFFICERS WINDSHIELD OUTER PANE CRACKED.  FLIGHT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED FIRST OFFICERS WINDSHIELD. (Z)


REMARKS:
MCI - FLIGHT 1796 - CAPTAINS WINDSHIELD OUTER PANE ARCHED AND CRACKED.  FLIGHT RETURNED TO MCI AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CAPTAINS WINDSHIELD.  (Z)


REMARKS:
MCI - ON APPROACH INTO MCI, CREW RECEIVED NO LIGHT INDICATION THAT THE GEAR WAS DOWN.  FLYBY TOWER SHOWED GEARS WERE DOWN.  RESET GEAR RELAY AND LIGHTS CIRCUIT BREAKER, NO HELP.   CHECKED GEAR THROUGH VIEWING LENSES, GEAR CHECKED DOWN AND LOCKED.  LANDED MCI WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND CIRCUIT BREAKER SECTOR 5 POPPED.  CYCLED CIRCUIT BREAKER.  ALL INDICATIONS NORMAL.  (Z)


REMARKS:
CHS - FLIGHT 1260 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO CHS WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND AFT SERVICE DOOR FALSE LOCKED.  RIGGED DOOR.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 54 INCHES BY 2 INCHES BS 947.5 - 1000.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER 51-10-02.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO PLACES 1 INCH BY 2 INCH CORROSION 'Z' ANGLE STATION 992 AND 947.5 LEFT AFT DOOR.  CORROSION TASK NR C52-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 32 INCHES BY 1 INCH BS 1006, LBL 16 TO RBL 16.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM CORRODED AROUND NUT PLATE HOLES BS 772 BS 813 RBL 8.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  REPAIRED PER SRM 53-00-53.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CORROSION AROUND ANCHOR NUT HOLES AT BS 753, BS 794, BS 826 AND BS 859.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION BS 772 - BS 859 LBL 12.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  REPAIRED PER SRM 53-00-53.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CORROSION AT CLIP NUT HOLES BS 947.5 TO BS 967 LBL 45.  REPAIREDPER SRM 51-10.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM 1 INCH CORROSION AROUND CLIP NUT HOLES BS 967 TO BS 947 RBL 45 AT BS 949.  REPAIRED PER SRM 51-10.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH CORROSION T-ANGLE BS 957 RBL 18 - RBL 22.  REPAIRED PER SRM 51-10.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND LOWER FUSELAGE SKIN BULGING BETWEEN FASTENERS AT BS 927, BETWEEN S27R AND S26R.  REPAIRED BELTFRAME PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND BELTFRAME TIE DOWN CLIP CRACKED AT RADIUS UNDER AFT CARGO DOOR SILL, AT BS 827,  RBL 20.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND RIGHT WING AUX TRACK AT NUMBER 4 SLAT CUTOUT CRACKED.  REPLACED PER SWA RA 1-251-228.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND RIGHT WING AUX TRACK AT NUMBER 5 SLAT CUTOUT CRACKED.  REPLACED PER SWA RA 1-251-227.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR AND PASSENGER DOOR EMERGENCY LIGHTS INOP.  REPLACED AFT BATTERY PACK PER BOEING M/M.


REMARKS:
DURING CRUISE, EXPERIENCE NUMBER 1 ENGINE N1 OVERSPEED WITH ASSOCIATED ENGINE SHUTDOWN.  AIRCRAFT RETURNED TO TUL AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 1 ENGINE PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND LEFT INBOARD MID FLAP SKIN TORN AT INBOARD L/E SKIN CUOUT.  REPAIRED PER SWA RA 1-357-229.


REMARKS:
DURING Q-1 CHECK INSPECTION, ACCOMPLISHED CORROSION TASK NRC57-58300 CARD NR J9-57-53700-C FOUND LEVEL 2 CORROSION AT THE AFT CARGO DOOR JAMB.  SPLICED IN NEW SECTION OF DOOR JAMB PER SRM 53-05 FIG 44.  (Z)


REMARKS:
DTW - THE FLOOR EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED THE AFT LEFT CHARGER ASSEMBLY FOR THE TAIL AREA FLOOR LIGHTS.  OPS CHECKS NORMAL.  (Z)


REMARKS:
JAX - FLT 1166 - WHILE EN ROUTE CLT TO NAS, THE CAPTAINS WINDSHIELD BEGAN CRACKING AND SEVERAL CRACKS CROSSED THE WINDSHIELD.  THE FLIGHT DIVERTED TO JAX AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD PER MM 56-10-02.  PRESSURE CHECKS OK.  (Z)


REMARKS:
DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT BELT FRAME 889 UPPER AND LOWER FLANGE BETWEEN LONGERON 19L AND 23L.  CLEANED OUT CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 7.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT ACCOMPLISHED SID PSE 58.09.029/030, FOUND 5 CRACKS .1250 INCH TO .25 INCH LONG COMING OUT FROM RIVET HEADS AT STATION 69 BETWEEN LONGERON 2L AND 3L.  INSTALLED FLUSH TYPE REPAIR PER SRO 9530289 AND EA NR 25748.(Z)


REMARKS:
DURING AGING AIRCRAFT VISIT ACCOMPLISHED SID PSE 53.09.029/030, FOUND 7 CRACKS RANGING FROM .1250 INCH TO .3750 INCH ATSTATION 76 BETWEEN LONGERON 2R AND 3R COMING FROM RIVET HEADS.  INSTALLED FLUSH TYPE DOUBLER REPAIR PER SRO 9530239 ANDEA 25748.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT, FOUND FUSELAGE SKIN CRACK .5 INCH LONG AT STATION 1087 BETWEEN LONGERON 296 AND 306.  INSTALLED DOUBLER PER SRM 53-04, FIG 12B CLASS I REPAIR.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT, INSPECTION FOUND CORROSION AT STATION 980 LONGERON 22L AT AFT SERVICE PANEL BOTTOM FORWARDCORNER.  INSTALLED DOUBLER TYPE REPAIR PER SRM 53-04 FIG 12B, DRW NR 5911523 SH1 ZONE 4, EA 26039 EA 26077 AND SRM 53-02 FIG 1.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT, FOUND 1.5 INCH CRACK IN RADIUS OF RT VERTICAL STABILIZER/FUSELAGE ATTACH ANGLE STATION 1095.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 23.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT INSPECTION, FOUND 3 CRACKS .1250 INCH TO .25 INCH IN LENGTH BETWEEN LONGERONS 2R AND 3R AT STATION 69 COMING FROM RIVET HEADS.  INSTALLED FLUSH TYPE REPAIR PER SRO 9530239 AND EA 25347.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT INSPECTION, REVEALED .3650 INCH CRACK OF THE LOWER AFT CORNER OF THE SERVICE DOOR JAMB RT SIDE FUSELAGE SKIN.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 35.  (Z)


REMARKS:
DURING AGING AIRCRAFT VISIT INSPECTION, FOUND 5 CRACKS RANGING FROM .1250 INCH TO .3750 INCH COMING FROM RIVET HEADS ATSTATION 69 BETWEEN LONGERON 2L AND 3L.  INSTALLED FLUSH REPAIR PER SP09530239 AND EA 25347.  (Z)


REMARKS:
DURING Q-1 CHECK, INSPECTION ACCOMPLISHED CPCP INSPECTION C46-53305 CARD NR J9-46-25700-C, FOUND LEVEL 2 CORROSION AT SUB FLOOR UNDER AND INBAORD OF NR 1 GALLEY SCUPPER AREA.  CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 2SHT 3.  (Z)


REMARKS:
DUIRNG Q-1 INSPECTION, FOUND 3 .1250 INCH CRACKS WHILE ACCOMPLISHING SID PSE 53.09.029/030 COMING FROM RIVET HEADS AT STATION 69 LONGERON 2R AND 3R.  INSTALLED DOUBLER REPAIR PER SRO 9530239 AND EA 25795.  (Z)


REMARKS:
JFK - FLT 206 - WHILE EN ROUTE DCA-BOS, THE CREW SHUTDOWN THE LEFT ENGINE DUE TO LOSS OF RPM, EPR AND EGT DROPPING.  THE FLIGHT DIVERTED TO JFK AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT ENGINE FUEL PUMP PER MM 73-10-1.  RAN ENGINE, LEAK AND OPS CHECKS GOOD.  (Z)


REMARKS:
BWI - FLT 268 - AFTER TAKEOFF ON GEAR RETRACTION, THE RIGHT GEAR UNSAFE LIGHT ILLUMINATED.  RECYCLED GEAR AND LIGHT STILL ON.  THE FLIGHT RETURNED TO BWI AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT GEAR UPLOCKS SWITCH PER MM 32-60-1.  FUNCTIONALLY CHECKED OK.  (Z)


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FORWARD SERVICE DOOR FORWARD FRAME CRACKED AT LOWER END INBOARD RADIUS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND FORWARD SERVICE DOOR FRAME Z ANGLE CRACKED AT BS 287.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2D CHECK, FOUND FORWARD SERVICE DOOR UPPER FRAME CUTOUT CRACKED AT LOWER OUTBOARD SIDE.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING ANNUAL SLIDE FUNCTIONAL CHECK, L1 SLIDE DEPLOYED NORMALLY AND HELD PRESSURE.  HOWEVER, NONE OF THE SLIDE MOUTED LIGHTS ILLUMINATED.  MAINTENANCE REPLACED BATTERY PACK.  (W)


REMARKS:
SFO - FLT 162 - FORWARD CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF.  FLIGHT RETURNED TO SFO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE RECLOSED DOOR.  (Z)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, STR 10L AND 10R, BS 887, STR 4R, BS 807, STR 8R, BS 827, STR 4R, BS 360, STR 4L, BS 867, STR 10R AND AT BS 867, STR 4R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 1038, AFTER TAKEOFF, CREW UNABLE TO PRESSURIZE AIRCRAFT.  AIRCRAFT RETURNED TO DTW AND MADE AN UNEVENTFUL LANDING.  FOUND AFT CARGO DOOR OPEN AND DOOR WARNING SWITCH BROKEN.


REMARKS:
DURING SCHEDULED A3 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 925, STRINGER 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND LEFT INBOARD MIDFLAP L/E SKIN CUTOUT CRACKED.  REPAIRED PER SWA RA 1-357-229.


REMARKS:
PIT - FLT 668 - BEFORE DEPARTURE OF FLIGHT, EMERGENCY FLOOR LIGHTING IN FIRST CLASS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED INVERTER.  SYSTEM CHECKS NORMAL.  (X)


REMARKS:
CLT - FLT 1863 - DURING FLIGHT, NR 2 CSD WARNING CAME ON AND WAS DISCONNECTED PER PILOT HANDBOOK.  AIRCRAFT RETURNED TOFIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND NR 2 CSD OVERSERVICED.  DRAINED OIL, OPERATION CHECKS NORMAL.  (X)


REMARKS:
PIT - FLT 2697 - DURING FLIGHT, 'FLAP ASYM' DISPLAYED ON MFDU.  AIRCRAFT RETURNED TO FIELD AND PERFORMED ZERO DEGREE FLAP LANDING WITHOUT INCIDENT.  MAINTENANCE REPLACED RT INBOARD SYNCHRONIZER.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
RIC - FLT 976 - AFTER DEPARTURE, CREW RECEIVED A RT GEAR DOOR RETRACTION WARNING INDICATING GEAR DOOR DID NOT RETRACT.RECYCLED GEAR, NO CORRECTION.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE ACCOMPLISHED GEAR SWING.  CHECKED ALL LINKAGE AND PROXIMITY SWITCHES ON RT MLG DOOR.  ACCOMPLISHED BITE TEST.  MAINTENANCE COULD NOT DUPLICATE PROBLEM.  (X)


REMARKS:
CMH - FLT 717 - DURING FLIGHT, FIRST OFFICER'S OUTER PANE WINDSHIELD BEGAN TO CRACK.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD PER MM 56-10-00 AND MM 30-41-00.  ALL CHECKS NORMAL. (X)


REMARKS:
CLT - FLT 1998 - ON CLIMB-OUT, DUCT OVERHEAT LIGHT ILLUMINATED.  IT EXTINGUISHED ON DESCENT WHEN POWER WAS REDUCED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 1 ENGINE FIREWALL HP SEAL.  ALL CHECKS NORMAL.  (X)


REMARKS:
DAY - LOW LEVEL EMERGENCY LIGHTS FOUND INOPERATIVE.  MAINTENANCE REPAIRED CORRODED AND BROKEN WIRES BENEATH ROW 8 AT SEAT TRACK.  ALL EMERGENCY LIGHTS CHECK NORMAL.  (X)


REMARKS:
RIC - FLT 546 - IN CRUISE, RT ENGINE ANTI-ICE INDICATES 40 PSI WITH THE ENGINE ANTI-ICE SWITCH IN AUTO OR OFF.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED RT ENGINE NR 2 ANTI-ICE VALVE.  ALL CHECKS NORMAL.  (X)


REMARKS:
TYS - FLT 504 - DURING FLIGHT, CARGO DOOR WARNING LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE OPENED AND CLOSED CARGO DOORS.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
GSO - DURING T-CHECK, EDDY CURRENT INSPECTION FOUND 2 MM CRACKS IN LT AND RT NR 2 WINDOW POST IN RADIUS.  REPAIRED PER TYPICAL REPAIR 53-10-01A.  (X)


REMARKS:
CLT - FLT 872 - AFTER TAKE-OFF, MAIN LANDING GEAR WARNING LIGHT ILLUMINATED.  CYCLED GEAR, LIGHT WOULD NOT EXTINGUISH.AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED RT GEAR DOOR SEQUENCE VALVE.  ALL CHECKS NORMAL.  (X)


REMARKS:
CLT - FLT 391 - AFTER TAKE-OFF, STARTER VALVE LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED STARTER VALVE ASSEMBLY.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
DURING S.I.P. VISIT AND ACCOMPLISHING S.I.P. 53-10-19, FOUND 2 EACH, 2 INCH CRACKS IN THE NOSE LANDING GEAR WHEEL WELL SIDE WALL AT STA 2650 (MM) AND STA 3050 (MM).  REMOVED DAMAGED AREA AND INSTALLED DOUBLERS PER SRM 53-11-00 AND EA NR 26044.  (X)


REMARKS:
DCA - MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED THE POWER UNIT AND INVERTER FOR THE FWD EMERGENCY LIGHTS AT THE ENTRANCE DOOR, SERVICE DOOR AND ALONG THE FWD CLOSET.  ALL LIGHTS CHECK NORMAL.  (X)


REMARKS:
AT EWR, ON TAXI OUT, FLT NR 7 EWR TO ATL NR 2 GEN FIELD TRIP A FEW SECONDS AFTER ENGINE START.  UNDER VOLTAGE NR 2 SYSTEM ILLUMINATED.  REMOVED AND REPLACED NR 2 VOLTAGE REGULATOR PER MM 24-20-0.  OPS CHECK NORMAL.  (Z)


REMARKS:
NR 2 ENGINE SN 657089 INJESTED FOD, DAMAGING C-1 AND C-2 BLADES ON REPOSITION FLIGHT TO LAKE CITY, FL.  TEAM FROM AEROTHRUST (MIAMI) DISPATCHED TO LAKE CITY, FL, BLENDED C-1 BLADES AND REPLACED C-2 FAN ASSEMBLY SN 4B0047 (ON) PN 759942 (ON).


REMARKS:
EWR - FLT 17 - ON PUSHBACK, NR 2 HYD B-PUMP FAILED ON TAXI OUT.  REMOVED AND REPLACED NR 2 B-SYSTEM ELECTRIC PUMP PER MM 29-11-11.  OPS CHECKED AND LEAK CHECKED OK.  (W)


REMARKS:
EWR - ON PUSHBACK, FLT 21, NR 3 ENGINE WOULD NOT LIGHT OFF DURING START.  REMOVED AND REPLACED HI ENERGY IGN SW S306 FOR NR 3 ENGINE.  REMOVED AND REPLACED NR 3 EXCITER BOX PER MM 74-31-13.  OPS CHECK OK.  (W)


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN FORWARD SERVICE DOOR ATTACH ANGLE, FORWARD END OF NR 1 HORIZONTAL BEAM.  REPAIRED PER DRAWING 9911579.  AIRCRAFT TOTAL CYCLES 74,615.


REMARKS:
MCI - DURING OP-16 FOUND RT FRAME AND DOUBLER BROKEN BETWEEN STRINGER 24R CUTOUT AND AILERON CABLE CUTOUT, IN CABIN A-ZONE, STA 380.  REPAIRED PER ARA 8059 AND SRM 51-30-02.  TOTAL CYCLES 17,042.


REMARKS:
MCI - DURING OP-16 FOUND LT FRAME AND DOUBLER BROKEN BETWEEN STRINGER 24L CUTOUT AND AILERON CABLE CUTOUT, IN CABIN A ZONE, STA 380.  REPAIRED PER ARA 8058 AND SRM 51-30-02.  TOTAL CYCLES 17,042.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A 1.25 INCH CRACK IN NR 1 HORIZONTAL FORWARD SERVICE DOOR END RADIUS, OUTBD SIDE.  REPLACED PER DRAWING 9911579.  AIRCRAFT TOTAL CYCLES 74,615.


REMARKS:
SFO - FLT 294 - RETURNED FROM FLIGHT ACCOUNT NR 2 ENGINE FIREWARNING INDICATION THAT CEASED WITH THROTTLE RETARDED.  FOUND RUPTURED PNEUMATIC WYE SUPPLY DUCT.  REPLACED DUCT, MFG PN 65-26738-21.  OPS CHECKS NORMAL.  CHECK C-4 7-10-93, MCI.


REMARKS:
STL - DURING C-CHECK, FOUND A .75 INCH CRACK IN LONGERON 3L, STAL 160 160.  REPAIRED LONGERON PER SRM 53-02, FIGURE 2, AND DRAWING SRO 9530128.  AIRCRAFT TOTAL CYCLES 71,420.


REMARKS:
STL - DURING C-CHECK, FOUND A ,1250 INCH CRACK IN LONGERON 6L, STA 756.  REPAIRED LONGERON PER SRM 53-02, FIGURE 2.  TOTAL CYCLES 71,420.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 216, WL 234 UNDER CAPTAIN'S NUMBER 2 WINDOW.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 639, LEFT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS  807, STR 10R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGERS DAMAGED AT BS 420, STR 23L AND 25L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 6L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 034, DURING DESCENT, FLIGHT ATTENDANT NOTED SMOKE AND ELECTRICAL SMELL AT AFT GALLEY COFFEEMAKER.  GALLEY POWER TURNED OFF AND COFFEEMAKER CIRCUIT BREAKER PULLED.  AIRCRAFT LANDED WITHOUT INCIDENT.  REPLACED COFFEEMAKER.


REMARKS:
FLIGHT 758, FOUND EMERGENCY EXIT LIGHTS AT ROW 11 INOP.  REPLACED LIGHT ASSEMBLY.


REMARKS:
FLIGHT 633, FORWARD GALLEY DOOR ESCAPE SLIDE ACCIDENTALLY DEPLOYED.  REPLACED SLIDE ASSEMBLY PER BOEING M/M.


REMARKS:
STL - FLT 560 - WHEN LANDING GEAR WAS EXTENDED FOR LANDING, A-HYDRAULIC SYSTEM HAD LOSS OF FLUID.  EXTENDED LANDING GEAR WITH ALTERNATE SYSTEM.  FOUND NOSE GEAR LOCK ACTUATOR HOUSING CRACKED.  REPLACED ACTUATOR, MFG PN 65-40467-6, BOTH ENGINE DRIVEN HYDRAULIC PUMPS, AND FILTERS.  OPS CHECKS NORMAL OP-17, 1-17-94, MCI.


REMARKS:
EWR - FLT 11 - EWR TO ATL, ON TAXI OUT, OUTBD FLAP INDICATED SPLIT AT 2 DEGREE POSITION ON EXTENSION.  REMOVED AND REPLACED RT OUTBD FLAP TRANSMITTER AND CANNON PLUG AS PER MM 27-52.  OPS CHECK OK.  (W)


REMARKS:
EWR - PREFLIGHT WALK AROUND, FLT NR 9 EWR TO MCO, FOUND HOLE RT SIDE FUSELAGE SKIN AT STATION 1091, R W/L 177, 1.5 INCHLONG, .75 INCH WIDE.  REPAIRED HOLE AT STATION 1091, RT W/L 177 AS PER SRM 53-30-3 PAGE 14A.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK VERTICAL ANGLE BS 727 BL0.  REPAIRED PER SRM 51-10-01. (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH CORROSION Z-ANGLE AT AFT ENTRY DOOR.  CORROSION TASKNR C53-107-01, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 910-926, BETWEEN STRINGERS 21 AND 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AND GOUGED FROM BS 358 TO 380, BETWEEN STRINGERS 3L AND 5L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
MCI - DURING OP-17 FOUND CORROSION IN FORWARD CARGO BIN FUSELAGE SKIN BETWEEN STRINGER 26L AND 26R, STA 685.  REMOVED CORROSION PER SRM 51-10-01 AND REPAIRED SKIN PER SRM 53-30-3, FIGURE 12 AND STANDARD PRACTICES.  TOTAL CYCLES 22,738.


REMARKS:
MCI - DURING OP-17 FOUND .5 INCH CRACK IN FORWARD CARGO BIN FORMER AND DOUBLER, STA 580, STRINGER 25L.  REPAIRED PER SRM 51-40-3, FIGURE 1.  TOTAL CYCLES 22,738.


REMARKS:
MCI - DURNG OP-17, FOUND FORWARD CARGO BIN FUSELAGE SKIN CORRODED BETWEEN STA 480 AND STA 500, OUTBD SIDE OF STRINGER 28R.  REMOVED DAMAGED SKIN AND REPAIRED PER SRM 53-30-3, FIGURE 3A.  TOTAL CYCLES 22,738.


REMARKS:
PHL - FLT 191 - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO OIL FILTER BYPASS LIGHT ILLUMINATING.  ACCOMPLISHED UNSCHEDULED LANDING.  FOUND ENGINE OIL FILTER FULL OF METAL PARTICLES.  REPLACED ENGINE SN 3903.  ENGINE TOTAL TIME 56,563 HOURS, 39,619 CYCLES.  CHECK C-2, 2-13-94, MCI.


REMARKS:
STL - DURING C-CHECK, FOUND A ONE-INCH CRACK IN SERVICE DOOR OPENING AT NR 1 BEAM WHERE HINGE IS SECURED.  REPLACED BEAM PER DOUGLAS DRAWING 9911582.  AIRCRAFT TOTAL CYCLES 79,160.


REMARKS:
STL - DURING C-CHECK, FOUND A ONE INCH CRACK IN NR 2 BEAM OF SERVICE DOOR AT SKIN FLANGE UPPER HINGE.  REPLACED BEAM PER DOUGLAS DRAWING 9911580.  TOTAL CYCLES 79,160.


REMARKS:
STL - DURING OP-15 FOUND .5 INCH CRACK AT LOWER ATTACH POINT OF VERTICAL SUPPORT UNDER OUTBD SEAT TRACK, STA 680.  REPLACED VERTICAL SUPPORT BEACKET PER SRM 53-30-5.  TOTAL CYCLES 71,163.


REMARKS:
STL - DURING C-CHECK, FOUND A 1.5 INCH CRACK IN LOWER RT CORNER OF BULKHEAD SKIN.  REPAIRED PER DRAWING JO 60088 AND SB53-137.  TOTAL CYCLES 29,969.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND DAMAGE TO LT FUSELAGE, STA 720-720A, STRINGERS S20 AND S21.  REPAIRED PER SRM 53-30-3, FIGURE 1, SHEET 4.  TOTAL CYCLES 32,233.


REMARKS:
REMOVING BELLY SKIN TO COMPLY WITH RD 90-06-09 FOUND STRINGER CORRODED BEYOND LIMITS.  FOUND MOISTURE INSIDE SKIN.  DRAIN HOLES MIGHT HAVE BEEN PLUGGED.


REMARKS:
ATL - NR 1 ENGINE NOSE COWL DAMAGED WHILE CLEANING A/C.  DAMAGE WAS AT 11 O'CLOCK, PUNCTURE LESS THAN .25 INCH.  INSPECTED NR 1 ENGINE NOSE COWL AND REPAIRED DAMAGE IAW SRM 54-30-3, PAGES 6, 7, AND 8.  INSPECTED, OKAY FOR SERVICE.  (X)


REMARKS:
DURING FC-5 INSPECTION, FOUND 2 INCH CRACK RT FRONT KEEL BEAM SIDE PLATE AFT SIDE OF FORWARD PRESSURE BULKHEAD.  STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER USAIR EA 25497.  (W)


REMARKS:
DURING FC-5 INSPECTION, FOUND 5 INCH CRACK IN FORWARD PRESSURE BULKHEAD AFT LOWER CONNECTION ANGLE BETWEEN STRINGERS 3 AND 72.  VISUAL/EDDY CURRENT INSPECTION.  STOP DRILLED CRACK ON INSTALLED TWO REPAIR DOUBLERS PER SRM 53-11-00.  (W)


REMARKS:
MSY - FLT 1473 - ON CLIMB-OUT, RECEIVED NR 1 CSD HIGH OIL TEMPERATURE INDICATION AND HIGH OIL TEMPERATURE ON TEMPERATURE GAUGE.  APU ON MEL.  FLIGHT RETURNED TO MSY WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 1 CSD AND OILCOOLER.  NR 1 CSD OIL TEMPERATURE INDICATOR AND CSD FILTER HOUSING.  ALSO, MAINTENANCE REPLACED APU LOP SWITCH AND CLEARED APU MEL.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES WIDE 4 INCHES LONG BS 1006 STR 27R.  REPAIRED PER SRM 51-10-01.  (W)


REMARKS:
INT - DURING Q-2 VISUAL INSPECTION, FOUND 1.5 INCH BY 3 INCH CORROSION BS 967- BS 987 S -26R.  REPAIRED PER SRM 53-10-03.  (W)


REMARKS:
INT - DURING Q-2 VISUAL INSPECTION, FOUND 30 INCH GOUGE ALONG SIDE OF FUSELAGE SKIN.  BS 360-400 S 18R S 19R.  REPAIREDPER SRM 53-30-3.  (W)


REMARKS:
INT - DURING Q-2 VISUAL INSPECTION, FOUND 2 CRACKS 1.25 INCH AND 2.5 INCH 30 INCHES BOTTOM LBL 8 INCHES BS 178 BULKHEAD.  REPAIRED PER TR 53-10-11.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL AND HFEC INSPECTION, FOUND 1.5 INCH CRACK AND 1 INCH CRACK BS 178 BULKHEAD AFT SIDE 20 INCHES FROM BOTTOM AND 30 INCHES FROM BOTTOM RBL 6 INCHES.  REPAIRED PER TR 53-10-11.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT TRANS ANGLE ATTACH HOLE ON BODY FRAME, BS 420 FRAME AT S-26L.  REPAIRED PER TR 51-40-3.  (W)


REMARKS:
INT - DURING Q-2 EDDY CURRENT CHECK INSPECTION, FOUND CRACK APPROXIMATELY.8750 INCH LONG OUTBD ROW OF LOWER FASTENER'S LT PIVOT BRACKET, W/L 278 (1156 BULKHEAD).  REPAIRED PER EO 5391G569.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND LIGHT SURFACE CORROSION AT SCREW HOLE, INTERCOSTAL BS 288 LBBL 12.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT - DURING Q-2 CHECK EDDY CURRENT INSPECTION, FOUND APPROXIMATELY .5 INCH LONG CRACK RT PIVOT BRACKET OUTBD LOWER ROWOF FASTENERS W/L 278, (1156 BULKHEAD).  REPAIRED PER EO 5391G569.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH AND 1 INCH BY 6 INCH CORROSION AT BS 983 THROUGH BS 1083 STR 27R.  REPAIRED PER SRM 53-10-3, FIGURE 1.  (W)


REMARKS:
PIT - THE EMERGENCY LIGHT AT SEAT 13R REMAINED ON AFTER TEST.  MAINTENANCE REPLACED THE LIGHT ASSEMBLY, OPS CHECKED GOOD.  (W)


REMARKS:
LGW - FLT 0195 - THE FLOOR PROXIMITY LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 1 THROUGH 4.  MAINTENANCE SWAPPED THE BATTERY PACK WITH THE R1 ESCAPE SLIDE LIGHT.  THE FLIGHT THEN PROCEEDED TO BALTIMORE.  BALTIMORE MAINTENANCE REPLACED THE BATTERY PACK FOR THE R1 ESCAPE SLIDE LIGHT.  (W)


REMARKS:
LGW - DURING ROUTINE CHECK, THE EMERGENCY FLOOR PROXIMITY LIGHTS, ROWS 10-14 AND THE EXIT IDENTIFIER LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE FOUND A CUT CABLE AT ROW 14 AND REPAIRED IT WITH RED RAYCHEM SPLICES.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION  FOUND 1 INCH BY 24 INCH CORRODED AFT RT GALLEY ENTRY Z-ANGLE.  REPAIRED PER SRM 53-10-01.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION  FOUND 2 INCH CRACK BS 664 RBBL 24.  REPAIRED PER EO 5791G632 AND EO 5974G046. (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION  FOUND 1.5 INCH CRACK BS 664 LBBL 24.  REPAIRED PER EA 37147.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND 1 INCH BY 3 INCH AREA CORRODED AND 3 SCREW HOLES CORRODED BS 986.5-1016 8 INCH RBL.  REPAIRED PER SRM 51-10-01.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION  FOUND 1 INCH BY 1INCH CORRODED AREA 5 SCREW HOLES BS 986.5-1016 24 INCHES RBL.  REPAIRED PER SRM 53-10-01.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK CARGO FLOOR SUPPORT STRINGER BS 490 ABOVE S27R.  REPAIRED PER SRM 53-10-05.  (W)


REMARKS:
LGA - FLT 485 - UNABLE TO PRESSURIZE ARICRAFT AFTER TAKEOFF, ALONG WITH AFT CARGO DOOR WARNING LIGHT.  FLIGHT RETURNED TO LGA WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE RECLOSED DOOR.  FLIGHT RETURNED TO GATE DURING TAXI OUT FOR SAME PROBLEM.  MAINTENANCE FOUND REAR CARGO DOOR HANDLE OVERCENTER SPRING BROKEN.  REPLACED SPRING.  OPS NORMAL.  (X)


REMARKS:
STL - FLT 171 - AFTER TAKEOFF ON LANDING GEAR RETRACTION, NOSE GEAR UNSAFE INDICATION LIGHT REMAINED ON UNTIL GEAR HANDLE WAS RECYCLED.  ADJUSTED UP POSITION PROXIMITY SENSOR, MFG PN 8-337-03.  OPS CHECK NORMAL.  CHECK C-1A, 4-6-94, MCI.


REMARKS:
PBI - FLT 479 - DURING CRUISE, SHUT DOWN NR 3 ENGINE DUE TO VIBRATION AND OIL FILTER BYPASS LIGHT ILLUMINATION.  FOUND OIL IN TURBINE AND METAL PARTICLES IN OIL FILTER.  REPLACED ENGINE SN 1534.  GROUND RUNUP OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME 29,957, 19,686 CYCLES.  CHECK C-2, 9-27-93, MCI.


REMARKS:
STL - DURING OP-15 FOUND CORROSION ON FORWARD CORNER OF SERVICE DOOR FRAME PAN.  REPAIRED PER SRM 53-05, FIGURE 55.  AIRCRAFT TOTAL TIME 64,683, 71,163 CYCLES.


REMARKS:
STL - DURING OP-15 FOUND CORROSION AT FORWARD SERVICE DOOR JAMB, EXTERNAL SKIN AND INTERNAL STRUCTURE, STA 168, LONGERON 18R.  REPAIRED PER SRM 53-05, FIGURE 55.  AIRCRAFT TOTAL TIME 64,683, TOTAL CYCLES 71,163.


REMARKS:
PIT - FLOOR TRACK EMERGENCY LIGHTING ROWS 11 THROUGH 18 INOPERATIVE.  MAINTENANCE REPLACED FORWARD CHARGER ASSEMBLY ANDBATTERY.  (W)


REMARKS:
CLT - FLT 1805 - NR 1 ENGINE A-SYSTEM HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON AS THE GEAR WAS RAISED AND REMAINED ON.FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 1 ENGINE A-HYDRAULIC PUMP, CASE DRAIN FILTER, PRESSURE FILTER, AND RETURN FILTER.  (W)


REMARKS:
DCA - FLT 1180 - ON APPROACH, WHEN LANDING GEAR LOWERED ALL THREE LIGHTS SHOWED RED AND GREEN.  RECYCLED GEAR, ALL LIGHTS GREEN.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED M-986 CARD.  PERFORMED OPS CHECK, OPS CHECK NORMAL.  (W)


REMARKS:
BOS - FLT 1999 - RETURN TO FIELD DUE TO A BURNING SMELL AND SMALL AMOUNT OF SMOKE IN THE COCKPIT.  MAINTENANCE FOUND THE AC BREAKER FOR THE SPOILER DEFECTIVE.  THE CIRCUIT BREAKER WAS REPLACED.  (W)


REMARKS:
DURING CLIMB, NR 1 ENGINE S/N 3237, SPOOLED DOWN.  SHUT DOWN NR 1 ENGINE AND MADE UNSCHEDULED LANDING.  FOUND TURBINE DAMAGE.  REPLACED ENGINE.  GROUND RUNUP AND OPERATION CHECKED NORMAL.


REMARKS:
ATL-PBI - FLT 61 - GEAR UPLATCH CHECK COULD ONLY BE ACCOMPLISHED WITH GEAR HANDLE RELEASE BUTTON PULLED OUT A BIT AND WITH HIGHER THAN NORMAL HANDLE DOWNFORCE.  FLIGHT RETURNED TO ATLANTA.  CYCLED GEAR HANDLE, CHECKED CABLES AND LINKAGE FROM HANDLE TO SELECTOR VALVE, OPS CHECK GOOD IAW MM 32-31, NO DEFECTS NOTED.


REMARKS:
STL - FLT 534 - AFTER TAKEOFF, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR, LIGHT REMAINED ILLUMINATED.  FOUND NOSE GEAR UPLOCK SENSOR, MFG PN 8-337-03, DEFECTIVE.  REPLACED UPLOCK SENSOR AND NOSE LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL.  CHECK C-2B 3-13-94, MCI.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 294.5, RBL 43, WL 208.  REPLACED PER SWARA 1-353-418.


REMARKS:
AFTER TAKEOFF, AFT CARGO DOOR OPEN WARNING LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPAIRED AFT CARGO DOOR LANYARD AND PROPERLY CLOSED DOOR.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BEARSTRAP DAMAGED AT BS 797, S25R.  REPAIRED PER TRAMCO EWO 94-0375.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN FRONT SPAR CHORD LEFT SIDE CRACKED AT FS 246.7.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO DOOR FRAME CRACKED UNDER FORWARD LOWER DOORWAY STOP, BS 440.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND RIGHT WING LOWER RIB CHORD CRACKED BETWEEN S2 AND S3R, WL 135.5 AND LEFT CHORD CRACKED AT BS 178 BULKHEAD.  REPAIRED PER SWA ACO 587-57 AND TRAMCO EWO 94-033.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, S26R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1080, S22 AND 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CORNERS OF HORIZONTAL STABILIZER CUTOUT UPPER AND LOWER HORIZONTAL BEAM CORRODED, BS 1138.  REPAIRED PER SWA ACO 6035-53.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CRACKED AT RIGHT O/B FLANGE AT S27R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD SKIN CRACK AT BS 178, RBL 10 R.  REPAIRED PER SWA EWO 94-0325.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 976, BETWEEN S22 AND 24L, AT BS 1024, S17L, AT 960, S22L,  AND AT BS 922, S22L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, S6R, AT BS 360, S11L, AND AT BS 767, S4R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGED AT BS  340, S16R AND AT BS 727B, S9L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEBS CRACKED AT BS 727 TO 727.4, LBL 20, WL 176 AND AT BS 695, WL 206, LBL 55.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 400, S21L, WL 180.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGERS CRACKED AT LEFT AND RIGHT WING L/E LIGHT SUPPORTS.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM SUPPORTS CORRODED AT BS 967-987, LBL 18. WL 208, AT BS 727-947, LBL21.5, WL 153 , AT BS 987-1016, LBL 20-13, WL 208, AT BS 997-1016, LBL 38, WL 208 AND AT BS 727-947.5, RBL 21.5, WL 153. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORROSION AT BS 967, RBL 43 AND AT BS 294.5, LBL 22, WL208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM  CORROSION AT BS 1006, RBL 37 TO LBL 37, WL 208, AT BS 344, LBL 11-52, WL 208 AND AT BS 1016, RBL 37 TO LBL 37, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND WEBS UNDER SEAT TRACK CORRODED AT BS 986-1016, RBL 37, WL 208 AND AT BS 1016, RBL 27, WL 208.  REPAIRED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORDS CORRODED AT BS 360, LBL 30 TO 65, WL 208, AT BS 987, LBL 42, WL 208, AT BS 312, LBL 18 TO RBL 3, WL 208 AND AT BS 859, LBL 12-RBL 3, WL 164.  REPAIRED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 277, WL 208, LBL 30-55.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
STL - INVESTIGATION INTO ENGINE SHUTDOWN DUE TO OIL FILTER WARNING LIGHT ILLUMINATION REVEALED THE NR 3 BEARING, MFG P/N 810641, FRACTURED RELEASING METAL PARTICLES INTO OIL SYSTEM.  ENGINE S/N 4629 WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
PIT - FLT 0675 - THE RIGHT LANDING GEAR LIGHT DID NOT ILLUMINATED WHEN THE LANDING GEAR WAS LOWERED.  THE GEAR WAS RECYCLED THREE TIMES BUT THE LANDING GEAR LIGHT STILL DID NOT APPEAR.  THE AIRCRAFT WAS THEN PUT INTO 25 DEGREE FLAP CONFIGURATION TO CHECK THE WARNING HORN DISAGREEMENT.  AT THIS TIME THE LANDING GEAR LIGHT APPEARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE PERFORMED BITE CHECK OF THE PSEU.  NO FAULTS WERE NOTED.  THE SOCKET WAS THEN RELAMPED.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
TPA - FLT 1933 - NOSE GEAR WOULD NOT RETRACT ON TAKEOFF.  FLIGHT RETURNED TO TPA AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND NOSE GEAR PIN INSTALLED.  REMOVED PIN.  OK FOR SERVICE.  (Z)


REMARKS:
WEATHER RADAR INDICATOR WENT BLANK.  AIRCRAFT DIVERTED TO MEM DUE TO WEATHER CONDITIONS AND MADE AN UNEVENTFUL LANDING. REPLACED R/T UNIT PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND MLG STRINGER RIGHT 18A SHEAR BEAM AT AFT END ATTACH TO BS 727 CRACKED.  REPAIRED PER SWA RA 1-353-1093.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD CARGO DOORWAY FORWARD FRAME CRACKED AT LOWER UPPER CORNER OF BOTTOM STOP FITTING.  REPAIRED PER SWA RA 1-353-1094.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD SERVICE DOORWAY AT BS 290-293, RBL 55 ANGLE CLIP O/B OF Z ANGLE CRACKED AT FORWARD DOOR POST.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD SERVICE DOORWAY AT BS 290.5, FORWARD FRAME CRACKED AT INBOARD RADIUS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD SERVICE DOORWAY  L ANGLE CRACKED AT BS 287, BELOW S12R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM UPPER FLANGES CRACKED AT BS 520, RBL 45.5, RBL 24.75, AND LBL 24.75.  REPAIRED PER SWA ACO 3198-53 AND RA 1-353-1095.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 10R CLIP AT BS 663 CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND SEAT TRACK SUPPORT CHANNELS CRACKED AT UPPER CORNERS, BS 520, RBL 24.75 AND 45.5.  REPLACED PER SWA ACO 3198-53.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND BELTFRAME INBOARD CHORD CRACKED AT LOWER CORNER, BS 613 LEFT.  REPAIRED PER SWA RA 1-353-1096.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAMS CORRODED AT BS 986.5, BS 1016, RBL 10, RBL 16.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 14.  REPAIRED PER SWA RA 1-353-1102.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORRODED AT BS 968, RBL 28.5.  REPAIRED PER SWA RA 1-353-1099.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM T CAP CORROSION AT BS 986.5, LBL 10.75.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM FORWARD FLANGE CORROSION AT BS 947, RBL 2.  REPAIRED PER SWA RA 1-353-1097.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND CHORD ANGLE CRACKED AT L/H RAM AIR INLET, BS 540, S23L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 45 - LBL 45, WL 208.  REPLACED PER SWA RA 1-353-542 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LEFT SIDE VERTICAL FIN GOUGED AND DENTED AT FS 274.3, 3 INCH AFT OF L/E.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0382.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 887, LBL 27 TO 48, WL 120 TO 160.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 320, WL 172 AND AT BS 76.5, RBL 28, BETWEEN S25R AND 24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, UPPER CHORD, RBL 33.  REPAIRED PER SWA RA 1-353-418 R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, S27L, LBL 12.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 359, S15L, WL 122 AND AT BS 927, S24L, WL 161.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, WL 208, LBL 30-55.  REPLACED SWA RA 1-353-418.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 26R CORRODED AT BS 500B, WL 150.  REPLACED BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 9-49, WL 208.  REPAIRED PER SWA  RA 1-353-427.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 294.5, LBL 11, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AT GATE, APU EXPERIENCED FAILURE.  REPLACED APU ASSEMBLY,  ISOLATOR MOUNTS, TAIL PIPE ASSEMBLY, BLEED AIR DUCT AND  REPAIRED HOLE IN LOWER APU SHROUD.


REMARKS:
FLIGHT 018, IN FLIGHT, LOST  A-SYSTEM HYDRAULIC PRESSURE.  AIRCRAFT LANDED AT HOUSING HIGH ENERGY STOPPING PROCEDURES.REPLACED NUMBER 6 SPOILER ACTUATOR.  PERFORMED HIGH ENERGY STOP AND BRAKE SEIZURE CONDITION INSPECTION.  REPLACED ALL FOUR MAIN GEAR WHEELS AND BRAKES.


REMARKS:
DURING SCHEDULED QUARTER CHECK, FOUND FUSELAGE SKIN CRACKED AT FORWARD ENTRY DOORWAY.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM FORWARD FLANGE CORRODED AT BS 986, RBL 10 TO 47 AND AT RBL 42 TO 45.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM TOP SURFACE CORRODED AT BS 360, RBL 1, 12, AND 19.  REPAIRED PER SWA RA 1-253-1115.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM T-CAP CORRODED  AT BS 294, LBL 21 TO 47.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND U-CHANNEL SUPPORT UNDER LAV BULKHEAD CORRODED AT LBL 11 BETWEEN BS 270 AND 284.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM UPPER AFT FLANGE CORRODED AT BS 360, LBL 10.75.  REPAIRED PER SWA RA 1-253-1115.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM UPPER AFT FLANGE CORRODED AT BS 344, LBL 0.  REPAIRED PER SWA RA 1-253-426.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, BL 0.  REPAIRED PER SWA RA 1-253-426.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM AFT FLANGE CORRODED AT BS 312, LBL 11.5 TO RBL 21.  REPAIRED PER SWA RA 1-253-420.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND AFT ENTRY DOOR TOP HINGE CUTOUT SKIN CRACKED 2 PLACES.  REPAIRED PER SWA RA 1-253-1114.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 328, FORWARD FLANGE, RBL 14 TO 49.  REPAIRED PER SWA RA 1-253-1116.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 328, AFT FLANGE, UPPER AND LOWER SURFACES, RBL 19.  REPAIRED PER SWA RA 1-253-1117.


REMARKS:
DURING SCHEDULED 1/4 CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 328, AFT FLANGE,  LBL 11.  REPAIRED PER SWA RA 1-253-1118.


REMARKS:
DURING CLIMB-OUT, ALL L/E SLATS WOULD NOT FULLY RETRACT.  AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING.  REPLACED SLAT RETRACT HYDRAULIC FUSE.


REMARKS:
DURING CLIMB-OUT, EXPERIENCED BIRDSTRIKE TO NUMBER 2 ENGINE.  AIRCRAFT DIVERTED TO CLE AND MADE AN UNEVENTFUL LANDING.ACCOMPLISHED BIRD STRIKE INSPECTION WITH DAMAGE TO NOSE COWL NOTED.  REPLACED ENGINE NOSE COWL PER BOEING M/M.  PERFORMED BORESCOPE INSPECTION, NO DEFECTS NOTED.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM WEB CRACKED AT BS 708, LBL 24, WL 204.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 847, S16L, BS 827, S15 AND 16L, AND AT BS 663.75, 10 L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, S19L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
LGA - FLT 1570 - RETURN TO FIELD DUE TO SMOKE IN THE COCKPIT.  MAINTENANCE FOUND THE SMOKE TO BE CAUSED FROM GLYCOL INGESTION.  PAX BURN OUT PROCEDURE WAS PERFORMED.  (Z)


REMARKS:
ATL - FLT 115 - AFTER TAKEOFF, MAIN ELECTRIC STABLIZER TRIM DID NOT RESPOND TO INPUTS THEN RUNAWAY NOSE DOWN.  CRUISE TRIM RESPONDED BACKWARDS.  REPLACED MAIN ELECTRIC AND CRUISE TRIM ACTUATORS, MFG  PN'S R1631MI AND 36024-003.  OPS CHECK NORMAL.  CHECK C-1, 8-27-93, MCI.


REMARKS:
DEN - FLT 457 - AFTER TAKEOFF LT RUNWAY TURNOFF LIGHT SWITCH OVERHEATED EMITTING ODOR AND SMOKE.  OPENED TURNOFF LIGHT CIRCUIT BREAKER, ODOR AND SMOKE DISSIPATED.  FOUND SWITCH, MFG PN A3-1219, CONTACTS STUCK.  REPACED LT RUNWAY TURN OFF LIGHT SWITCH AND RELAMPED LIGHT AND OPERATION CHEKCED NORMAL.  OP-17, 5-1-94, MCI.


REMARKS:
STL - DURING C-CHECK, FOUND CORROSION IN FUSELAGE SKIN, STA 993, LONGERON 26L.  REPAIRED PER SRM 51-10-3, AND STANDARD PRACTICES.  TOTAL CYCLES 76,528.


REMARKS:
STL - RETURNED FROM FLIGHT ACCOUNT ELECTRICAL ODOR AND SMOKE IN COCKPIT.  FOUND AUTO GROUND SPOILER ACTUATOR OVERHEATEDAND CIRCUIT BREAKER TRIPPED.  REPLACED ACTUATOR, MFG PN 1040T100-5.  OPS CHECKS NORMAL.  CHECK C-4, 12-15-93, STL.


REMARKS:
MCI - DURING OP-15 FOUND CORROSION AT RT AFT LAV FLOOR BEAM CAP, STA 996, RBL 41.  REPAIRED PER SRM 51-10-01 AND 53-05,FIGURE 20A.  TOTAL CYCLES 71,936.


REMARKS:
STL - DURING C-CHECK, FOUND FUSELAGE SKIN AND LONGERON 23L CORRODED AND FIVE RIVET DIMPLES, CORRODED AND CRACKED STA 945, LONGEORN 23L.  REPAIRED PER SRM 51-30-2 AND 53-02, FIGURE 2.  TOTAL CYCLES 76,528.


REMARKS:
PHL - FLT 1673 - FLIGHT WAS UNABLE TO MAINTAIN CABIN PRESSURE AT FL 250.  RETURNED TO PHL AND LANDED OVERWEIGHT AT 175,000.  MAINTENANCE FOUND THE RT PACK DUCT BLOWN AT MIX MANIFOLD.  REPLACED DUCT AND PERFORMED OVERWEIGHT LANDING INSPECTION.  RETURNED AIRCRAFT TO SERVICE.  (W)


REMARKS:
TPA - FLT 1875 - AFTER 45 MINUTES OF FLIGHT DURING DESCENT FROM 18,000 TO 10,000 FEET WITH THROTTLES IDLE, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED INTERMITTENTLY.  MAINTENANCE INSPECTED THE ENGINE STRUT FIRE LOOP AND WIRING AND PERFORMED LEAK CHECK OF ALL ASSOCIATED DUCTING.  THE OVERHEAT DETECTOR BOX WAS THEN REPLACED.  (W)


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT MLG W/W STRINGER 18A SHEAR BEAM AT AFT INBOARD FASTENER CRACKED FROM FASTENERTO T/E.  REPAIRED PER SWA RA 1-353-1111.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD GALLEY DOOR UPPER FORWARD FUSELAGE FRAME CRACKED AT BOTTOM OF UPPER STOP CASTING.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 30, AND 32.  REPAIRED PER SWA RA 1-353-1104.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CORROSION AT BS 967, LBL 5.5.  REPAIRED PER SWA RA 1-353-1107.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 14.5.  REPAIRED PER SWA RA 1-353-1108.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, LBL 11.  REPAIRED PER SWA RA 1-353-1106.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SEAT TRACK LINK SUPPORT CHANNELS CRACKED AT BS 520, RBL 24.75, 45.5, AND LBL 24.75,.  REPAIRED PER SWA ACO 3198-53 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM FLANGE RADIUS CRACKED AT BS 520, LBL 24.75, RBL 24.75 AND 45.5.  REPAIRED PER SWA ACO 3198-53 AND RA 1-353-1105.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FORWARD ENTRY DOORWAY  UPPER HINGE CUTOUT ON FORWARD FRAME CRACKED AT AFT END OF LOWER FORWARD SHEAR TIE WEB, BS 294.5, S10L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 400, APPROX LBL 71.5, WL 230.5.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD CRACKED AT BS 178, WL 235, RBL 10.  REPAIRED PER TRAMCO EWO 94-0455.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACK NOTED AT LH OB KEEL BEAM AFT OF SPLICE AT BS 727A.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 294, LBL 0, 7, 12, AND 23, WL 208.  REPAIRED PER TRAMCO EWO 94-0469 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AROUND NUTPLATES AT BS 987, LBL 5 TO RBL 40, WL 208.  REPAIRED PERSWA RA 1-253-465 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FAIL SAFE CHORD CRACKED AT BS 460, BETWEEN S20R AND S21R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD SIDE CHORDS LEFT AND RIGHT CRACKED AT BS 178, WL 195.  REPAIRED PER TRAMCO EWO94-0456 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 639, S17R, RBL 65.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 1 ENGINE PYLON FORWARD CORNER FRAME CHAFED.  REPLACED FORWARD CORNER FRAME PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM WEB CRACKED AT BS 716, RBL 24, WL 104-207. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED AT BS 967.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 10R CRACKED AT BS 787, 807, 827, AND  847.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, S15R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
SYR - FLT 449 - ON CLIMB-OUT FROM YUL, EN ROUTE TO PIT, ELECTRICAL PROBLEM OCCURRED.  FLIGHT DIVERTED TO SYR WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND NR 5 AND NR 6 MASTER CAUTION CIRCUIT BREAKERS POPPED.  RESET BREAKERS, REPLACED R-34 MASTER DIM RELAY AND MASTER DIM MODULE CONTROL CARD.  REFERENCE CONTROL NR USAA940500.  (W)


REMARKS:
MIA - FLT 1708 - AFTER TAKEOFF, THE LE FLAP INTRANSIT LIGHT WOULD NOT GO OUT.  FLIGHT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 LE EXTEND SWITCH, OPS CHECK NORMAL.  (W)


REMARKS:
INT - DURING 'SSI' DROP IN CHECK VISUAL INSPECTION FOUND A 1.5 INCH BY 3 INCH HOLE IN SKIN BETWEEN STR 18L PLUS 19L AT STA 1030.  REPAIRED PER SRM 53-30-3, FIGURE 1.  (W)


REMARKS:
LGW - THE FORWARD EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY CHARGER AND BATTERY.  OPS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 0146 - WITH THE EMERGENCY LIGHT SWITCH IN ARM POSITION, SOME OF THE EMERGENCY LIGHTS WERE ILLUMINATED ON THE REAR BULKHEAD DOOR.  MAINTENANCE REPLACED BATTERIES AT SEVERAL LOCATIONS.  (W)


REMARKS:
PIT - FLT 0096 - THE AFT LT EXTERIOR EMERGENCY DOOR LIGHT WAS INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK, OPS CHECKED GOOD.  (W)


REMARKS:
PHL - THE FLOOR LEVEL EMERGENCY LIGHTS FAILED TEST AT ROWS 9, 26, 1 AND 29.  MAINTENANCE REPLACED THE BATTERY PACK AT ROWS 9, 26, 1 AND 29.  ALL LIGHTS PASSED TEST.  (W)


REMARKS:
PHL - THE FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 FAILED TEST.  MAINTENANCE REPLACED THE BATTERY.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
MCI - FLT 29 - FLIGHT EN ROUTE IND TO LAX WHEN NR 2 ENGINE OIL QUANTITY WENT TO ZERO.  LOW OIL PRESSURE LIGHT CAME ON.CREW SHUT DOWN NR 2 ENGINE.  FLIGHT DIVERTED TO MCI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND INNER RT ANGLE GEAR BOX RADIAL DRIVE SHAFT INNER SHAFT HOUSING CRACKED.  REPLACED INNER AND OUTER SHAFT HOUSING.  (W)


REMARKS:
CLT - EMERGENCY LIGHTS IN OVERHEAD PANEL INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACKS.  (W)


REMARKS:
SYR - FLT 449 - ON CLIMB-OUT FROM YUL, EN ROUTE TO PIT, ELECTRICAL PROBLEM OCCURRED.  FLIGHT DIVERTED TO SYR WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND NR 5 AND NR 6 MASTER CAUTION CIRCUIT BREAKERS POPPED.  RESET BREAKERS, REPLACED R-34 MASTER DIM RELAY AND MASTER DIM MODULE CONTROL CARD.  REFERENCE CONTROL NR 94ZZZW2035.  (W)


REMARKS:
MCO - FLT 0536 - AIRCRAFT DIVERTED TO MCO DUE TO CIRCUIT BREAKERS ON THE CENTER TANK BOOST PUMPS NOT ABLE TO STAY RESET.  THE AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE REPAIRED WIRES IN THE RT WING ROOT.  ALL SYSTEMS CHECKED NORMAL.  (W)


REMARKS:
MIA - FLT 1869 - WHEN THE CREW TRIED TO EXTEND THE GEAR, THE NOSE WHEEL GEAR LIGHTS DID NOT UNLOCK.  THE CREW RECYCLED THE GEAR AND THE SAME PROBLEM AROSE.  A FLYBY WAS PERFORMED AND THE TOWER CONFIRMED THAT THE NOSE WHEEL DOORS WERE CLOSED.  THE CREW THEN FREE-FALLED THE NOSE GEAR AND LANDED NORMALLY.  MAINTENANCE CHECKED THE PRELOAD RIGGING IN THE NOSE LANDING GEAR DOOR.  THE DOOR WAS ALSO CHECKED FOR BINDING AND FREE PLAY.  OPS CHECKED GOOD.  (W)


REMARKS:
ATL/EWR - FLT 20 - ON TAXI OUT, NR 1 ENGINE START VALVE WOULD NOT OPEN ELECTRICALLY.  REMOVED AND REPLACED NR 1 ENGINE START VALVE.  LEAK CHECKED AND OPS CHECK OKAY PER MM 80-11-11.  (X)


REMARKS:
IAD - FLT 123 - INVESTIGATION INTO ENGINE SN 3237 SPOOLING DOWN REVEALED THIRD STAGE LOW PRESSURE TURBINE BLADE, MFG PN798403, FRACTURED, CAUSING TURBINE DAMAGE.  REPAIRED TURBINE INCORPORATING PW SB 5867.  ENGINE SN 3237 RETURNED TO SERVICE.


REMARKS:
TPA - FLT 1027 - DURING FLAP RETRACTION AFTER TAKEOFF, FORWARD AND OVERHEAD LE FLAP INDICATIONS ILLUMINATED.  NR 2 LE INDICATED EXTENDED.  FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED FLAP/SLAT ACCESSORY UNIT.  OPS CHECKED GOOD.  (W)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 380 TO 420, S15 - 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 071, DURING CLIMB-OUT, LOST B-SYSTEM HYDRAULIC PRESSURE.  AIRCRAFT DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING.  TROUBLESHOT AND FOUND RUPTURED OUTLET FLEX LINE FROM B SYSTEM PUMP TO B SYSTEM PRESSURE MODULE.  REPLACED LINE, CHECKED FILTERS AND SERVICED SYSTEM PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.6, STRINGER 24 AND 25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 384, STRINGER 19R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AROUND NUTPLATE HOLES AT BS 344, FROM RBL 4 TO LBLB 60, WL 208.  REPAIRED PER SWA RA 1-353-427.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CHORD CORRODED AT BS 986.5, FROM LBL 55 TO RBL 55.  REPLACED CHORD PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1092, STRINGER 12R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STRINGER 14R.  REPAIRED PER TRAMCO EWO 94-0468 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CORRODED AT BS 913, S27L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787, S20R AND S24R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU ACCESS DOOR AFT FRAME LONGERON CRACKED AT TWO PLACES.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 947, LBL 22, RBL 21, WL 208.  REPAIRED PER SWA RA 1-253-465.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT BS 492, STRINGER 25R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 26 TO RBL 26, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STRINGER 17L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D CHECK, FOUND INBOARD RIGHT FLOOR BEAM CORRODED AT BS 328, LBL 24.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D CHECK, FOUND WEB CRACKED AT TOP OF NOSE WHEEL WELL AT BL 0, AFT OF BS 227.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D CHECK, FOUND RIGHT FLOOR BEAM CORRODED AT BS 328, FORWARD GALLEY AREA.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP OVERHEAD AFT ENTRY DOOR.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
STL - DURING OP-9 FOUND A .5 INCH CRACK IN LOWER SIDE OF LONGERON 17R, STA 408.  REPAIRED PER SRM 53-02, FIGURE 2.  TOTAL CYCLES 29,368.


REMARKS:
STL - DURING OP-9 FOUND .5 INCH CRACK IN LOWER SIDE OF LONGERON 17R, STA 389.  REPAIRED PER SRM 53-02, FIGURE 2.  TOTALCYCLES 29,368.


REMARKS:
STL - DURING OP-15 FOUND CORROSION RT SIDE OF FLOOR BEAM WEB, STA 996.  CUT OUT CORROSION RT SIDE OF FLOOR BEAM WEB, STA 996.  CUT OUT CORROSION IN WEB, INSTALLED FILLER AND DOUBLER PER SRM 53-01, FIGURE 4, SHEET 3.  TOTAL CYCLES 71,163.  (W)


REMARKS:
STL - FLT 558 - ON LANDING GEAR EXTENSION, RT MAIN LANDING GEAR GREEN LIGHT DID NO ILLUMINATE.  CYCLED LANDING GEAR WITH SAME RESULTS.  REPLACED DOWN LIMIT SWITCH, MFG PN H14-1015.  OP CHECKS NORMAL.  CHECK C-6, 10-25-93, MCI.


REMARKS:
JFK - FLT 368 - AFTER TAKEOFF, RT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON WHEN GEAR RAISED.  INDICATION NORMAL WITH GEAR LOWERED.  CYCLED LANDING GEAR WITH SAME RESULTS.  REPLACED WORN SWITCH LINK BEARING, MFG PN C437A0250.  CHECK C-6, 10-15-93, STL.


REMARKS:
CLT - FLT 1172 - RETURN TO FIELD DUE TO A DUAL FLIGHT MANAGEMENT COMPUTER FAILURE.  MAINTENANCE RESET NR 1 AND NR 2 FMCCIRCUIT BREAKERS.  BITE TESTED NORMAL.  REPLACED FMC NR 1 AS A PRECAUTION.  (W)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, RBL 11 TO 55, WL 208.  REPLACED BEAM PER SWA RA 1-353-424 R3.


REMARKS:
DURING SCHEDULED D CHECK, FOUND LEFT HORZ STAB L/E RIB CRACKED AT STA.161.04.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 500, RBL 51, BETWEEN STRINGERS 22 AND 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND RIGHT KEEL BEAM CRACKED AT BS 727A AFT OF SPLICE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, S23R, WL 183.  REPLACED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER 25R CORRODED AT BS 867, WL 162.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, AT STRINGER 3R.  REPAIRED FRAME PER TRAMCO EWO 94-0465.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, AT STRINGER 2R.  REPAIRED FRAME PER TRAMCO EWO 94-0464.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 26R, JUST AFT OF AFT TOILET PANEL AT STA 1006, CORRODED AND CRACKED.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND GIRT BAR STRUCTURAL ATTACH PLATE CORRODED AT BS 312, LBL 62, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 907, S21 TO 22R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, BL O TO LBL 11, WL 208.  REPLACED FLOOR BEAM CHORD PER SWA RA 1-353-1 R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM DAMAGED BY DRILL START AT BS 947, WL 208, LBL 53.  REPLACED FLOOR BEAM UPPER CHORD PER SWA RA 1-353-542.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 6 FRAME AT APU ACCESS BENT AND CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CORROSION UNDER STRINGER 25L, BS 996, WL 180.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 20L GOUGED AT BS 727B.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 674, RBL 38, WL 202.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU AIR INLET STRUCTURE OPENING CORRODED AROUND ENTIRE SEAL MATING SURFACE AT BS 1120, RBL 21, WL 239.  REPAIRED PER BOEING DRAWING 65-46579.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP AT FIRST EIGHT ROWS.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD CABIN FLOOR TRACK LIGHTING INOP.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
DURING APPROACH, LEFT MAIN GEAR WOULD NOT FULLY EXTEND.  CYCLED LANDING GEAR HANDLE AND GEAR EXTENDED PROPERLY.  REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
CLT - FLT 1525 - ON CLIMB-OUT OF PIT, VIBRATION FELT ALONG LONGITUDINAL AXIS.  EN ROUTE PBI, GREEN NOSE GEAR LIGHT WOULD NOT TEST.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NOSE WHEEL BRAKE LINING AND NOSE GEAR LIGHT ASSEMBLY.  AIRCRAFT OK FOR SERVICE.  REFERENCE CONTROL NR USAA940481.  (W)


REMARKS:
CLT - FLT 1525 - ON CLIMB-OUT OF PIT, VIBRATION FELT ALONG LONGITUDINAL AXIS.  EN ROUTE PBI, GREEN NOSE GEAR LIGHT WOULD NOT TEST.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NOSE WHEEL BRAKE LINING AND NOSE GEAR LIGHT ASSEMBLY.  AIRCRAFT OK FOR SERVICE.  REFERENCE CONTROL NR 94ZZZW2100.  (W)


REMARKS:
PHL - THE INTERVALVE FLOOR LEVEL EMERGENCY LIGHT SYSTEM FAILED TEST AT ROWS 1 AND 9.  MAINTENANCE REPLACED THE BATTERIES AT ROWS 1 AND 9.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PHL - THE RT WING OVERWING EMERGENCY LIGHTS WOULD NOT TEST FROM NOSE GEAR.  MAINTENANCE REPLACED THE BATTERY CHARGER UNIT.  OPS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 1237 - FLIGHT EN ROUTE FLL TO PIT WHEN NR 2 ENGINE DEVELOPED A VIBRATION.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED BLADES 8 AND 27, 38 AD 19, 24 AND 5, 28 AND 9 DUE TO FOD.  (Z)


REMARKS:
DURING Q-4 CHECK INSPECTION, FOUND 3 .25 INCH CRACKS IN STATION 1095 SKIN EMANATING FROM RIVET HOLES BETWEEN LONGERONS 2L AND 3L, 3L AND 4L, 2R AND 3R.  VISUAL AND EDDY CURRENT CONFIRMED.  INSTALLED PLUG AND DOUBLER REPAIRS PER SRM 53-04 FIG 38 SHEET 20 AND 21.  (Z)


REMARKS:
DURING Q-4 CHECK INSPECTION, FOUND A 1.5 INCH CRACK AT STATION 1109 BELTFRAME LONGERON 9 LEFT.  INSTALLED DOUBLER TYPE REPAIR PER SRM 53-01 FIG 2 SHEET 3.  (Z)


REMARKS:
DURING Q-4 CHECK INSPECTION, FOUND A .75 INCH CRACK IN THE RIGHT WHEEL WELL INBOARD DOOR JAMB BELOW HYDRAULIC RESERVOIR.  INSTALLED DOUBLER SRM 53-06 FIG 60 SHEET 1 CONFIG 7007.  (Z)


REMARKS:
DURING Q-4 CHECK INSPECTION, FOUND .75 INCH CRACK IN BELTFRAME AT STATION 389 AND LONGERON 30.  INSTALLED DOUBLER REPAIR PER SRM 5-03 FIG 2A VIEW Q.  (Z)


REMARKS:
DURING Q-4 CHECK INSPECTION, FOUND 2 .1250 INCH CRACKS EMANATING FROM 2 RIVETS AT STATION 69 BETWEEN LONGERON 2L AND 3L.  INSTALLED DOUBLER REPAIR PER SR09530239 AND USAIR EA26143.  (Z)


REMARKS:
DURING Q-4 CHECK INSPECTION, FOUND 3 .25 INCH CRACKS IN SKIN EMANATION FROM RIVETS AT STA 76 BETWEEN LONGERON 2R AND 3R.  INSTALLED DOUBLER REPAIR PER DWG SR09520239 AND USIAR EA 26143.  (Z)


REMARKS:
CLT - FLIGHT 232 - BIRD STRIKE ON NR 2 ENGINE.  FLIGHT RETURNED TO CLE WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCEREPLACED 8 FAN BLADES ON NR 2 ENGINE AND PERFORMED DYNAMIC TRIM BALANCE.  (Z)


REMARKS:
PIT - THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED ALL EMERGENCY LIGHT BATTERY PACKS.  OPERATIONAL CHECKED GOOD.   (Z)


REMARKS:
CLT - FLT 1781 - LT PACK TRIPPED DURING CLIMB-OUT.  RT PACK ON MEL.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED BOTH HEAT EXCHANGERS AND RT PACK DOOR RAM AIR ACTUATOR.  REFERENCE CONTROL NR USAA940507.  (W)


REMARKS:
CLT - FLT 1781 - LT PACK TRIPPED DURING CLIMB-OUT.  RT PACK ON MEL.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED BOTH HEAT EXCHANGERS AND RT PACK DOOR RAM AIR ACTUATOR.  REFERENCE CONTROL NR 94ZZZW2121.  (W)


REMARKS:
IN FLIGHT, THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. RIGGED T/R SWITCH S529 IN NOSE WHEEL WELL AND REPLACED ENGINE ACCESSORY UNIT.


REMARKS:
IN FLIGHT, THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED T/R GROUND SENSE SWITCH S529.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AND STRINGER TIE CORRODED AT BS 913.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING TRANSITION CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 40 AND 50, WL 207.5.  REPAIRED PER SWA RA 1-353-427R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, RBL 24 AND RBL 45.  REPAIRED PER SWA RA 1-353-542.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 294. WL 208, RBL 14 TO 60.  REPAIRED PERSWA RA 1-353-418.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 947.5, WL 208, RBL 9 TO 10 AND AT LBL 43.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 16L CRACKED AT BS 500C.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, BELOW STRINGER 17L AND AT BS 807, ABOVE STRINGER 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
ROA - FOLLOWING ENGINE RUN AFTER C3-CK, IMMEDIATELY AFTER SHUTDOWN, THE RT ENGINE WAS NOTICED TO HAVE SLIGHTLY TITLED DURING SPIN DOWN.  FURTHER INVESTIGATION REVEALED ENGINE MOUNT BOLT, AT THE FORWARD UPPER INBOARD MOUNT, BROKE WHERE THREADS MEET THE SHANK, NUT WAS FOUND INSIDE COWLING, (THIS AREA WAS NOT PART OF THE C-3 CHECK).  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 16L AT STATION 965.  ACCOMPLISHED LONGERON SPLICE REPAIR PER USAIR TYPICAL REPAIR NR 53-10-17.  (Z)


REMARKS:
LGA - FLT 1915 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO LGA WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE ACCOMPLISHED OPERATIONAL TEST AND SYSTEM TEST FOR PRESSURIZATION CONTROL SYSTEM.  NO FAULTS FOUND.  REPLACED CONTROLLER AS PRECAUTIONARY.  (Z)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND TOP OF FRAME AT BS 747, STRINGER 20L CRACKED AND PUNCTURED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLIGHT 212, AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT.  CREW USED OVERRIDE AND GEAR RETRACTED.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED LANDING GEAR HANDLE LATCHING SOLENOID.  AIRCRAFT RETURNED WITH SAME PROBLEM.  RERIGGED RIGHT GEAR GROUND SHIFT CABLE .


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND COMPRESSION CHORD CRACKED 2.4 INCH AT BS 727, BL 0.  A PREVIOUSLY INSTALLED COMPRESSION CHORD DOUBLER AT BL 0  HAS A 1.5 INCH CRACK IN RADIUS.  REPAIRED PER SWA RA 1-253-1132 AND BOEING S/B 737-53-1072.


REMARKS:
IN FLIGHT, NUMBER 1 ENGINE OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED.  CREW PERFORMED NUMBER 1 ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT LAX.  REPLACED MAIN OIL FILTER, OIL BYPASS WARNING SWITCH, AND PERFORMED ENGINE POWER ASSURANCE RUN.


REMARKS:
JFK - DURING MODIFICATIONS TO THE CABIN WHILE IN HANGAR, THE LT POTABLE WATER TANK UPPER POLAR CAP ERUPTED UPWARD, PENETRATING THE CABIN FLOOR AND PSU AREA ON CEILING AT STA 980 TO 984.  REPAIRS TO DAMAGED AREA WERE MADE AND THE AIRCRAFT WAS RETURNED TO SERVICE.  INVESTIGATION INDICATES THE MOST PROBABLE CAUSE WAS THE TANK BECAME OVERPRESSURIZED DUE TO A MALFUNCTION IN THE AIR COMPRESSOR SWITCH, MFG PN 1G216, AND THE RELIEF VALVE, MFG PN 524-6D-45, SETTING WAS ABOVE THE 50 PSIG MAXIMUM BECAUSE OF A LOOSE ADJUSTMENT LOCKING NUT.  A FLEET CAMPAIGN HAS BEEN INITIATED FOR RELIEF VALVE PRESSURE CHECKS AND REPLACEMENTS WILL BE OF A NEW VALVE DESIGN, MFG PN RV05-361.  TOTAL CYCLES 15,653.


REMARKS:
UPON ARRIVAL AT GATE, SMOKE NOTED AT AFT CABIN AREA.  INSPECTED AND FOUND APU LEAKING OIL FROM DRAIN MAST, CAUSING SMOKE TO ENTER CABIN.  REPLACED APU ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP.  REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY EMERGENCY EXIT TRACK LIGHTS INOP.  REMOVED AND REPLACED BATTERY PACK CHARGER PER BOEING M/M.


REMARKS:
FOUND FORWARD CABIN AREA EMERGENCY EXIT TRACK LIGHTS INOP.  REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME BENT AND CRACKED AT BS 460, RBL 9, WL 150.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 344 - LBL 12 INCHES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH STRINGER S-26 R, BS 538.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  REPAIRED PER SRM 53-10-3.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 18 INCHES CORROSION BY 3 INCHES BS 328 - BS 344 RBBL 53.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  REPAIRED PER SRM 53-10-2 AND SRM 51-10-1.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 6 INCHES AND 12 INCHES CORROSION BS 277 - 294.5 AND BS 312-328.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1 AND SRM 51-10-6.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CREASE 10 INCHES LONG BY .5 INCH WIDE O.100 DEEP.  AFT CARGO NR 15 INCHES FROM LEADING EDGE OF DOOR AND DOWN 18 INCH FROM TOP.  REPAIRED PER EA 37303.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND BODY FRAME CRACKED AT BS 767 BETWEEN S-24 L - 25 L.  REPAIRED PER SRM 51-40-3.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT LOWER FAST HOLE ON INNER CHORD OF BS 616, BODY FRAME WL200 APPROXIMATELY.  REPAIRED PER EA 37283.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND NR 2 CRACK BS 616 INNER CHORD OF FRAME.  REPAIRED PER EA 37293.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK LBL 8 BS 178.  REPAIRED PER SRM 53-10-17.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION BS 963 - BS 983.  AFT SERVICE DOORZ ANGLE.  REPAIRED PER SRM 51-10-1.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 32 INCHES CORRODED AREAZ ANGLE FORWARD ENTRY DOOR.  REPAIRED PER SRM51-10-1.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUNDZ ANGLE CORRODED ENTIRE LENGTH AT AFT ENTRYZ ANGLE.  REPAIRED PER SRM 51-10-01.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FROM 2-4 O'CLOCK AROUND OUTBOARD BOLT RT 663 BEAM, RBL 69, WL 188.  REPAIRED PER SB 737-53-1082 DRAWING NR 65C29221.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK SEVERAL PLACES BS 460 BETWEEN S-20L AND 24L.  REPAIRED PER SRM 51-40-03.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 6 INCH GOUGE FUSELAGE SKIN BS 348 S-18 L TO S-19 L.  REPAIRED PER SRM 53-30-3 FIG 1.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH DENT BS 450 BETWEEN S-15 L AND S-16 L.  REPAIRED PER SRM 53-30-3FIG 1.  (Z)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 965 LONGERON 13R.  SPLICED IN NEW SECTION OF LONGERON PER SRM53-02.  (Z)


REMARKS:
DURING Q-2 CHECK INSPECTION, .5 INCH CRACK IN BELT FRAME AT STATION 980 LONGERON 16L.  ACCOMPLISHED SPLICE REPAIR OF BELT FRAME PER SRM 53-03-32.  (Z)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND .5 INCH CRACK AT LONGERON 17L AT STATION 980 LEFT.  SPLICED IN NEW SECTION OF LONGERON FROM STATION 965-996 PER SRM 53-02.  (Z)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT, FOUND .5 INCH CRACK AT STATION 680 LONGERON 2L.  ACCOMPLISHED SPLICE REPAIR OFTHE LONGERON PER SRM 53-02 FIG 2A.  (Z)


REMARKS:
DURING Q-3 INSPECTION VISIT, FOUND .25 INCH CRACK STATION 1043 LEFT FUSELAGE TO PYLON ATTACH ANGLE.  INSTALLED FILLER AND REPAIR ANGLES PER USAIR EA 26785.  (Z)


REMARKS:
DURING Q-3 INSPECTION VISIT, FOUND ..3750 INCH CRACK AT STATION 980 LONGERON 17L.  REPLACED LONGERON AND SPLICE PER SRM53-04.  (Z)


REMARKS:
DURING Q-3 INSPECTION VISIT, FOUND .5 INCH CRACK IN STATION 965 LONGERON 13L AND 14L SKIN CLIP.  ACCOMPLISHED SKIN CLIPSPLICE REPAIR PER SRM 53-03 FIG 3 PG 4M.  (Z)


REMARKS:
DURING Q-3 INSPECTION VISIT, FOUND .5 INCH CRACK IN LONGERON 17R AT STA 980.  REPLACED LONGERON ANS SPLICE REPAIR PER TYPICAL REPAIR 53-10-17.  (Z)


REMARKS:
DURING A SCHEDULED MAINTENANCE VISIT (PIT) FOR A NOSE LANDING GEAR CHANGE, CORROSION WAS FOUND IN THE NOSE GEAR WHEEL.WHEEL ON THE LEFT SUPPORT BEAMS JUST FORWARD AND BELOW THE TRUNNION FITTING.  REMOVED CORROSION AND INSTALLED A DOUBLERREPAIR PER USAIR EA NR 26948A.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORRODED AREA S-28 R KEEL BEAM (VERTICAL FLANGE) AT BS520.  REPAIRED PER EA 37335.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORROSION AREA, AND 2 INCH CRACK S-28 L KEEL BEAM, LOWER CHORD BS 500D PLUS 13, BS 520-526.  REPAIRED PER EA 37333A.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA BS 328-360, RBL 58 GALLEY TRACK.  REPAIRED PER BOEING DRW 69-40352, SRM 51-10-02 AND 51-40-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH BY 20 INCH CORROSION, FLOOR BEAM STATION 328 LBL 35 RBL 60.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TOP OF BS 312 FLOOR BEAM IS CORRODED 5 INCHES WITH 20 PERCENT LOSS AT SCREW HOLES (1 INCH DIAMETER) BS 312 FROM LBL 10 TO RBL 15 (APPROX 20 PERCENT LOSS).  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
DURING Q-2 CHECK INSPECTION FOUND A 5.75 INCH CRACK AT RT WHEEL WELL STA 718 FRAME FWD POCKET, INBD, CRACKED NEXT TO WEB RADIUS.  INSTALLED REPAIR PER USAIR TYPICAL REPAIR NR 53-10-15 AND DRAWING NR 5D534083.  (W)


REMARKS:
DURING Q-2 CHECK INSPECTION FOUND LEVEL II CORROSION.  REF Q-CHECK CARD NR 9-58-38701-C TASK NR C58-53300 CUT OUT CORRODED AREA AND INSTALLED CUSP DOUBLER REPAIR PER SRM 53-05 FIGURE 25.  (W)


REMARKS:
DURING Q-2 CHECK INSPECTION FOUND .3750 INCH CRACK IN LONGERON 16L AT STA 965.  SPLICED IN NEW SECTION OF LONGERON FROMSTA 945 TO 996 END FITTING PER SRM 53-02.  (W)


REMARKS:
DURING Q-2 CHECK INSPECTION FOUND 3 INCH CRACK IN THE LT FLAP ASSY FORWARD SPAR WEB.  CRACK WAS INBD OF CENTER FLAP HINGE.  INSTALLED DOUBLER REPAIR PER SRM 53-01 FIGURE 2 SHEET 3.  (W)


REMARKS:
DURING Q-2 CHECK INSPECTION FOUND A .3750 INCH CRACK AT STA 180 LONGERON 1R.  INSTALLED DOUBLER REPAIR PER SRO DRAWING NR 9530129.  (W)


REMARKS:
DURING Q-2 CHECK INSPECTION FOUND A .25 INCH CRACK AT STA 160 LONGERON 4L.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2.  (W)


REMARKS:
DURING Q-2 CHECK INSPECTION FOUND A .3750 INCH CRACK AT LONGERON 5R STA 699.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2, REV A.  (W)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT FOUND A .5 INCH RACK EA AT STA 617 AND 658 LONGERON 5 LT.  ACCOMPLISHED SPLICE REPAIR PER TYPICAL REPAIR USAIR NR 58-10-17.  (W)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT FOUND A .5 INCH CRACK AT STA 63 LONGERON 5R.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-00 FIGURE 2A.  (W)


REMARKS:
EWR - FLT 31 - ON TAXI OUT, NR 2 ENGINE SHUT DOWN, AFTER SHUT DOWN, OIL QUANTITY NR 2 DECREASED TO ZERO.  REMOVED AND RPELACED NR 2 ENGINE PER MM 71-00-00.  PERFORMED OPS CHECK AND LEAK CHECK OKAY.  TEAR DOWN REPORT DETERMINE NR 5 OIL SEALSHOWS EVIDENCE OF LEAKAGE.  (X)


REMARKS:
ATL/MDW - FLT 61 - ON TAXI OUT, OUTBOARD FLAP LOCKOUT, BETWEEN 3 DEGREES TO 5 DEGREES WHILE EXTENDING.  REMOVED AND REPLACED OUTBOARD FLAP INDICATOR PER 27-80.  OPS CHECK OKAY.  (X)


REMARKS:
EWR/MCO - FLT 4011 - NR 3 LEADING EDGE SLAT AMBER LIGHT DID NOT EXTINGUISH UPON FLAP RETRACTION FROM 2 DEGREES TO UP.  REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER MM 27-81-11.  OPS CHECK OKAY (X)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND MULTIPLE CORRODED AREAS AROUND NUT PLATE HOLES 1 INCH BY 3 INCH FORWARDCARGO LBL 21.8 BS 380-460 AND BS 500 TO 500D.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 12 INCH STATION 294 - STATION 312 LBL 10.  REPAIREDPER SRM 51-10-1.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 15 INCH CORRODED AREA BL0, BETWEEN BS 344 AND BS 360 FLOOR BEAMS.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TRANSITION ANGLE IN FORWARD CARGO RBL 21.8 APPROXIMATELY 48 INCHES CORRODED AROUND FASTENER HOLES BS 494.4 TO BS 500 D 30 PERCENT LOSS.  REPAIRED PER SRM 51-10-02, CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUT PLATE HOLES 1 INCH BY 3 INCH FORWARD CARGO RLL 13.8 BS 500C-BS 500D.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA IN SEVERAL SPOTS ON CHANNELS 40 PERCENT LOSS, AFT CARGO LBL 17.2 TO RBL 8.1 STATION 727 C PLUS 9 TO 727 E PLUS 8.  REPAIRED PER SRM 53-60-53.  CORROSION TASK NRC53-208-01, CORROSION LEVEL 2.


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA BS 322, S-28R.  REPAIRED PER SRM 53-00-03, FIG 201.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 48 INCH BY 2 INCH CORRODED AREA FLOOR BEAM, UPPER TEE CHORD, BS 986.5 LBL 28 TO RBL 28.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH CORRODED AREA BS 290-310, S-17 R (FORWARD SERVICE DOOR P/N654587545 SILL ANGLE).  REPAIRED PER SRM 51-10-02 AND 51-40-02.  CORROSION TASK NR C53-1107-02, CORROSION LEVEL 2.(Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 40 INCH BY 2 INCH CORRODED AREA SILL SUPPORT ANGLE (Z ANGLE) S-17L ATLEFT HAND AFT ENTRY DOORWAY.  REPAIRED PER SRM 51-10-02 AND 51-40-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 10 INCH CORRODED AREA RBL 12, BS 312-328 (CABIN FLOOR SUPPORT).  REPAIRED PER SRM 51-10-02 AND 51-40-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORRODED AREA AROUND NUT PLATE HOLES 20 PERCENT LOSS AFT CARGO STATION 790 INTERCOSTAL BRACKETS AT S-22, S-23 AND S-24.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.   (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH D SPOTS OF CORROSION AT SCREW HOLES IN SILL PLATED AT AFT CARGO DOOR CUTOUT BS 787-847 APPROXIMATELY 25 PERCENT LOSS.  REPAIRED PER 51-10-2.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA 20 PERCENT LOSS LBL 17 STATION 907 TO 870 AND STATION 913.5 TO 945.  REPAIRED PER SRM 51-10-02 PAGE 15.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  P/N BAC15201392717876.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORRODED AREAS AROUND NUT PLATE HOLES ETC 30 PERCENT LOSS AFT CARGO TRANSITION ANGLE RBL 22.5 STATION 847 TO 947.  REPAIRED PER SRM 53-30-53.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORRODED AREAS AT NUT PLATE HOLES ETC 30 PERCENT LOSS,AFT CARGO TRANSITION ANGLE LBL 22.5 FS 727 TO 947.  REPAIRED PER SRM 53-60-53.  CORROSION TASK NR C53-208-01, CORROSIONLEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA ON FLOOR BEAM CHANNELS 80 PERCENT LOSS AFT CARGO LBL 17.2 TO RBL 8.1 STATION 770.  REPAIRED PER SRM 53-60-53.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.(Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND (2) 1 INCH BY 5 INCH CORRODED AREAS 30 PERCENT LOSS AFT CARGO RBL 13.5 STATION 727 D PLUS 1 727 D PLUS 12 TO STATION 779.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  P/N BAC152013977178T6  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 10 INCH CORROSION AT STRINGER BS 967 S-27 L.  REPAIRED PER SRM 53-10-3 FIG 1.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY .5 INCH BS 507 - BL0 SUPPORT ANGLE.  REPAIRED PER SRM 53-10-6 (REMOVED AND REPLACED).  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION BS 380 THROUGH BS 520 .25 INCH BY 9 INCH TRANSITION ANGLE.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 1 INCH BY 4 INCH BS 727-731 S-27R.  REPAIRED PER EA 37342.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
TPA - FLT 8646 - FLT EN ROUTE LAS TO RSW WHEN RIGHT GEAR RED LIGHT CAME ON.  FLIGHT DIVERTED TO TPA WHERE ON APPROACH RECEIVED THREE GREEN LIGHTS WHEN GEAR WAS EXTENDED.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED RIGHT GEAR UP LOCK PROXIMITY SWITCH.  GEAR CHECKS GOOD.  (Z)


REMARKS:
PIT - FLIGHT NR 493 - ON APPROACH SELECTED GEAR DOWN, NOSE GEAR STAYED IN WELL.  RECYCLED GEAR AND TOWER CONFIRMED GEARDOWN.  AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE PER MM 32-32-01.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLT 901 - UPON ARRIVAL AT GATE, THE RIGHT BRAKE WAS ON FIRE.  PASSENGERS EVACUATED AIRCRAFT FROM LT SIDE OVERWINGEMERGENCY DOOR EXITS.  NO INJURIES REPORTED.  FIRE DEPARTMENT RESPONDED.  MAINTENANCE REPLACED NR 3 AND NR 4 MLG BRAKE ASSY AND IBR AND XBR MLG BRAKE TEMPERATURE SENSORS.  ACCOMPLISHED AXLE CHECKS.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
CLT - FLT 291 - ON APPROACH, LT MLG INDICATED UNSAFE WHEN SELECTED DOWN.  RECYCLED GEAR.  FLYBY INDICATED GEAR WAS DOWN.  AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE RELACED LEFT MAIN GEAR PRIMARY SENSOR.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
ATL - FLT NR 476 - BEFORE DEPARTURE, THE EVACUATION LIGHTS IN ROWS 5, 6, 8, 9 AND 11 WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER ASSY.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION AT WEB STATION 847 S-25R.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01 CORROSION LEVEL 2.  (Z)


REMARKS:
AIRCRAFT 909 ON FLIGHT 116 EXPERIENCED SUDDEN DEPRESSURIZATION EN ROUTE TO IAD.  AIRCRAFT FLEW BACK TO ATL WITHOUT CUSTOMERS.  THE OUTFLOW VALVE ACTUATOR AND THE CABIN DIFFERENTIAL PRESSURE SENSOR WAS REPLACED AS A PRECAUTIONARY MEASURE.  AIRCRAFT OPS CHECKED OKAY IAW DOUGLAS MM 21-00.


REMARKS:
AFTER RAISING GEAR RETRACTION HANDLE DURING ASCENT, PILOTS NOTICED UNSAFE GEAR LIGHT ILLUMINATING.  AIRCRAFT RETURNED TO ATL, WHERE AIRCRAFT LANDED SAFELY WITH DAMAGE TO THE MAIN GEAR DOORS DUE TO DRAGGING OF THE DOORS UPON LANDING.  REPLACED MAIN LANDING GEAR DOORS AND PERFORMED GEAR SWING IAW DOUGLASS MM 32-00.


REMARKS:
COPILOTS OUTER WINDSHIELD PANE SHATTERED.  FLIGHT HAD TO RETURN TO ATL DUE TO ICING CONDITIONS ON THE AIRCRAFTS ROUTE.FLIGHT 122 ATL TO PHL, 6/26/94.  REPLACED F/O WINDSHIELD.  LEAK CHECK OK.


REMARKS:
PIT - FLT 383 - ON CLIMB-OUT OF BWI, EN ROUTE TO ORD, RIGHT WING/BODY OVERHEAT LIGHT ILLUMINATED AND FLIGHT CREW COULD NOT CONTROL PRESSURIZATION.  CREW DEPLOYED PASSENGER OXYGEN MASKS.  MAX CABIN ALTITUDE WAS 11,000 FEET.  FLIGHT DIVERTEDTO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE RAN RIGHT ENGINE, COULD NOT DUPLICATE WING/BODY OVERHEAT.  REPLACED LEFT HP BLEED REGULATOR DUE TO LOW AIRFLOW.  RAN ENGINE BLEED PRESSURE CHECKED GOOD.  (Z)


REMARKS:
PIT - FLT 1470 - AFTER TURNING OFF OF THE RUNWAY, A GRABBING AND GRINDING SENSATION WAS FELT WHICH SEEMED TO COME FROM THE LT GEAR.  MAINTENANCE FOUND THAT NR 4 WHEEL FAILED.  REPLACED BOTH MAIN TIRES, BRAKES AND TRANSDUCER ON RT GEAR.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
COS - FLT 484 - RETURNED FROM FLIGHT ACCOUNT RT ENGINE SHUT DOWN DUE TO LOUD NOISE REPORT AND POWER LOSS.  FOUND METAL IN TAIL PIPE AND TAIL CONE MISSING.  REPLACED ENGINE SN 3228.  ENGINE TOTAL TIME 21,342, 12,759 CYCLES.  CHECK C-2A 3-26-9.  INVESTIGATION INTO ENGINE SN 3228 SHUT DOWN DUE TO LOUD NOISE REPORT AND POWER LOSS, REVEALED A FIRST STAGE LOW PRESSURE TURBINE BLADE, PN 836201, FRACTURED CAUSING TURBINE DAMAGE.  REPAIRED DAMAGE.  ENGINE SN 3228 RETURNED TO SERVICE.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 11 - 16.  REPLACED BATTERY PACK AND POWER SUPPLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND .5 INCH CRACK AT CAPTAIN'S  C-D WINDOW POST SKIN.  REPAIRED PER SWA RA 1-353-1134.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LEFT SIDE FUSELAGE SKIN DENTED AT BS 382, WL 217.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LEFT WING ILLUMINATION LIGHT SUPPORT STRINGER CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND S/B 737-53-1145.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 55 TO LBL 55, WL 208.  REPAIRED PER SWA RA 1-353-542.


REMARKS:
NUMBER 2 ENGINE SURGES IN FLIGHT.  ACCOMPLISHED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 2 ENGINE ASSEMBLY PER BOEING M/M.


REMARKS:
FLT NR 37 - EWR TO MDW ON TAXI OUT, ON START NR 3 OIL PRESS GAUGE DID NOT INDICATE ABOVE 31 PSI OIL PRESS LIGHT AND TEMP NORMAL.  CLEANED CANNON PLUG.  OPS CHECK OIL PRESS OK.


REMARKS:
FLT NR 76 - MCO-ATL - ON TAXI OUT LOST ALL HYDA QUANTITY AND BOTH NR 1 AND NR 2 ENGINE LOW PRESSURE PUMP LIGHTS CAMEON.  REMOVED AND REPLACED CASE DRAIN FILTERS AND PRESS FILTERS ON NR 1 AND NR 2 ENGINE, FOUND NO METAL, FOUND SYSTEMA


REMARKS:
DTW - FLT 285 - DURING CRUISE, NR 1 ENGINE WAS SHUT DOWN DUE TO FIRE WARNING INDICATION.  A-LOOP ON STEADY, B-LOOP INTERMITTENT WHEN SWITCHED TO SINGLE LOOP OPERATION.  FOUND DEFECTIVE PYLON LOOP MFG PN 10-61096-24.  REPLACED CHECK C-2 , 11-8-93, MCI.


REMARKS:
IND - FLT 100 - ON APPROACH WHEN LANDING GEAR WAS EXTENDED, UNSAFE LIGHT REMAINED ON WITHOUT A SAFE GREEN LIGHT UNTIL LANDING GEAR WAS RECYCLED.  REPLACED LOCK ACTUATOR.  OPS CHECKS NORMAL.  CHECK C-1 - 10-9-93 - MCI.


REMARKS:
STL - DURING OP-15, FOUND A 2.50 INCH CRACK IN FLOOR BEAM UPPER RADIUS, STA 294.  REPAIRED PER SRM 53-05, FIGURE 3, SRM51-10-03, ARA 8009 AND STANDARD PRACTICES.  AIRCRAFT TT, 62,704 HOURS; 77,963 CYCLES.


REMARKS:
STL - DURING OP-15, FOUND A .1875 INCH CRACK IN VERTICAL STABILIZER-TO-FUSELAGE RT ATTACH ANGLE, STA 944.  REPAIRED PERSRM 53-05, FIGURE 23A, SHEET 1,  AIRCRAFT TT:  62,704 HOURS; 77,963 CYCLES.


REMARKS:
PHL - FLT 191 - INVESTIGATION OF ENGINE, S/N 3903, SHUT-DOWN DUE TO OIL FILTER BYPASS LIGHT ILLUMINATING, REVEALED A FAILURE OF THE NR 3 BEARING.  REPLACED BEARING, REPAIRED HOUSING AND RELOCATED COMPONENTS.  ENGINE S/N 3903 RETURNED TO SERVICE.


REMARKS:
PBI - FLT 479 - INVESTIGATION OF ENGINE SN 1534, SHUT-DOWN DUE TO VIBRATION AND OIL FILTER BYPASS LIGHT ILLUMINATING, REVEALED A FAILURE OF NR 3 BEARING.  REPLACED BEARING, REWORKED HOUSING AND RELATED COMPONENTS. ENGINE SN 1534 RETURNED TO SERVICE.


REMARKS:
PHL - FLT 1072 - IMMEDIATELY AFTER LIFT-OFF, THE CREW NOTICED A BURNING RUBBER ODOR IN THE COCKPIT AND CABIN.  AIRCRAFTRETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE INSPECTED ENGINES, PACK INLETS AND LANDING GEAR AND WAS UNABLE TO DETECT ANY BURNING RUBBER ODOR.  MAINTENANCE DID REPLACE BOTH NOSE WHEEL BRAKE PADS DUE TO EVIDENT WEAR.  (X)


REMARKS:
RIC - FLT 372 - ON LIFT-OFF, THE MAIN ENTRY DOOR YELLOW CAUTION LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE MAIN ENTRY DOOR HANDLE LOCK SWITCH.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
CLT - EMERGENCY EXIT LIGHTS FAILED TO OPERATE DURING TEST.  MAINTENANCE REPLACED THE BATTERY PACK AT ENTRANCE TO AIRCRAFT AND ALSO AT THE LT FWD CARGO BIN.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
PHL - FLT 910 - ON APPROACH WHEN GEAR LEVER PLACED IN DOWN POSITION, THE LT LANDING GEAR DOWN (GREEN LIGHT) DID NOT ILLUMINATE.  GEAR RECYCLED WITH NO CORRECTION.  AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LT MAIN GEAR D0OWNLOCK ACTUATOR PER MM 32-32-05.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
DURING FC-6 INSPECTION, FOUND A .50 INCH CRACK IN THE ATTACH BRACKET MAIN GEAR TRUNNION TO FALSE SPAR JUST FORWARD OF PANEL 82X (RT WHEELWELL).  FABRICATED AND INSTALLED ATTACH BRACKET L ANGLE PER SRM 57-02-09.  (X)


REMARKS:
DURING S.I.P. INSPECTION 53-10-20 J.P.C. NR JE-50-53502 EDDY CURRENT INSPECTION OF THE SERVICE EMERG. DOOR APERTURE, FOUND A .3750 INCH AND .75 INCH CRACK IN THE SKIN TOP FORWARD CORNER.  CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 53-02-16 AND USAIR EA 26349.  (X)


REMARKS:
DURING S.I.P. INSPECTION 53-10-19 J.P.C. NR JE-42-53503, VISUAL INSPECTION REVEALED .25 INCH CRACK LT AIR CONDITIONING BAY SKIN 5 INCHES FORWARD OF FRAME 3050 WHEELWELL SKIN.  CUT OUT DAMAGED AREA AND INSTALLED SKIN AND REPAIR DOUBLER PER SRM 53-11-00, PAGE 3.  (X)


REMARKS:
EWR - FLT 7880 - LT ENGINE FAILED ON TAKEOFF AT ROTATION.  HEARD LOUD POP/BANG AND SLIGHT SMELL OF SMOKE IN CABIN.  FLIGHT CREW SHUT DOWN ENGINE PER CHECK LIST.  FLIGHT RETURNED TO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LT ENGINE.  (X)


REMARKS:
CLE - EMERGENCY EXIT CEILING LIGHT IN FIRST CLASS INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK AND POWER SUPPLY (X)


REMARKS:
OAJ - FLT 1763 - AFTER TAKEOFF, NOSE GEAR RETRACTED, BUT MAIN GEARS DID NOT.  CYCLED GEAR.  NORMAL GEAR INDICATIONS WITH GEAR LOWERED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE JACKED AIRCRAFT, INSPECTED HARNESS/HYDRO LINES - PERFORMED SEVERAL RETRACT/EXTENSIONS AFTER RESETTING EMERGENCY EXTENSION.  ALL CHECKS GOOD.  (X)


REMARKS:
TLH - FLT 7882 - AFTER TAKEOFF, RETRACTED GEAR -- WITH THE GEAR HANDLE UP, THE NOSE GEAR HAD NO INDICATION.  CYCLED GEAR.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED RT MLG DOOR UP SEQUENCE VALVE DUE TO STUCK PLUNGER PER MM.  OPERATION CHECKS NORMAL. (X)


REMARKS:
ATL - FLT 476 - BEFORE DEPARTURE, THE EVACUATION LIGHTS IN ROWS 5, 6, 8, 9, AND 11 WERE FOUND INOPERATIVE.  MAINTENANCEREPLACED THE BATTERY PACK AND CHARGER ASSY.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER 25L CORRODED AT BS 857.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND PRESSURE DOME GOUGED AT BS 1028, STRINGER 6.  REPAIRED PER TRAMCO EWO 94-0584.


REMARKS:
DURING SCHEDULED D CHECK, FOUND PRESSURE DOME GOUGED AT BS 1040, STRINGER 23L.  REPAIRED PER TRAMCO EWO 94-0559.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT EXIT AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, S24L, WL 60.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKINS CORRODED FROM BS 727-907, S20 -25L AND R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0549.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND TIE STRAP CORRODED FROM BS 787 TO 850, RBL 20.5, WL 160.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND WEB CRACKED IN AIR INLET LEFT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 798, STRINGER 27R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 807, BETWEEN STRINGERS 28R AND 28L.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND INBOARD WING T/E L/E SUPPORT BRACKET CRACKED AT WING ROOT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND NUMBER 1 ENGINE NOSE COWL AFT CIRCUMFERENTIAL FRAME CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DFW - FLT 916 - SHORTLY AFTER TAKEOFF, DURING ENGINE BLEED RECONFIGURATION, A LOUD POP WAS HEARD AND SMOKE STARTED FILLING THE CABIN.  FLIGHT RETURNED TO DFW WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE CHECKED PACK OPERATION, FOUND OKAY FOR SERVICE.  FOUND B-NUT LOOSE ON 13TH STAGE MOD VALVE CONTROL AIR LINE.  SECURED LINE. OPS OKAY.  (X)


REMARKS:
MSY - FLT 293 - FOLLOWING TAKEOFF, CLIMBING THROUGH 2,000 FEET JUST BELOW CLIMB, POWER SETTING GOT TAIL COMPARTMENT TEMP HIGH LIGHT.  LIGHT EXTINGUISHED WHEN POWER REDUCED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE OPERATED APU AND BOTH PACKS, BUT COULD NOT DUPLICATE TAIL TEMP LIGHT.  GROUND OPERATION CHECKS GOOD IAW MM'S.  (X)


REMARKS:
INT - DURING 'Q-5' CHECK VISUAL INSPECTION FOUND .50 INCH CRACK IN LOWER AFT STOP FITTING ON DOOR BS 325 WL 219 (FORWARD GALLEY DOOR).  REPAIRED PER SRM 51-10-1.  (X)


REMARKS:
INT - DURING 'Q-5' CHECK VISUAL INSPECTION FOUND 2 INCH CRACK AFT SIDE OF BS 1156 BULKHEAD IN OUTER CHORD AT WL 280 (RIGHT SIDE).  REPAIRED PER E.O. 5391G569.  (X)


REMARKS:
INT - DURING 'Q-5' CHECK VISUAL INSPECTION FOUND FRAME CRACKED .25 INCH AT STA 480 ABOVE STR 26L, STA 480.  REPAIRED PER SRM 51-40-3.  (X)


REMARKS:
INT - DURING 'Q-5' CHECK VISUAL INSPECTION FOUND HOLE BURNED IN FLOOR BEAM WEB .1250 INCH DIAMETER, STA 344, RBL 23 INCH.  REPAIRED PER SRM 51-40-2.  (X)


REMARKS:
DCA - F LT 670 - FLIGHT EN ROUTE PIT TO PVD WHEN RADAR WOULD NOT PAINT WEATHER.  FLIGHT DIVERTED TO DCA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED RADAR INDICATOR.  WEATHER RADAR OPERATES NORMALLY.  (X)


REMARKS:
TPA - FLT 1798 - AFTER TAKEOFF FROM MIA, AT CLIMB POWER, NR 1 ENGINE OVERHEAT LIGHT CAME ON.  REDUCED THRUST ON NR 1 ENGINE, LIGHT WENT OUT.  ADDED POWER, LIGHT CAME ON AGAIN.  FLIGHT DIVERTED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CRACKED 13TH STAGE CROSSOVER DUCT.  LEAK AND OPS CHECKS SATISFACTORY.  (X)


REMARKS:
INT - DURING 'DROP-IN' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION BS 500 BS 28L.  REPAIRED PER EA 37444.(X)


REMARKS:
BDL - FLT 1783 - LOST SYSTEM 1 HYDRAULIC QUANTITY DURING FLIGHT.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED O-RING AT SPIGOT ON PRESSURE SIDE OF LT ENGINE DRIVEN HYD PUMP. OPERATION CHECKS NORMAL.  (X)


REMARKS:
PIT - FLT 326 - AFTER LANDING GEAR DOWN SELECTION, GOT A NOSE GEAR UNSAFE RED LIGHT.  RECYCLED THE GEAR AND GOT A NORMAL INDICATION.  AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND ALL OPERATIONS AND INDICATIONS NORMAL.  LUBED AND SWUNG GEAR.  (X)


REMARKS:
PIT - FLT 1234 - AFTER TAKEOFF, NLG WOULD NOT RETRACT.  CYCLED GEAR.  AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT.MAINTENANCE REPLACED NLG PN 201071001 PER J532-21-1.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
PIT - FLT 1786 - AFTER TAKEOFF, THE GREEN LIGHT WOULD NOT ILLUMINATE FOR THE LT LANDING GEAR, ALSO THE LT GEAR DOOR WOULD NOT CYCLE TO THE UP POSITION.  THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LT MAIN GEAR DOOR.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
DAY - FLT 1160 - ON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED.  CYCLED GEAR.  AIRCRAFT LANDED AT DESINATION WITHOUT INCIDENT.  MAINTENANCE REPLACED THE PROXIMITY SWITCH CONTROL UNIT.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
MCI - FLT 450 - DURING CRUISE, RT ICING PROTECTION HIGH LIGHT ILLUMINATED.  CREW WENT THROUGH ABNORMAL PROCEDURE AND WAS UNSUCCESSFUL IN GETTING LIGHT EXTINGUISHED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND A HOLE IN THE RT PACK COLD AIR DUCT.  MAINTENANCE REPLACED DUCT.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
BOS - FLT 1181 - AFTER GEAR RETRACTION, BLUE LIGHT IN HANDLE EXTINGUISHES AND THEN ILLUMINATES.  CYCLED GEAR, NO CORRECTION.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED RT UPSTOP DAMPER PER MM 32-11-05.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
CLT - FLT 340 - AFTER TAKEOFF, THE MED RED WARNING LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE ADJUSTED DOOR WARNING SWITCH.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
GSO - DURING 'PCI 901 AND PCI 902' CHECK VISUAL INSPECTION FOUND .281 INCH CRACK FORWARD CARGO DOOR HINGE 'MOST FORWARDLUG' UPPER HINGE HALF.  NOTE:  THIS WAS FOUND WHILE ACCOMPLISHING INSPECTION OF LOWER HINGE HALF WHICH IS NOT THIS JOB CARD.  DEFERRED OM-7 NR 03796 EA 27029.  (X)


REMARKS:
SHOP FUNCTION CHECK OF SLIDE.  THE SLIDE LIGHT HARNESS DID NOT ILLUMINATE ALTHOUGH BATTERY LANYARD WAS PROPERLY PULLED FROM THE BATTERY SWITCH.  A REPLACEMENT BATTERY WAS INSTALLED AND LIGHT HARNESS FUNCTIONED OKAY PER MAINTENANCE.  SLIDE - MFR P/N D31793101, S/N 0030.  (X)


REMARKS:
CMH - FLT 212 - ON FINAL, CAPTAIN NOTICED A HIGH READING ON THE RT ENGINE OIL TEMPERATURE WITH THE OIL QTY DECREASING AT AN ACCELERATED RATE.  THE RT ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED.  AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RT ENGINE.  OPERATION CHECKS NORMAL.  (X)


REMARKS:
MCI - DURING OP-16 FOUND CORROSION AT RT FUSELAGE FRAME, STA 420, STRINGER 17R.  REMOVED CORROSION PER SRM 51-10-06 ANDREPAIRED PER SRM 51-40-03 AND STANDARD PRACTICES.  TOTAL CYCLES 14,767.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND CORROSION AND 1.25 INCH CRACK IN LT LOWER FUSELAGE SKIN, STA 589.  REPAIRED BY REMOVING CORROSION, STOP DRILLING CRACK AND INSTALLING DOUBLER PER SRM 53-31-00, PAGE 827, AND ARA 8101.  TOTAL CYCLES 21,934.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND CORROSION AND A TWO INCH CRACK IN SKIN AT LEFT LOWER FUSELAGE, STA 629.  REPAIRED BY REMOVING CORROSION, STOP DRILLING CRACK AND INSTALLING DOUBLER PER SRM 53-31-00, PAGE 827, AND ARA 8101.  TOTAL CYCLES 21,934.


REMARKS:
MCI - DURING OP-17 FOUND 6 INCH CRACK IN RT WING FALSE SPAR LOWER CHORD ANGLE AT INBD END OF NR 8 GROUND SPOILER ATTACHMENT.  REPAIRED PER RM 51-40-4.  TOTAL CYCLES 24,634.


REMARKS:
MCI - DURING OP-16 FOUND CABIN INTERCOSTAL CRACKED .1250 INCH AT STRINGER 26L, BETWEEN STA 360 AND 380.  REPAIRED PER SRM 51-40-02 AND 51-30-02.  TOTAL CYCLES 14,767.


REMARKS:
MCI - DURING OP-17 FOUND 2 INCH CRACK IN LT WING TE FALSE SPAR LOWER CHORD ANGLE, AT INBD END, NR 7 GROUND SPOILER LOWER ATTACHED.  REPAIRED PER SRM 51-40-4 FIGURE 1, PAGE 5.  TOTAL CYCLES 24,634.


REMARKS:
MCI - DURING OP-15 FOUND DENT IN FUSELAGE LT SIDE, STA 232, ABOVE STRINGER 18L.  INSTALLED DOUBLER PER SRM 53-04, PAGE 59, FIGURE 12B.  TOTAL CYCLES 71,936.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON FUSELAGE STA 836 TO STA 843, ON LAPSEAM 39L.  INSTALLED REPAIR PER SRM 53-30-03, FIGURE 11, CHART NR 1.  TOTAL CYCLES 14,767.


REMARKS:
CDG - FLT 903 - DURING CRUISE, NR 1 ENGINE SPUN DOWN.  FOUND ENGINE DRIVEN FUEL PUMP SHAFT SEPARATED.  REPLACED PUMP, MFG PN 373401-26.  OP CHECKS NORMAL.  CHECK C-8B, 10-28-93, JFK.


REMARKS:
STL - DURING C-CHECK, FOUND .25 INCH CRACK IN LONGERONS 12R AND 13R, STATION 965.  REPAIRED BY SPLICING IN SECTION OF NEW LONGERONS PER SRM 53-02, FIGURE 2.  TOTAL CYCLES 77,962.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR BEAM CAP, STATION 1680, RBL 44.  REMOVED CORROSION PER SRM 51-10-01, AND REPAIRED PER SSRM 53-00-509 AND STANDARD PRACTICES.  TOTAL CYCLES 77,962.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON RT WING LOWER SPAR CAP OUTBOARD LEADING EDGE, STATION 1360.  REPAIRED PER SRM 57-30-03.  TOTAL CYCLES 77,962.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON CABIN FLOOR BEAM CAP STATION 880, LBL 24 TO LBL 70.  REPLACED FLOOR BEAM CAP PERSRM 53-10-07, FIGURE 10, SRM 51-10-01, AND SRM 51-30-02.  TOTAL CYCLES 77,962.


REMARKS:
NOSE GEAR GREEN LIGHT DID NOT COME ON FOR LANDING AT PBI, VISUALLY CONFIRMED GEAR WAS DOWN.  FOUND PIN PUSHED OUT OF SWITCH CONNECTOR, SECURED PIN, GEAR POSITION NORMAL, INDICATING NORMAL.  CHECKS GOOD PER MM 32-00.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A, 1 INCH ABOVE STRINGER 16L.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STRINGER 24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, 18 INCHES FORWARD OF POTABLE WATER SERVICE DOOR.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, LEFT SIDE, ABOVE T/E FLAPS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW FRAME OUTER SKIN CRACKED AT UPPER OUTER CORNER.  NDT REVEALED NO CRACK IN GUSSET.  REPAIRED PER SWA RA 1-353-1154.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND LEFT HORIZONTAL STABILIZER CENTER SECTION BALANCE PANEL BAY I/B WEB WORN FROM PANELSEAL.  REPAIRED PER SWA RA 1-355-177.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND LEFT HORIZONTAL STABILIZER, INBOARD BALANCE PANEL BAY I/B WEB WORN FROM PANEL SEAL. REPAIRED PER SWA RA 1-355-177.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND LEFT HORIZONTAL STABILIZER, CENTER  BALANCE PANEL BAY O/B WEB WORN FROM PANEL SEAL. REPAIRED PER SWA RA 1-355-177.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND LEFT HORIZONTAL STABILIZER, OUTBOARD BALANCE PANEL BAY I/B WEB WORN FROM PANEL SEAL.  REPAIRED PER SWA RA 1-355-177.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND LEFT HORIZONTAL STABILIZER, OUTBOARD BALANCE PANEL BAY O/B WEB WORN FROM PANEL SEAL.  REPAIRED PER SWA RA 1-355-177.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND RIGHT HORIZONTAL STABILIZER, CENTER BALANCE PANEL BAY I/B WEB WORN FROM PANEL SEAL. REPAIRED PER SWA RA 1-355-176.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND RIGHT HORIZONTAL STABILIZER, OUTBOARD BALANCE PANEL BAY O/B WEB WORN FROM PANEL SEAL.  REPAIRED PER SWA RA 1-355-176.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND CABIN FLOOR LEFT VERTICAL FRAME LEG CRACKED AT BOTTOM END BELOW FLOOR TO FIRST FASTENER, JUST FORWARD OF EMERG EXIT.  REPAIRED PER SWA RA 1-353-1139.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND LEFT WING RIB CRACKED .5 INCHES IN WING STRUCTURE IN AREA OF SECOND FROM INBOARD HINGEOF AILERON.  REPAIRED PER BOEING STRUCTURE REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND STRINGER TO FUSELAGE FRAME TIE DOWN CLIP CRACKED AT BS 344, STRINGER 11R.  REPAIRED PER BOEING STRUCTURE REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FORWARD ENTRY  DOOR MOP SILL ANGLE CORRODED.  REPLACED PER BOEING STRUCTURE REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FORWARD CARGO DOOR, FORWARD AND AFT FRAMES CRACKED.  REPLACED PER SWA ACO 3194-52.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT GALLEY DOOR FORWARD FRAME CRACKED AT BS 955, RBL 56, WL 265.  REPLACED PERSWA ACO 3194-52.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 344, WL 208, LBL 45 - RBL 12.  REPLACED PER SWA RA 1-353-427.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD AT BS 986, LBL 14 TO RBL 45, WL 208.  REPLACED PER SWA RA 1-353-542.


REMARKS:
DURING TAKEOFF ADVANCED POWER, WARNING HORN SOUNDED.  CHECKED FLAPS 5 DEGREES, TRIM 6 DEGREES, CYCLED SPOILERS FLAPS AND TRIM, NO HELP.  RETURNED TO RAMP.  REPOSITIONED SWITCH ROLLER OF FLAP QUADRANT FOR TAKEOFF WARNING SWITCH (HORN) OPERATED FLAPS AND THROTTLE, NO FURTHER HORN INDICATIONS, OPS CHECKED OK PER MM CHAPTER 32-00.


REMARKS:
NOSE LANDING GEAR LOCK AND UPLIMIT SWITCH INOPERATIVE FLIGHT 34 IN SAVANNAH.  REMOVE AND REPLACE SWITCH AND REMOVED ANDREPLACED QUICK DISCONNECT PLUG PER MM 32-00.  OPERATIONAL CHECK GOOD.


REMARKS:
IND - FLT 22 - THE CREW GOT HYDRAULIC SYSTEM 1 LOW QUANTITY INDICATION DURING FLIGHT.  HYD QTY DROPPED TO 36 PERCENT.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND ENGINE NR 1 SYTEM NR 1 HYDRAULIC PUMP PRESSURE LINE LEAKING AT QUICK DISCONNECT.  MAINTENANCE REPLACED QUICK DISCONNECT.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION FOUND 12 INCH CORROSION STR BS 907 S-27L.  REPAIRED PER SRM 53-10-3, CORROSIONTASK NR C53-208-01, CORROSION LEVEL 2.  (W)


REMARKS:
GSO - FLT 929 - A-SYSTEM HYDRAULIC LOSS DURING CLIMB-OUT FROM ROA.  FLIGHT DIVERTED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND A-SYSTEM RETURN LINE CRACKED.  REPLACED RETURN LINE.  (W)


REMARKS:
PIT - DURING Q-4 INSPECTION FOUND A .6250 INCH CRACK AT THE RT AFT EMERGENCY EXIT WINDOW DOOR PAN TOP AFT STOP.  VERIFIED BY VISUAL AND EDDY CURRENT INSPECTION.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 52-20-03.  (W)


REMARKS:
PIT - DURING Q-4 INSPECTION, FOUND .75 INCH CRACK LT FORWARD EMERGENCY EXIT WINDOW DOOR PAN AROUND THE TOP FORWARD STOP.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 52-20-03.  (W)


REMARKS:
PIT - DURING Q-4 INSPECTION, FOUND 1 INCH CRACK IN THE RT UPPER PYLON DRAG ANGLE FWD END.  INSTALLED DOUBLER REPAIR PERSRM 54-04 FIGURE 10.  (W)


REMARKS:
PIT - DURING Q-4 INSPECTION FOUND A 1.25 INCH CRACK AT THE RT AFT EMERGENCY EXIT WINDOW AFT BAYONET RECEPTACLE.  (DOOR PAN).  INSTALLED DOUBLER REPAIR PER SRM 53-05, FIGURE 32A.  (W)


REMARKS:
DURING Q-4 INSPECTION, FOUND A .5 INCH SCRATCH .008 DEPTH IN SKIN AT STA 332 LONGERON 24R-25R.  INSTALLED DOUBLER REPAIR PER SRM53-04, FIGURE 38.  (W)


REMARKS:
SFO - FLT 0048 - AFTER DEPARTURE AT 7000 - 8000 FEET, THE DOOR WARNING LIGHT CAME ON STEADY AND THE RT AFT DOOR HANDLE MOVED 3-4 INCHES.  THE FLIGHT ATTENDANT TRIED TO RESTOW THE HANDLE BUT IT WOULD NOT REMAIN IN ITS NORMAL POSITION.  THE AIRCRAFT THEN RETURNED TO SFO.  NO EMERGENCY WAS DECLARED.  MAINTENANCE REPLACED THE LATCH ROLLER BEARING.  OPS CHECKED NORMAL.  (W)


REMARKS:
PIT - FLT 0271 - ON GEAR RETRACTION, THE RED UNSAFE LIGHTS REMAINED ON WITH THE GEAR DOOR OPEN LIGHT ON.  ON RETURNING TO PIT, THE GEAR HANDLE WAS DOWN WITH THE GEAR DOOR OPEN LIGHT STILL ON.  THE CREW LANDED WITH THE EMERGENCY HANDLE UP.THE AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE INSTALLED BOTH GEAR DOORS, RIGGED THE UPLOCK AND DOOR LIGHTS.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
GSO - FLT 2124 - FLIGHT EN ROUTE TPA TO BWI WHEN AIRCRAFT LOST A-SYSTEM HYDRAULICS.  FLIGHT DIVERTED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND RT MAIN GEAR UP LINE CHAFED AND LEAKING.  REPLACED LINE.  REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS, PRECAUTIONARY.  (W)


REMARKS:
CLT - FLT 363 - ON CLIMB-OUT FROM CLT, THE NR 1 ENGINE FUEL FLOW, N1, N2 AND EGT BEGAN FLUCTUATING.  FLIGHT RETURNED TOFIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED FUEL CONTROL ON LT ENGINE.  LEAK CHECKED AND GROUND RAN LT ENGINE, OPS CHECK NORMAL.  (W)


REMARKS:
MIA - FLT 1814 - CLIMBING THROUGH 10,500 FEET, THERE WAS A VERY LOUD BANG FOLLOWED BY A PRESSURIZATION BUMP.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND THE FLEX DUCT DISCONNECTED ON THE LT PACK INLET TO THEWATER SEPARATOR.  MAINTENANCE PROPERLY SECURED THE DUCT.  LEAK AND OPS CHECKS NORMAL.  (W)


REMARKS:
GSO - DURING C-7 CHECK VISUAL INSPECTION FOUND 3 INCH CRACK OUTBD ATTACH ANGLE FOR NR 2 SLAT ACTUATOR.  REPAIRED PER TYPICAL REPAIR 57-20-01 A/ENGINEERING REPORT NR 07-07-90.  (W)


REMARKS:
BWI - EEL POWER PACK AND BATTERY, AFT OF SEAT 14 INOPERATIVE.  ALSO, THE EXTERIOR EMERGENCY LIGHTS FROM ROW 14 INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY POWER PACK.  THE LIGHTS CHECKED GOOD.  (W)


REMARKS:
ORY - FLT 1778 - THERE WERE NO EMERGENCY PATH LIGHTS IN THE AFT RT SECTION.  MAINTENANCE REPLACED THE EMERGENCY BATTERY.  OPS CHECKED GOOD.  (W)


REMARKS:
PHL - THE FLOOR LEVEL EMERGENCY LIGHT AT POSITION 34 FAILED THE RON TEST.  MAINTENANCE REPLACED THE BATTERY PACK.  OPS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 179 - FLIGHT EN ROUTE CLT TO MSP WHEN BOTH PACKS WENT FULL HOT.  UNABLE TO CONTROL TEMPERATURE OF AIR IN MANUAL OR AUTO.  DESCENDED TO FL250 AND BOTH PACKS BECAME CONTROLLABLE.  AIRCRAFT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE ACCOMPLISHED BITE TEST ON ZONE TEMP CONTROLLERS.  FOUND 2 FAULTS, CLEARED FAULTS.  REPLACED LT MIX MANIFOLD TEMP SENSOR.  (W)


REMARKS:
CLT - FLT 1157 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF FROM CLT.  LT PACK TRIPPED NUMEROUS TIMES, RIGHT PACK ON MEL.  AIRCRAFT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LT PACK PRIMARY AND SECONDARY HEAT EXCHANGERS.  (W)


REMARKS:
JFK - DURING C-CHECK, FOUND DELAMINATION OF HOT BOND REPAIR ON TOP INBOARD END OF NR 7 LEADING EDGE SLAT.  REPAIRED BY REMOVING OLD REPAIR AND HONEYCOMB CORE, REPLACED CORE PER SRM 51-70-10 AND INSTALLED HOT BOND REPAIR PER SRM 51-70-10, FIGURE 9.  TOTAL CYCLES 21,464.


REMARKS:
MCI - DURING OP-16, FOUND A 1.5 INCH CRACK IN CABIN FORMER RADIUS, STATION 2200, BETWEEN STRINGER 11R AND 12R.  STOP DRILLED CRACK PER SRM 51-10-01 AND REPAIRED PER ARA 8224.  TOTAL CYCLES 14,767.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON BELLY SKIN FROM FS 520 TO 590, STRINGER 44L TO 44R.  REPAIRED BY REPLACING SKIN PER ARA 8216.  TOTAL CYCLES 14,767.


REMARKS:
JFK - DURING C-CHECK, FOUND A ONE INCH CRACK IN FUSELAGE SKIN BETWEEN STRINGERS 28 AND 29, STATION 1745, AND FOUND FIVEDISTRESSED FASTENERS.  REMOVED CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-31-00, PAGE 828, FIGURE 815, AND REPLACED DISTRESSED FASTENERS.  TOTAL CYCLES 21,464.


REMARKS:
MCI - DURING OP-16, FOUND CRACK IN BULKHEAD WEB FS 400 LEFT SIDE, LBL 88, WL 160.  REPAIRED PER SRM 53-10-309, PAGE 210.  TOTAL CYCLES 14,767.


REMARKS:
JFK- DURING CRUISE, SMOKE AND ELECTRICAL SPARKS APPEARED FROM OVERHEAD LUGGAGE BINS AT ROWS 35 AND 36, SEATS 8 AND 9.  FLIGHT CREW DEACTIVATED FLOURESCENT CABIN LIGHTING BY TRIPPING CIRCUIT BREAKERS.  FOUND LIGHT BALLAST, MFG P/N 917-1, DEFECTIVE.  REPLACED BALLAST, RESET BREAKERS, AND OPS CHECKS NORMAL.  CHECK C-1.


REMARKS:
MCI - DURING OP-16, FOUND CRACKS ON FORWARD PRESSURE BULKHEAD RIGHT AND LEFT SIDE.  REPAIRED PER SRM 53-10-311.  TOTAL CYCLES 14,767.


REMARKS:
JFK - DURING C-CHECK, FOUND .5 INCH CRACK IN FUSELAGE SKIN BETWEEN STRINGERS 39 AND 40, STATION 1695.  REMOVED CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-31-00, PAGE 822.  TOTAL CYCLES 21,464.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON SKIN UNDER STRINGER 41L, BETWEEN FS 1700-1740.  REPAIRED BY ADDING EXTERNAL DOUBLER PER SRM 53-30-03, FIGURE 1.  TOTAL CYCLES 14,767.


REMARKS:
CLT - FLT 0002 - AFTER DEPARTURE, A FIRE WARNING ON ENGINE NR 2 WAS RECEIVED.  PER PROCEDURE, THE THROTTLE WAS PULLED BACK AND THE WARNING BELL STOPPED.  WHEN THE THROTTLE WAS AGAIN ADVANCED TO APPROXIMATELY 81 PERCENT, THE FIRE WARNING ACTIVATED AGAIN.  THE FLIGHT RETURNED TO CLT WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 ENGINE ANTI-ICE DUCT.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
LGA - THE EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER POPS WHEN FLIGHT DECK SWITCH IS PLACED IN THEOFF POSITION. MAINTENANCE REPAIRED CHAFED WIRE BETWEEN RIGHT AND LEFT LAVATORY BATTERY PACKS.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
PIT - FLT 0467 - THE FIRST LOWER LEVEL LIGHT WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE LOWER LEVEL EMERGENCY LIGHT SOCKET.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
PIT - FLT 0441 - AFTER TAKEOFF, THE SLAT DISAGREEMENT LIGHT CAME ON UPON SLAT RETRACTION.  THE LIGHT STAYED ON UNTIL THE SLATS EXTENDED AGAIN.  THE CREW RETURNED TO PIT.  MAINTENANCE REPLACED THE RIGHT SLAT RETRACT SWITCH.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
GSO - FLT 2158 - AFTER TAKEOFF, GEAR LEVER WOULD NOT MOVE TO THE UP POSITION.  RESET LEVER LATCH CIRCUIT BREAKER, NO HELP.  FLIGHT RETURNED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND PLUNGER IN LEVER LATCH SOLENOID STICKING.  LUBRICATED LEVER LATCH PLUNGER.  OPS CHECKED OK.  (Z)


REMARKS:
CLT - FLT 1079 - NR 2 ENGINE BIRD STRIKE ON TAKEOFF.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE PERFORMED BIRD STRIKE INSPECTION AND ENGINE RUN, NO DEFECTS NOTED.  AIRCRAFT OK FOR CONTINUED SERVICE.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND (4) CRACKS .5 INCH LONG, AT FRAME BS 767 LBBL 2.5 INCH AND RBBL 2.5 INCH BELLY.  REPAIRED PER SRM 51-40-3.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND LIGHTNING STRIKE ON FUSELAGE CROWN SKIN BETWEEN S-4 L AND S-6 L BS 470-540 (2 HEAVY STRIKES AT BS 535).  REPAIRED PER SRM 53-30-3 FIG 28, AND SRM 53-30-3 FIG 6.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SKIN WRINKLED 3 INCHES BY 8 INCHES BOTTOM SKIN BS 727 PLUS 10 INCHES ATRBL 6 INCHES.  REPAIRED PER EA 37457.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 3 INCH CORROSION S-27 R SPLICE BS 907 S-27 R.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01 CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL, INSPECTION FOUND LOWER SURFACE 1 INCH BY 1 INCH CORROSION BS 312 BS 328 RBBL 12 INCHES.REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 22 INCH CORROSION BS 270 LBBL 11 INCH, RBBL 11 INCH.  REPAIRED PER TR 53-20-04.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 44 INCH CORROSION BS 304 BS 348 LBBL 56 INCHES FORWARD ENTRY DOORZ ANGLE.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 1 INCH CORRODED INTERCOSTAL BS 277 TO BS 294 LBL 11 INCHES.  REPAIRED PER SRM 51-10-06.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 1 INCH BY 24 INCHES BS 320 RBL 46 TO RBL 22.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .25 INCH BY .22 INCH CORRODED AREA ON TOP OF FLOOR BEAM BS 259 AT LBL 11 THROUGH RBL 11.  REPAIRED PER TR 53-10-6.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 3 INCH CORROSION BS 294.5 LBL 11.  REPAIRED PER TR 53-10-04. CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT -DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH BY .060 STATION 344 LBL 11.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CORROSION FROM BS 294.5 TO BS 312 RBL 11.  REPAIRED PER SRM 51-3-02.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 16 INCH CORROSION RBL 12 INCHES FROM BS 344 TO 360.  REPAIREDPER SRM 51-10-1.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL NDT INSPECTION, FOUND 5 CRACKS .03125 INCH S-13 R BS 415.  REPAIRED PER SRM 53-30-3.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL INSPECTION, FOUND .03125 INCH CRACK AT S-13 R BS 377.  REPAIRED PER SRM 53-30-3.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL INSPECTION, FOUND 3 CRACKS .015625 INCH AT S-13 R BS 453 IN FASTENER HOLES.  REPAIRED PEREA 37529.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL NDT INSPECTION, FOUND CRACKS (4) PLACES .03125 INCH EACH, BS 397 S-13R.  REPAIRED PER SRM53-30-3.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL NDT INSPECTION, FOUND 3 CRACKS .03125 INCH S-10 L BS 500A AND S-13 L BS 500B.  REPAIRED PER SRM 53-30-3.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL NDT INSPECTION, FOUND CRACK .03125 INCH S-13 L BS 500A.  REPAIRED PER SRM 53-30-3.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL NDT INSPECITON, FOUND .25 INCH CRACK BS 520 PLUS 6D ROW RIVETS S-13L.  REPAIRED PER SRM 53-30-3.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL NDT INSPECTION, FOUND 4 CRACKS .015625 INCH AT FASTENER HOLES S-13 R BS 477.  REPAIRED PER EA 37530.  (Z)


REMARKS:
INT - DURING PCI CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION COVERING APPROXIMATLY 1 FOOT BY 1 INCH.  FLOOR BEAM AT STATION 259, UPPER CHORD.  REPAIRED PER EA 37527.  (Z)


REMARKS:
MCI - DURING OP-16 FOUND CRACK IN C-1 CARGO BIN UPPER FLANGE, STA 870, STRINGER 32L.  REPAIRED PER SRM 53-10-03, FIGURE1.  TOTAL CYCLES 14,767.


REMARKS:
JFK - DURING C-CHECK, FOUND A .1250 INCH CRACK IN FUSELAGE SKIN AT RT FORWARD CORNER OF NOSE WHEEL WELL, STA 328.  REPAIRED PER SRM 51-10-04.  TOTAL CYCLES 21,464.


REMARKS:
MCI - DURING OP-16 FOUND CRACK IN CARGO BIN LOWER FLANGE, FS 897, STRINGER 32L.  REPAIRED PER SRM 53-10-03, FIGURE 1.  TOTAL CYCLES 14,767.


REMARKS:
JFK - DURING C-CHECK, FOUND CORROSION AT INBD RADIUS OF INTERNAL SURFACE OF RT OUTBD FUSE PIN, ON RT PYLON.  REPLACED FUSE PIN PER 767 MM.  AIRCRAFT TOTAL CYCLES 12,051.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON SKIN SPLICE DOUBLER AFT OF FS 2180, BETWEEN STRINGERS 50L AND 51L.  REPAIRED PER ARA 8090A.  TOTAL CYCLES 14,767.


REMARKS:
LIS - FLT 900 - DURING CRUISE, THE RT VOR-DME CONTROL PANEL EMITTED SMOKE.  CIRCUIT BREAKERS WERE PULLED AND SMOKE DISSIPATED.  REPLACED PANEL, MFG PN 285T0554-5.  OPS CHECKS NORMAL.  CHECK C-6A, 8-2-94, JFK.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION IN FORWARD CARGO AREA, STRINGER 46L TO 47L CORD ANGLE, STA 986.  REPAIRED PER SB 747-53-2316.  TOTAL CYCLES 14,767.


REMARKS:
STL - DURING APPROACH WHEN LANDING GEAR WAS LOWERED, THE NOSE GEAR INDICATION WARNING LIGHTS FAILED TO INDICATE DOWN AND LOCKED.  REPLACED DEFECTIVE DOWNLOCK SWITCH, MFG, PN H14-6.  OPS CHECKS NORMAL.  CHECK C-10, 3-6-94, STL.


REMARKS:
STL - DURING C-CHECK, FOUND .3750 INCH CRACK IN BELT RING, STA 756, LONGERON 3R.  REPLACED LONGERON SECTION PER SRM 53-02, FIGURE 2.  TOTAL CYCLES 73,518.


REMARKS:
STL - DURING C-CHECK, FOUND A .5 INCH CRACK IN LONGERON 12R, STA 965.  REPAIRED PER RM 53-02, FIGURE 2 AND STANDARD PRACTICES.  TOTAL CYCLES 73,518.


REMARKS:
JFK - DURING C-CHECK, FOUND CRACK IN RT PYLON INBD MIDSPAR FUSE PIN.  REPLACED PIN PER SB 767-54A0062.  TOTAL CYCLES 11,421.


REMARKS:
JFK - DURING SPECIAL CHECK, FOUND A 5 INCH CRESCENT SHAPE CRACK IN NR 3 PYLON INBD SIDE AT FORWARD END OF LOWER PYLON ACCESS PANEL.  REPAIRED PER SRM 54-30-03, FIGURE 17.  TOTAL CYCLES 12,276.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION IN FORWARD CARGO AREA ON STRINGER 47L, STA 960 TO 980, AND STA 970 TO 986.  REPAIREDPER SRM 53-10-03.  TOTAL CYCLES 14,767.


REMARKS:
EXPERIENCED BIRDSTRIKE TO NUMBER 2 ENGINE, RESULTING IN ENGINE COMPRESSOR STALL AND SLIGHT SMOKE IN CABIN.  AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRDSTRIKE INSPECTION AND ENGINE POWER ASSURANCE RUN WITH NO DEFECTS NOTED.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND STRINGER 27L CORRODED AT BS 947 THROUGH 957.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND STRINGER 26L CORRODED AT BS 907.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LOWER FUSELAGE SKIN CRACK 4 INCHES AFT OF BS 867, STRINGER 25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LOWER FUSELAGE SKIN CRACK AT  BS 867, STRINGER 25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING MAINTENANCE REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL REPAIR VISIT, FOUND FORWARD CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING MAINTENANCE REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD ENTRY DOOR INTERCOSTAL WEB CRACKED AT BS 306, STRINGER 4L, WL 291.  REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORROSION AT BS 999, LBL 12, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
SPECIAL REPAIR VISIT, ACCOMPLISHED REPAIR TO CRACKS FOUND AT BS 178, WL 181-200, LBL 6, PRESSURE BULKHEAD WEB CRACKED 25 INCHES EXTENDING UP FROM 651630093 STIFFENER TO 651630090 STIFFENER, THE 651630049 STRAP CRACKED 1 INCH LONG AROUND RIVET HEADS, LOCATED FWD SIDE OF BULKHEAD AND AFT SIDE OF BULKHEAD T CHORD 651758347 CRACKED 6 INCH IN RADIUS.  DOUBLER AND SPLICE PLATE INSTALLED PER REPAIR DRAWING ASA SWA-FT-003 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
SPECIAL REPAIR VISIT, ACCOMPLISHED REPAIR TO 2 FOOT CRACK FOUND AT BS 663.75, WL 191.5, RBL 70.  REAR SPAR BULKHEAD FITTING 6567740504 THROUGH INBOARD FLANGE EXITING UNDER BATH TUB FITTING, LOCATED APPROX 20 INCH UP FROM BOTTOM EDGE.  REPLACED PER BOEING S/B 737-53-1082 R3, PART III AND 737 -53-1110.


REMARKS:
IN FLIGHT, EXPERIENCED BIRDSTRIKE TO NUMBER 2 ENGINE.  AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRDSTRIKE INSPECTION AND ENGINE POWER ASSURANCE RUN, NO DEFECTS NOTED.


REMARKS:
FOUND CABIN FLOOR TRACK LIGHTING INOP IN AFT CABIN AREA.  REPAIRED SHORTED FLOOR TRACK LIGHTING AT ROW 17 AND REPLACED RIGHT BATTERY PACK AT BASE BS 947.


REMARKS:
IN FLIGHT, FIRST OFFICERS ALTIMETER WENT INOP.  AIRCRAFT DIVERTED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACED INDICATOR PER BOEING M/M.


REMARKS:
IN FLIGHT, NUMBER 1 L/E SLAT CREEPS DOWN IN FLIGHT.  AIRCRAFT DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACEDSLAT ACTUATOR PER BOEING M/M.


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETER CORROSION S-5 R STATION 440.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORROSION 26 L F/S 540 ON STRINGER.  REPAIRED PER SRM 53-10-01.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH STATION 323.7 AT STR 28R.  REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 20 INCHES LONG, .1875 INCH WIDE STATION 480 TO STATION 500 S-6 R.  REPAIRED PER SRM 53-10-3, FIG 4.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETER CORROSION S-5 R STATION 420.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STATION 987.5 RBL 43 INCH.  REPAIRED PER TR 53-10-05 AND SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION NUMEROUS AREAS AT STATION 987.5 FULL WIDTH OF AIRCRAFT.  REPAIRED PER TR 53-10-05 REV C.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION STATION 312, RBL 32.  REPAIRED PER TYPICAL REPAIR 53-10-13.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 2 INCH CORROSION STATION 380 RBL 55.  REPAIRED PER TP 53-10-01A.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 2 INCH MORE THAN 30 INCHES MATERIAL LOSS, CORROSION FLOOR BEAM CORRODED STATION 294.5 10 INCHES LBL.  REPAIRED PER TR 53-10-04B, CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 33 INCH STA 947.6 TO STATION 980 RBL 48.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 33 INCH STA 947 TO 980 LBL 48.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .25 INCH BY .015 INCH CORRODED AREA SHEAR TIE ON BS 727 A FRAME AT S-22L.  REPAIRED PER SRM 51-10-1, 51-30-2.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY .5 INCH BY 1 INCH AREA OF SURFACE CORROSION, STATION 1006, LBL 11.  REPAIRED PER EA 37496.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA BL 0 BETWEEN BS 767 AD 788 (BELLY SKIN).  REPAIRED PER SRM 51-10-1 AND 51-30-2.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY .5 INCH CRACK STATION 520 FLOOR BEAM UPPER CHORD AFT FLANGE RADIUS AT LBL 25.  REPAIRED PER EA 37458.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION FOUND APPROXIMATLY 1 INCH CRACK STATION 520 FLOOR BEAM UPPER CHORD AFT FLANGE RADIUS AT RBL 23.  REPAIRED PER EA 37458.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY .5 INCH CRACK STATION 520 FLOOR BEAM UPPER CHORD AFT FLANGE RADIUS AT RBL 4.  REPAIRED PER EA 37458.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 4 INCHES BS 312 AT RBL 37 INCHES.  REPAIRED PER SRM 53-10-13.  CORROSION TASK NR C53-107-01.  CORROSION LEVEL 2. P/N BAC1505100246707T6 (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 60 INCHES CORRODED AREA ON FLOOR SUPPORT TRACK BS 787-847 AT RBL 13.5.  REPAIRED PER SRM 53-10-5, FIG 11.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION BS 312 LBBL 56 INCHES ON GIRT BAR.  REPAIREDPER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION BS 344 LBBL 56 INCHES ON GIRT BAR.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SRM 51-10-1.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA BS 270 TO 283 LBL 10 INCHES ON INTERCOSTAL.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK FLOOR BEAM BS 520 RBBL 24.75.  REPAIRED PER EA 37441.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION FOUND .25 INCH CRACK IN FORWARD RADIUS OF LOWER HINGE ARM CUTOUT ON FUSELAGE FOR FORWARD SERVICE DOOR.  REPAIRED PER SB 53-10-74 AND EA 37442.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CRACK IN 2 INCH SUPPORT ANGLE, CRACK IN 1 INCH FLOOR BEAM BS 520 LBBL 25 INCHES.  REPAIRED PER EA 37411.  (Z)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION FOUND 1 INCH CRACK AFT CARGO VERTICAL STIFFENER RT KEEL BEAM RBL 6.5 ON BACKSIDE OF 727 BULKHEAD 4 INCHES ABOVE BELLY SKIN.  REPAIRED PER SRM 51-10-1.  (Z)


REMARKS:
CLT - FLT 1850 - ON DEPARTURE FROM CLT, THE RIGHT ENGINE HYDRAULIC PRESSURE LOW LIGHT CAME ON .  THE PRESSURE GAUGE SHOWED RAPID DROP.  NO QUANTITY LOSS WAS NOTED.  THE AIRCRAFT RETURNED TO CLE WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE DRIVE HYDRAULIC PUMP.  THE LEAK CHECKED NORMAL.  (Z)


REMARKS:
PHL - FLT 1877 - AFTER TAKEOFF, TWO COLUMNS ON THE LEFT AND RIGHT ANNUNCIATOR PANEL ILLUMINATED WITH MULTIPLE FALSE WARNINGS.  THE CREW RETURNED TO PHL WITHOUT INCIDENT.  MAINTENANCE REPLACED THE ANNUNCIATOR PANEL AND DIMMING SWITCH.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
CLT - FLT 1625 - AFTER TAKEOFF, THE NOSE GEAR LIGHT WAS RED DURING RETRACT.  THE CREW LOWERED THE GEAR AND RETURNED TO CLT WITHOUT INCIDENT.  MAINTENANCE REPLACED THE ARM-LOCK LINK SPRING ATTACHMENT AND PIN-UPPER LOCK LINK.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
BWI - FLT 0311 - EN ROUTE TO PHL, THE NR 2 ENGINE THROTTLE WAS STUCK IN CRUISE POWER.  THE CREW SHUTDOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY, AND DIVERTED TO BWI.  SINGLE ENGINE TIME WAS 22 MINUTES.  MAINTENANCE SECURED THE CROSS SHAFT THROTTLE LINKAGE, INSPECTED THE CHIP DETECTOR, REPLACED THE OIL SCREEN AND PERFORMED A LINKAGE STATIC CHECK.  OPERATIONSCHECKED NORMAL.  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND A 1.5 INCH CRACK AT LONGERON 13L SKIN CLIP AT STATION 1019.  INSTALLED MANUFACTURED SKIN CLIP ANGLES AND FILLER PER USAIR EA 26940.  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND .75 INCH CRACK IN LONGERON 11R INTERCOSTAL STATION 160.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-10-09.  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND .75 INCH CRACK STATION 110 LEFT SIDE AFT NOSE GEAR DOOR HINGE CUT OUT SKIN.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 62.  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND .4375 INCH CRACK STATION 965 RT AFT BULKHEAD WEB, (REAR PRESSURE BULKHEAD).  INSTALLED WEBAND STIFFENERS PER DOUGLAS SRM 53-03, FIG 19.  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND .625 INCH CRACK AT STATION 965 LONGERON 10R AND 13 ON FORMER.  REPAIRED FORMER PER DOUGLASSRM 53-03 FIG 3.  (Z)


REMARKS:
DURING Q-4 INSPECTION, FOUND .5 INCH CRACK IN LONGERON 14L AT STATION 965.  SPLICED IN NEW LONGERON PER USAIR TYPICAL REPAIR NR 53-10-17, FIG 2.


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT, FOUND CORROSION IN FWD CARGO BIN, LOWER BEAM.  DOOR FRAME STRUCTURE HAS CORROSION AROUND MISC HARDWARE.  INSTALLED NEW LOWER PANE ASSY AND DOUBLER REPAIR PER DOUGLAS SRM 53-05 FIG 44 AND USAIR EA 27133.  (Z)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT, FOUND PREVIOUS TEMP REPAIR INSTALLED, STATION 996 LONGERON 16R.  REMOVED AND REPLACED REPAIR WITH DOUBLER TYPE PER DOUGLAS SRM 53-04 FIG 17 AND USIAR EA NR 27205.  (Z)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT, FOUND FORWARD CARGO DOOR HAD SMALL PIECES OF MATERIAL MISSING ANG BROKEN OUT OF FORWARD LOWER CORNER.  INSTALLED DOUBLER REPAIR PER SRM 52-05 FIG 4.  (Z)


REMARKS:
DURING AGING AIRCRAFT MAINTENANCE VISIT, FOUND TEMPORARY REPAIR INSTALLED IN RT WHEEL WELL IN AREA OF CEILING PRESSURE PANEL.  REMOVED TEMP REPAIR AND INSTALLED DOUBLER TYPE REPAIR PER DOUGLAS SRM 53-05 FIG 19.  (Z)


REMARKS:
DURING Q-CHECK INSPECTION ACCOMPLISHED SIDE PSE NR 53.09.031 USAIR WORKCARD NR J9-46-80146 AND FOUND A .25 INCH CRACK IN THE SKIN AT THE TOP AFT MAIN ENTRANCE DOOR STOP HOLE AT STATION 200.  INSTALLED DOUBLER PER DOUG SRM 53-05 FIG 26A.  (Z)


REMARKS:
PIT - FLT 1146 - THE SLAT DISAGREEMENT LIGHT REMIANED ON AFTER THE FLAP RETRACTION SLATS APPEARED TO HAVE BEEN UP.  THEAIRCRAFT RETURNED TO FIELD.  MAINTENANCE CLEANED AND LUBED THE SLAT ETRACK AND TRACK DOORS AND SWITCHES.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
MCO - FLT 1164 - RETURN TO FIELD, UNABLE TO PRESSURIZE IN PRIMARY OR STANDBY.  THE AFT PRESSURE CONTROLLER FAILED BITE AND WOULD NOT TRANSFER TO STANDBY.  MAINTENANCE REPLACED THE AFT CONTROLLER.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
LAX - DURING SPECIAL DEPLOYMENT CHECK OF PASSENGER EVACUATION SLIDE, L4 DOOR SLIDE DID NOT DEPLOY WHEN THE DOOR WAS OPENED.  THE SLIDE CAME OFF THE DOOR AND FELL TO GROUND LEVEL.  APPARENTLY, ONE SIDE OF GIRT BAR WAS NOT ENGAGED TO THE FLOOR FITTING THEREBY ALLOWING MISALIGNMENT, RESULTING IN THE SLIDE BEING PULLED FROM THE DOOR.  THE SLIDE, MFG PN D29401-539, WAS REPLACED, AND GIRT BAR RIGGING OF AIRPLANE WAS CHECKED AND FOUND NORMAL.  TOTAL CYCLES 22,521.


REMARKS:
PILOT NOTICED LOW OIL QUANTITY DURING FLIGHT 115, RETURNED TO ATL.  FOUND LOOSE OIL CAP, RESERVICED ENGINE OIL WITH 10 QUARTS OF OIL, REINSTALLED CAP PER MM 12 AND 79, OPS CHECKED GOOD.


REMARKS:
FRONT ENTRY DOOR OUT OF RIG CAUSING LACK OF PRESSURIZATION AND PASSENGER DISCOMFORT.  AIRCRAFT RETURNED TO ATL FLT NR 142.  REPLACED DOOR SEAL DUE TO SEAL BEING DAMAGED BY OUT OF RIG DOOR.  RERIGGED DOOR PER MM52-00.  (Z)


REMARKS:
SLC - RETURNED FROM FLIGHT ACCOUNT LEFT ENGINE INCURRED A LOW RUMBLE AND VIBRATION.  REDUCED POWER AND LANDED.  FOUND METAL IN MAIN OIL SCREEN.  REPLACED ENGINE S/N 1208.


REMARKS:
AT TPA, FLT 81 - TPA TO ATL - ON TAKEOFF, WHEN FLAP SELECTED TO 5 DEGREES, RT INBOARD TRAILING FORE FLAP WENT TO 5 DEGREES AND THE LEFT WENT ONE NEEDLE WIDTH MORE THAN 5 DEGREE, ON VISUAL INSPECTION INDICATION WERE CONFIRMED.  FOUND LEFT INBOARD FLAP TORQUE TUBE SEPARATED AT INBOARD FLAP PCU, INSPECTED PCU TORQUES TUBES, GR BOXES, TRANS AND JACKSCREWS, ALL OK, INSTALLED NEW HARDWARE, SAFETIED AND RIGGED INBOARD TRAILING EDGE FLAPS PER MM 27-51-01.  OPS CHECK OK.  (Z)


REMARKS:
AT EWR FLT NR 7, EWR-ATL - UPON LEVELING OFF AIRCRAFT BANKING TO LEFT, RUDDER INPUT DISENGAGED BY FLT CREW, AIRCRAFT CHARACTERISTICS BECAME NORMAL.  REMOVED AND REPLACED LOWER YAW DAMPER PER 22-11-31 AND REMOVED AND REPLACED AIR DATA COMPUTER PER 34-12-12.  OPS CHECKED OK.  (Z)


REMARKS:
NEWARK - FLT 57 - DEPARTED AT 2115Z.  DURING CLIMB-OUT, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT CABIN.  THE AIRCRAFT RETURNED TO NEWARK AT 2135Z.  MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE R-1 DOOR NOT FULLY CLOSED.  THE LOWER HOOKS OF THE R-1 DOOR WERE NOT ENGAGED.  MAINTENANCE INSPECTED THE DOOR AND DOOR INDICATION SYSTEM, CHECKED NORMAL.  (X)


REMARKS:
TPA/MDW - FLT 42 - EN ROUTE, NR 1 ENGINE WOULD NOT RESPOND TO AIRCRAFT THROTTLE MOVEMENT.  AS A PRECUATIONARY ACTION, AN IN-FLIGHT SHUT DOWN WAS ACCOMPLISHED.  AN EMERGENCY WAS DECLARED.  AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND A BOLT MISSING FROM FUEL CONTROL UNIT ROD LINKAGE AT THE FCU.  REPLACED BOLT, NUT AND COTTER PIN.  OPS CHECKED NORMAL. TOTAL CYCLES, 83.  (X)


REMARKS:
ATL - FLT 88 - AFTER STARTING NR 2 ENGINE, AIRCRAFT RETURNED TO GATE WITH NR 2 ENGINE ICING LIGHT ILLUMINATED.  MEL ASSIGNED.  MAINTENANCE REPAIRED WIRING TO FUEL FILTER PRESSURE SWITCH.  (X)


REMARKS:
FLT 39 - DEPARTED EWR TO TPA.  EN ROUTE LT PACK IN PPED CABIN PRESSURE WENT TO FULL 2000 FPM.  CABIN OXYGEN MASK DEPLOYED AC RETURNED TO EWR.  MAINTENANCE REPACKED O2 MASK.  ACCOMPLISHED PRESS CHECK.  LT PACK ISOLATION VALVE AND RT OUTFLOWVALVE FAILED.  SEE REPORT IXKA940025.   REFERENCE CONTROL NR 94ZZZW2710. (W)


REMARKS:
JFK - DURING C-CHECK, FOUND CORROSION INSIDE OF PIN BORE ON NR 2 PYLON OUTBD MIDSPAR FUSE PIN.  REPAIRED BY REPLACING OTBD MIDSPAR FUSE PIN PER 767 MM 54-51-02, PAGE 401.  TOTAL CYCLES 11,945.


REMARKS:
LGA - FLT 546 - DURING DESCENT, NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON.  SHUT DOWN ENGINE.  FOUND METAL PARTICLES IN MAIN OIL SCREEN.  REPLACED ENGINE SN 1527.  ENGINE TOTAL TIME 31,838 HOURS, 20,237 CYCLES.  CHECK C-2, 7-15-94, MCI.


REMARKS:
STL - FLT 530 - RETURNED FROM FLIGHT ACCOUNT THE RT ENGINE FIREWARNING CAME ON SHORTLY AFTER TAKEOFF.  FOUND THIRTEENTHSTAGE FUEL HEAT PNEUMATIC HEAT DUCT FAILED AT FLANGE JOINT.  REPLACED DUCT, MFG PN 577957.  OPS CHECKS NORMAL, CHECK C-9, 11-21-93, STL.


REMARKS:
FLT 235 - AIRCRAFT ON FINAL APPROACH INTO DFW, CREW PLACED THE FLAP TO 50 DEGREE POSITION AT WHICH TIME THE CREW HEARD A LOUD POP.  AIRCRAFT LANDED WITHOUT INCIDENT.  INSPECTION REVEALED THE RT INBD WING FLAP HINGE BROKEN.  REPLACED WING FLAP HINGE, OPS CHECK GOOD PER MM 27-00.


REMARKS:
ATL-FLL - FLT 219 - RADAR TRIPS CIRCUIT BREAKER AND COULD NOT CONTINUE FLIGHT INTO KNOWN THUNDERSTORMS, RETURNED TO ATL.  REPLACED RECEIVER TRANSMITTER, PLANE TAXIED OUT AND THEN RETURNED TO THE GATE WITH THE SAME TROUBLE.  SWAP WITH AIRCRAFT 914.  REMOVED AND REPLACED RADAR CONTROL PANEL, OP CHECKS GOOD PER MM 34-00.


REMARKS:
FLT 225 - AIRCRAFT EN ROUTE TO PHL EXPERIENCE HIGH OIL TEMPERATURE BECAUSE OF A LOSS OF ENGINE OIL IN NR 1 ENGINE.  FLIGHT DIVERTED TO IAD.  DECLARED AN EMERGENCY AFTER SHUTTING NR 1 ENGINE DOWN WHEN OIL PRESSURE DROPPED TO 35PSIG AND OIL QUANTITY WENT TO 2 QTS.  MTC CAME FROM ATL, RESERVICED WITH OIL.  RAN ENGINE AT IDLE AND MAX CONTINUOUS POWER.  NO LEAKSNOTED.  FOUND FUEL HEAT TIMER INOP.  SYSTEM CHECKS OK.


REMARKS:
FLT 226 - AIRCRAFT EN ROUTE TO PHL EXPERIENCED ERRATIC PRESSURIZATION WHILE AT FL 220.  CABIN PRESSURE ALTITUDE WAS CLIMBING IN AUTO AND MANUAL MODE.  PRESSURE REGULATOR WAS REPLACED AND ALL OXYGEN MASKS REINSTALLED AND DROP CHECKED PER MM35-00.


REMARKS:
ON APPROACH TO ATL, FLT 177, NR 1 ENGINE OIL PRESSURE DROPPED BELOW 35 PSI, LOW OIL PRESSURE LIGHT CAME ON, AND OIL QUANTITY WENT FROM 16 QTS TO 2 QTS.  PILOT SHUT DOWN THE ENGINE BEFORE QUANTITY AND PRESSURE GOT TO ZERO.  LANDED WITHOUT INCIDENT.  REPLACED NR 1 ENGINE.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY DOOR LOWER BOTTOM WEB AT AFT CONTROL ROD LIGHTENING HOLE DAMAGED ONUPPER RADIUS.  INSTALLED REPAIR DOUBLER PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 344 BETWEEN S21R - S22R.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT MAIN WHEEL WELL STRINGER 18A SHEAR BEAM AT AFT END ATTACH CRACKED.  REPAIRED PER SWA RA 1-353-1144.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD FRAME OF ESCAPE EXIT AT BS 616  CRACKED BELOW CREASE BEAM RBL 64.5.  REPAIRED PER SWA RA 1-353-1145.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER CLIP TO BELT FRAME CRACKED AT BS 663.75.  REPLACED CLIP PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB ANGLE CRACKED BETWEEN BS 500 AND 520.  REPLACED ANGLE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND SUPPORT CHANNEL CRACKED BETWEEN BL 0 AND 24.  REPLACED CHANNEL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB ANGLE CRACKED BETWEEN BS 927 AND 947.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND Z ANGLE CORRODED, BS 281.5, RBL 52.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAMS CORRODED AT BS 986, RBL 14, 23, 31, 43.  REPAIRED PER SWA RA 1-353-1153.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAMS CORRODED AT BS 986, LBL 26, 30, 31 , 35, AND 43.  REPAIRED PER SWA RA 1-353-1152.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND Z ANGLE CORRODED AT BS 280, RBL 26, 53.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND DOOR FRAME CRACKED AT BS 294.5, RBL 55.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND L ANGLE CRACKED IN TOP SUPPORT STRUCTURE FOR RH RAM AIR DOOR AT BS 540, JUST ABOVE S22R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STABILIZATION STRAP BELOW FLOOR BEAM CRACKED AT BS 344, LBL 46.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 986, RBL 25.  REPAIRED PER SWA RA 1-353-1148.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 328, RBL 21.5.   REPAIRED PER SWA RA 1-353-1150.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND VERTICAL STABILIZER RIGHT SIDE DENTED, 36 INCHES FROM TOP.  REPAIRED PER SWA  RA 1-355-181.


REMARKS:
FOUND 2 DENTS ON UNDERSIDE OF FUSELAGE AT AFT CARGO DOOR.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND HOLE IN FUSELAGE SKIN AT BS 947.5, BETWEEN S27R AND S28L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND RIGHT WING TO BODY CHORD CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND Z CHANNEL CORRODED AT BS 270, WL 208, BL 0 TO 11R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 5 AND RBL 10 TO 15, WL 208.  REPAIRED PER TRAMCO EWO 94-0629.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM VERTICAL WEB CRACKED AT BS 710, WL 204, RBL 25.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED  BS 178, WL 235, RBL 10.  REPAIRED PER TRAMCO EWO 94-0613.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKIN DENTS AT BS 502, BETWEEN S21R AND S22R, AT BS 288, BELOW S24L, AND AT BS 322, S18R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW S7L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 4, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AND OIL CANNING AT BS 840, WL 214, 6 INCHES ABOVE S17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST OUTER SKIN CRACKED .75 INCHES AT UPPER CORNER.  REPAIRED PER SWA RA 1-353-1155 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND SEVERAL FLOOR TRACK LIGHTS INOP.  REPAIRED WIRES PER BOEING M/M.


REMARKS:
FLIGHT 4356, AFTER TAKEOFF, OVERRIDE HANDLE WAS USED TO RAISE GEAR.  AIRCRAFT RETURNED TO LAX AND MADE AN UNEVENTFUL LANDING.  RIGGED RIGHT MAIN GEAR GROUND SHIFT CABLE AND PERFORMED GEAR RETACT TEST PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND WING LIGHT ILLUMINATION STRINGERS 16L AND 16R CRACKED AT WS 500C.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AND OIL CANNING AT BS 394, WL 210.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FORWARD GALLEY DOOR CUTOUT CRACKED AT UPPER FORWARD CORNER.  REPAIRED PER BOEING DRAWING 65C33800 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT SERVICE DOOR FORWARD FRAME CRACKED AT BS 957, RBL 65, WL 265.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO LAX AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND NOSE GEAR UPLOCK ACTUATOR FITTING LEAKING.  REPLACED UPLOCK ACTUATOR HYDRAULIC FITTINGS AND LINES.  PERFORMED GEAR RETRACT TEST PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE BROKEN AT BS 887, LEFT SIDE, WL 230.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, RBL 25 TO LBL 25.  REPAIRED PER SWA RA 1-353-421 R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN FASTENER HOLE ELONGATED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FORWARD GALLEY DOORWAY UPPER CORNERS CRACKED.  REPAIRED PER SWA ACO 3167-53.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663.75, S10R, S10L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND VERTICAL STRIFFENER CRACKED AT BS 727, RBL 18, WL 154.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND APU ACCESS DOOR DENTED AND GOUGED BETWEEN RIBS 4 AND 5.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, AT STRINGER 1 AND AT BS 500, BETWEEN S24 AND 25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN  DENTS AT BS 992, BETWEEN STRINGERS 23 AND 24L, AT BS 880, BELOW STRINGER16L, AT BS 360, 8 INCHES AFT OF S18R, AT BS 360-375, S4 AND 6L, AND AT BS 417, AT S24R.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, BETWEEN STRINGERS 10L AND 10.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FAIL/SAFE CHORD CRACKED AT BS 827, S27R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM VERTICAL WEB CRACKED AT BS 709-710, WL 204.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM VERTICAL WEB CRACKED AT BS 709-712, BBL 0, WL 204.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, UNDER S3L.  REPAIRED PER SWA EWO 94-0615.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 727-907, S20-25 LEFT AND RIGHT.  REPLACED SKINS PER BOEING DRAWING 65-45174-67, 66, AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 12 TO RBL 21, WL 207.  REPAIRED PER SWA RA 1-353-418.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT BS 667, WL 207, LBL 25.  REPAIRED PER SWA EWO 94-0640.


REMARKS:
DURING SCHEDULED D CHECK, FOUND VERTICAL WEB AT AFT CARGO DOOR CRUSHED IN 7 PLACES.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AFT BAY VERTICAL WEB CORRODED FROM BS 847 TO 867, RBL 18, WL 160.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER 3R CRACKED AT BS 663.  REPAIRED PER TRAMCO EWO 94-0615.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AFT GALLEY DOOR CUTOUT LOWER LATCH CUTOUT CRACKED.  REPAIRED PER TRAMCO EWO 94-0630.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKATE ANGLE CRACKED AT BS 560, WL 150, RIGHT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD GALLEY DOORWAY SKIN CUTOUT UPPER CORNERS CRACKED.  REPAIRED PER SWA ACO 3167-53.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 15 TO LBL 20.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SEAT TRACK SUPPORT CHANNEL CRACKED AT BS 520, RBL 45.5.  REPAIRED PER SWA ACO 3198-53.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 987, WL 208, RBL 24 TO LBL 15.  REPAIRED PER SWA RA1-353-542.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, RBL 25 TO LBL 45, WL 208.  REPAIRED PER SWA RA 1-353-427 R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CRACKED AT BS 520, RBL 45, WL 207.5.  REPAIRED PER SWA ACO 3198-53 AND SB 737-53-1120.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS AT CRACKED AT BS 1147, S13R AND AT BS 1129, STRINGER 13R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 25L DAMAGED AT BS 395.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, NUMBER 2 ENGINE EGT INDICATOR FAILED.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACED EGT TRANSMITTER CANNON PLUG PINS AT NUMBER 2 ENGINE FIREWALL AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU AIR INLET CUTOUT STRUCTURE UPPER CHORD AND AROUND INLET AREA CORRODED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 882, 1 INCH BELOW S22R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, LEFT MAIN GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  REPLACED LEFT LANDING GEAR CONTROL MODULE AND PERFORMED GEAR RETRACTION TEST PER BOEING MAINTENANCE MANUAL.


REMARKS:
IN FLIGHT, EXPERIENCED A SYSTEM HYDRAULIC FAILURE.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  INSPECTEDAND FOUND NUMBER 2 BRAKE LEAKING.  REPLACED BRAKE ASSEMBLY AND INSPECTED A SYSTEM FILTERS, NO DEFECTS NOTED.


REMARKS:
FOUND CABIN FLOOR TRACK LIGHTING AT OVERWING EXIT INOP.  REPAIRED BROKEN WIRE PER BOEING M/M.


REMARKS:
BWI - FLT 1697 - FLIGHT EN ROUTE BDL TO DCA WHEN AFT CARGO DOOR WARNING LIGHT ILLUMINATED.  AIRCRAFT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED SENSOR.  (X)


REMARKS:
LGA - SERVICE DOOR EMERGENCY LIGHT INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK.  (X)


REMARKS:
BWI - FLT 2147 - AFTER TAKEOFF, AUTO PRESSURE FAIL LIGHT ILLUMINATED.  SHORTLY THEREAFTER NR 1 TR AND EQUIPMENT COOLINGCIRCUIT BREAKER TRIPPED.  NR 1 GENERATOR WENT OFF LINE.  FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 1 GENERATOR.


REMARKS:
PIT - FLT 2332 - FLIGHT EN ROUTE CMH TO BOS WHEN 'A' HYDRAULIC QUANTITY SLOWLY DECREASED TO 1.4 GALLONS.  FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE SERVICE HYDRAULICS.  NO LEAKS NOTED.  (X)


REMARKS:
TPA - FLT 350 - UNABLE TO RETRACT LEFT MAIN GEAR AFTER TAKEOFF.  FLIGHT CONTINUED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT MAIN GEAR TRUNNION PIN.  OPS CHECK GOOD.  (X)


REMARKS:
CLT - FLT 99 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF IN AUTO OR STANDBY.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED PRESSURIZATION CONTROLLER.  OPS CHECK GOOD.  (X)


REMARKS:
PIT - FLT 2347 - FLIGHT EN ROUTE ROC TO CLT WHEN LOST OIL PRESSURE ON NR 2 ENGINE.  REDUCED ENGINE TO IDLE AND DIVERTEDTO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED RIGHT ENGINE DUE TO OPERATION AT LOW OIL PRESSURE.  (X)


REMARKS:
MCI - FLT 93 - FLIGHT EN ROUTE IND TO PHX WHEN AIRCRAFT HAD INTERMITTENT NR 2 ENGINE OVERHEAT LOOP FAULT INDICATIONS ONBOTH 'A' AND 'B' LOOPS.  FLIGHT DIVERTED TO MCI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND HP VALVECLAMPS LEAKING.  RETIGHTENED CLAMP.  REPLACED P8-1 PANEL FIRE LOOP.  OPS CHECK GOOD.  (X)


REMARKS:
LAS - FLT 1125 - ON CLIMB OUT OF LAS, NR 2 LED GREEN LIGHT REMAINED ON.  CYCLED FLAPS SEVERAL TIMES, NO CHANGE.  FLIGHTRETURNED TO LAS WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED FLAP/SLAT ACCESSORY UNIT.  CHECKS OKAY.  (X)


REMARKS:
GSO - DURING 'C-16' CHECK, VISUAL INSPECTION FOUND 4 INCH CRACK TOP FRAME AFT END OF FORWARD ENTRY DOOR.  DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER.  (X)


REMARKS:
INT - DURING 'CX5' EDDY CURRENT AND VISUAL INSPECTION FOUND .3125 INCH AND .5625 INCH LONG CRACKS LOWER AFT CORNER OF FORWARD GALLEY DOOR CUTOUT BS 332.0.  REPAIRED PER E.A. 37301.  (X)


REMARKS:
INT - DURING 'CX5' VISUAL INSPECTION FOUND 2 INCH BY 5 INCH CORRODED AREA, BS 727, STR 27R.  REPAIRED PER E.A. 37309 AND E.A. 37310.  (X)


REMARKS:
CLT - FLT 70 - FLIGHT EN ROUTE TPA TO IND WHEN AT FL 310 ALTITUDE WARNING HORN SOUNDED AND OXYGEN MASKS DEPLOYED.  UNABLE TO CONTROL PRESSURIZATION IN ALL MODES.  FLIGHT DESCENDED TO FL 100 AND DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND BLOWN DUCT IN LEFT PACK BAY.  REPLACED DUCT.  PRESSURIZATION CHECK OKAY.  (X)


REMARKS:
ATL - FLT 1053 - FLIGHT EN ROUTE CLT TO DFW WHEN NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED IN-FLIGHT.  CREW SHUT DOWN NR 2 ENGINE.  FLIGHT DIVERTED TO ATL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND STARTER GARLOCK SEAL LEAKING.  REPLACED SEAL ON NR 2 ENGINE AND ACCOMPLISHED LEAK CHECK.  NO LEAKS FOUND.  (X)


REMARKS:
ORF - FLT 26 - FLAPS LOCKED OUT AT 5 UNITS ON RETRACTION AFTER TAKEOFF.  ALT FLAPS USED TO SET FLAPS 15 FOR LANDING.  FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED FLAP POSITION INDICATOR.  (X)


REMARKS:
SYR - FLT 1105 - AIRCRAFT DIVERTED TO SYR DUE TO AN INOPERATIVE VOR NAVIGATION RECEIVER.  MAINTENANCE REPLACED THE NR 2VOR NAVIGATION RECEIVER.  OPERATIONS CHECKED NORMAL.  (X)


REMARKS:
CLE - THE CENTER CEILING EMERGENCY LIGHTS WERE FOUND INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  (X)


REMARKS:
BOS - FLT 0453 - AFTER TAKEOFF, AIRCRAFT BANKED TO THE RIGHT AND OBSERVED 'RUDDER CONTROL MANUAL' AND 'R HYD PRESS LOW'.  THE AIRCRAFT RETURNED TO FIELD.  MAINTENANCE REPLACED THE RIGHT ENGINE HYDRAULIC PUMP.  OPERATIONS CHECKED NORMAL.  (X)


REMARKS:
PIT - THE OVER WING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE.  MAINTENANCE REPLACED THE BATTERIES.  OPERATIONS CHECKED GOOD.  (X)


REMARKS:
FLT 39 - DEPARTED EWR TO TPA.  EN ROUTE LT PACK IN PPED CABIN PRESSURE WENT TO FULL 2000 FPM.  CABIN OXYGEN MASK DEPLOYED AC RETURNED TO EWR.  MAINTENANCE REPACKED O2 MASK.  ACCOMPLISHED PRESS CHECK.  LT PACK ISOLATION VALVE AND RT OUTFLOWVALVE FAILED.  SEE REPORT IXKA940025.   REFERENCE CONTROL NR IXKA9400019. (W)


REMARKS:
FLT 67 DEPARTED EWR AT 19:55.  EN ROUTE TO MCO.  THE CREW WAS UNABLE TO CONTROL CABIN PRESSURE AUTO OR MANUAL MODE.  AIRCRAFT RETURNED TO EWR.  MAINTENANCE FOUND LT PACK ISOLATION VALVE WITH A SHEARED SHAFT.  REPLACED VALVE.  REPLACED RT OUTFLOW VALVE DURING PRESSURE DECAY CHECK.  (W)


REMARKS:
EN ROUTE MSY-ATL, FLIGHT 158, COFFEE MAKER IN FORWARD GALLEY SPARKED AND SMOKED.  FLIGHT ATTENDANT DISCHARGED PORTABLE HELON EXTINGUISHER.  REMOVED DEFECTIVE COFFEE MAKER ASSEMBLY AND REPLACED WITH SERVICEABLE UNIT.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CRACK AT BS 1104, STRINGER 13R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK,  FOUND FUSELAGE SKIN CREASED AT BS 380, WL 206, AT STRINGER 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK,  FOUND APU ACCESS DOOR DENTED BETWEEN NUMBER 1 AND 3 RIBS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
IN FLIGHT, EXPERIENCEDA SYSTEM HYDRAULIC FAILURE.  AIRCRAFT RETURNED TO SJC AND MADE AN UNEVENTFUL LANDING.  REPLACED HYDRAULIC LINE TO ELEVATOR PCU, CHECKED CASE DRAIN FILTERS AND SERVICED SYSTEM PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND L ANGLE ON WEB CRACKED AT BS 380-400, BL 0, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND RIGHT WING UPPER STRINGER 13R CRACKED IN RADIUS AT WS 157 AT RIB ATTACH POINT. REPAIRED PER BOEING DRAWING 65C344533 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD AND GALLEY ENTRY DOOR CUTOUTS CRACKED.  REPAIRED PER SWA ACO 3198-52.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT WING L/E ILLUMINATION LIGHT SUPPORT STRINGERS CRACKED.  REPAIRED PER BOEING SB 737-53-1145.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 15, 22, 29, AND 36, WL 208.  REPAIRED PER SWA RA 1-353-427.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 312, LBL 30.  REPAIRED PER SWA RA 1-353-421.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND SUPPORT ANGLE JUST AFT AND TOP OF NOSE GEAR ACTUATOR CRACKED IN RADIUS.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND FLOOR BEAM STABILIZING STRAP CRACKED AT BS 312, LBL 11.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND FLOOR BEAM LOWER STABILIZING STRAPS CRACKED AT BS 312, RBL 31.5, FORWARD FLANGE ANDAT BS 344, LBL 12.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW FRAME CRACKED AT UPPER OUTBOARD CORNER.  REPAIRED PER SWA RA1-353-1138.


REMARKS:
ON CLIMB-OUT, NUMBER 1 LEADING EDGE SLAT WOULD NOT RETRACT.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 1 LEADING EDGE SLAT ACTUATOR PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND WEB STRAP CRACKED AT BS 303, LBL 50, WL 244.5.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP.  REPLACED RIGHT EMERGENCY EXIT LIGHT BATTERY PACK PER BOEING MM.


REMARKS:
MID CABIN OVERHEAD EMERGENCY LIGHT WOULD NOT EXTINGUISH.  REMOVED POWER SUPPLY.  RESET LIGHT ELECTRICAL CANNON PLUG.


REMARKS:
ALB - EMERGENCY LIGHTING FOR CABIN INOPERATIVE.  MAINTENANCE FERRIED FLIGHT TO PHL.  FOUND LOOSE GROUND WIRE ON AFT ENTRY DOOR EMERGENCY LIGHT.  TIGHTENED WIRE.  OPS CHECKS NORMAL.  (Z)


REMARKS:
AIRCRAFT 1269L - FLT 178 - EN ROUTE TO IAD, EXPERIENCED UNCONTROLLABLE PRESSURIZATION IN AUTO AND MANUAL MODE.  AIRCRAFT RETURNED SAFELY TO ATL WITHOUT INCIDENT.  MAINTENANCE REMOVED AND REPLACED OUTFLOW VALVE ACT.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 663, STRINGER 3L OUTER CHORD CRACKED FORE AND AFT OF FORWARD RIVET.  REPAIRED PER TRAMCO EWO 94-0580.


REMARKS:
JFK - FLT 842 - RETURNED FROM FLIGHT ACCOUNT DURING CLIMB, NR 4 ENGINE OIL LOSS.  SHUT DOWN ENGINE.  FINDINGS INDICATE AN INTERNAL OIL LEAKAGE.  REPLACED ENGINE SN 4285.  ENGINE TOTAL TIME 62,438, TOTAL CYCLES 13,033.  CHECK C-8A, 1-22-94,JFK.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FUSELAGE INNER BELLY SKIN CORRODED BENEATH SEVERAL NUTPLATES AFT OF BS 700 BETWEEN STR 28L AND STR 28R.  CORROSION OUT OF LIMITS.  FABRICATED REPAIR DOUBLER, TREATED AND PRIMED PER SRM 51-10-2,SRM 53-30-2, AND SRM 51-10-2.  INSTALLED DOUBLER PER SRM 53-30-2 AND STRM 51-30-3.


REMARKS:
DURING C-CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 950F AND BS 970 AT STR 28L.  REMOVED DAMAGED INTERCOSTAL.  FABRICATED NEW, TREATED AND INSTALLED PER SRM 51-40-3, SRM 51-30-8, SRM 51-30-2, AND SRM 51-10-2.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND BULGE IN OUTER SKIN AT BS 660 BETWEEN STR 28L AND STR 28R, CORROSION OUT OF LIMITS.  REMOVED DAMAGED SKIN, FABRICATED REPAIR FILLER, EXTERNAL DOUBLER AND INSTALLED PER SRM 53-30-3, STRM 51-30-8, SRM 51-10-2, AND SRM 51-20-4.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SKIN BULGE AT BS 690, STR 28L - STRINGER CORROSION OUT OF LIMITS.  CUT OUT DAMAGED SECTION AND FABRICATED NEW STRINGER SECTION AND INSTALLED STRINGER SPLICE PER SRM 53-10-3, SRM 51-10-2, AND SRM 51-30-2.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND STR 27L EXFOLIATED AT BS 610 - REMOVED DAMAGED SECTION, FABRICATED STRINGER SPLICE AND FILLERS AND INSTALLED PER SRM 53-10-3, SRM 51-10-2, AND SRM 51-20-4.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND STA 178 BULKHEAD EXT. APPROX. WL 200, BBL 5.7 HAS TWO STIFFENERS WITH CORROSION AND ONE CORNER BROKEN OFF.  FOUND CRACK IN WEB RUNNING ALONG SIDE RIGHT VERTICLE STIFFENER AT BL 5.7.  REPAIRED BY FABRICATING AND INSTALLING REPLACEMENT STIFFENERS, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER PER BOEING SB 727-56-0213, BOEING REPAIR PLAN NR M-7272-94-4125, REPAIR DWG NR 65-636289, AND APPLICABLE SRM REF.


REMARKS:
DURING C-CHECK AND C.P.C.P., FOUND INTERCOSTAL TO SKIN ANGLE CRACKED AND CORRODED JUST FORWARD OF BS 950B A STR 30 - FOUND OUT OF LIMITS.  REPALCED WITH FABRICATED INTERCOSTAL PER SRM 51-30-2, SRM 51-40-3, SRM 51-10-2, SRM 51-30-2 AND SRM 51-20-4.


REMARKS:
DURING C-CHECK, FOUND LONGERON 29L CORRODED AFT OF BS 990.  AFTER FASTENER REMOVAL, REMOVED CORROSION (SURFACE), FOUND WITHIN LIMITS, TREATED AND PRIMED PER SRM 51-10-6, SRM 51-10-2.  REINSTALLED FASTENERS PER SRM 51-30-2.


REMARKS:
DURING C-CHECK FOUND FRAME 1164 CORRODED JUST RIGHT OF STR 30 - CORROSION WITHIN LIMITS.  REMOVED CORROSION, TREATED AND PRIMED IAW SRM 51-10-6 AND SRM 51-10-2.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND STRINGER SPLICE AT BS 685, STR 27L CORRODED.  REMOVED SPLICE, CLEANED UP CORROSION.  FOUND WITHIN LIMITS.  TREATED, PRIMED AND REINSTALLED STRINGER SPLICE.  REF. SRM 51-10-6, SRM 53-10-1, SRM 51-10-2, SRM 51-30-2.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND STR 28L AND SKIN CORRODED BETWEEN 950F AND BS 970, FOUND OUT OF LIMITS.  FABRICATED NEW STRINGER SECTIONS AND TREATED PER SRM 53-10-3, SRM 51-30-2, AND SRM 51-10-2.  CUT OUT DAMAGED SKIN, FABRICATED DOUBLER AND FILLER AND TREATED PER SRM 51-30-2, SRM 51-30-8, SRM 51-30-3, AND SRM 51-10-2.  INSTALLED AND SEALED PER SRM 51-30-2 AND SRM 51-20-4.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND CORROSION ON SHIM UNDER SHEAR TIE AT STA 1148, STR 26L, CORRODED OUT OF LIMITS.  FABRICATED NEW SHIMS, TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2, SRM 51-30-2, AND SRM 51-20-4.


REMARKS:
DURING C-CHECK, FOUND CORROSION ON ALL ANTENNA MOUNTING POINTS.  REMOVED SURFACE CORROSION, TREATED AND PRIMED AFFECTEDAREAS PER SRM 51-10-6, SRM 51-10-2.


REMARKS:
DURING OP-15, FOUND RIVET BROKEN TOP OF RIGHT PYLON AND .5 INCH CRACK IN ATTACH ANGLE, STATION 1019.  REPAIRED PER SRM 54-04, FIGURE 10-3.


REMARKS:
STL - DURING OP-15, FOUND .25 INCH CRACK AT RIGHT PYLON ATTACH ANGLE, STATION 996.  REPAIRED BY STOP DRILLING CRACK ANDINSTALLING EXTERNAL DOUBLER PER SRM 54-04, FIGURE 10.


REMARKS:
STL - DURING OP-15, FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER ATTACH ANGLE LEFT SIDE, STATION 1132.  INSTALLED DOUBLER REPAIR PER SRM, FIGURES 23 AND 23A.


REMARKS:
STL - DURING OP-15, FOUND A 1.5 INCH CRACK AT AFT END OF FORWARD PASSENGER DOOR, NR 8 BEAM.  REPLACED BEAM PER DRAWING 9955757.


REMARKS:
STL - DURING OP-9, FOUND .75 INCH CRACK IN LONGERON 25L, STATION 160.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
BOS - INVESTIGATION OF ENG S/N 4188 SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION, STALL, EGT RISE AND SPOOL DOWN, REVEALED A FAILURE OF THE NR 2 BEARING P/N 785732.  REPLACED BEARING, REPAIRED/REPLACED AFFECTED COMPONENTS.  ENGINE W/N 4188 RETURNED TO SERVICE.


REMARKS:
STL - DURING OP-15 FOUND A ONE-INCH CRACK IN VERTICAL STABILIZER ATTACH ANGLE RIGHT SIDE, STA 1132.  INSTALLED DOUBLER REPAIR PER SRM 53-05, FIGURES 23-23A.


REMARKS:
STL - DURING OP-15 FOUND .3750 INCH CRACK IN LONGERON 1, BELT RING FS 756.  REPAIRED PER SRM 53-02, FIGURE 4.


REMARKS:
STL - DURING OP-15 FOUND .3750 INCH CRACK IN LONGERON 7L, STA 756.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
PIT - DURING Q-3 INSPECTION DISCOVERED 1 INCH CRACK LT PYLON TO FUSELAGE DOUBLER AT STA 1019.  INSTALLED DOUBLER REPAIRPER SRM 54-04 FIG. 10.  (W)


REMARKS:
PIT - DURING Q-3 INSPECTION DISCOVERED 2 CRACKS .5000 INCH LONG EACH LONGERON 4L THROUGH INBOARD AND OUTBOARD FASTENER ATTACHMENT AREA AT STA 160.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG. 5.  (W)


REMARKS:
PIT - DURING Q-3 INSPECTION DISCOVERED 1 INCH CRACK IN LONGERON 3R THROUGH INBD FASTENER AT STA 639.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG. 2.  (W)


REMARKS:
CMH - FLT 2107 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO CMH WHERE LANDING WAS WITHOUT FURTHERINCIDENT.  MAINTENANCE FOUND FORWARD SERVICE DOOR FALSE LOCKED.  RECLOSED DOOR.  PRESSURIZED AIRCRAFT.  NO PROBLEMS FOUND.  (W)


REMARKS:
PIT - FLT 847 - THE INTERIOR REAR EMERGENCY EXIT LIGHTS ARE INOPERATIVE.  MAINTENANCE REPLACED BATTERIES IN THE OVERWING EMERGENCY POWER PACK.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
BWI - EMERGENCY EXIT LIGHT AFT ENTRY DOOR INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK AND CHARGER.  (W)


REMARKS:
DCA - FLT 1697 - AFTER TAKEOFF FROM DCA, AFT CARGO DOOR LIGHT CAME ON.  FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED AFT CARGO DOOR WARNING SWITCH.  (W)


REMARKS:
SDF - FLT 2406 -  FLIGHT EN ROUTE CLT TO IND WHEN CAPTAIN'S WINDSHIELD CRACKED.  FLIGHT DIVERTED TO SDF WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CAPTAIN'S WINDSHIELD.  (W)


REMARKS:
CLT - FLT 227 - FLIGHT EN ROUTE LGA TO RSW WHEN CAPTAIN'S NR 1 WINDSHIELD CRACKED.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CAPTAIN'S WINDSHIELD.  (W)


REMARKS:
BOS - FLT 1937 - AT 2,000 FEET, THE AFT SMOKE ALARM SOUNDED.  THERE WAS A FOUL SMELL AND HAZE IN THE CABIN.  AT 3,000 FEET, THE CREW DEPRESSURIZED THE AIRCRAFT AND RETURNED TO BOS.  AN EMERGENCY WAS NOT DECLARED.  MAINTENANCE REPLACED BOTHWATER BAGS.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 1146 - THE SLAT DISAGREEMENT LIGHT WENT OUT THEN CAME BACK ON DURING CLIMB.  IT CONTINUED TO FLICKER ON AND OFF DURING FLIGHT.  MAINTENANCE REPLACED THE RIGHT SLAT UP SWITCH.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
DTW - FLT 1206 - THE LEFT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED ON CLIMB OUT.  THE CREW REDUCED POWER TO IDLE AND THE LIGHT REMAINED ON.  MAINTENANCE REPLACED THE OIL SWITCH.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
DCA - FLT 1462 - THE FIRST THIRTEEN CABIN EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED A BROKEN WIRE.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
PIT - RT EMERGENCY EXIT LIGHTS INOPERATIVE.  MAINTENANCE REPLACED BATTERY CHARGER.  OPS CHECK OK.  (W)


REMARKS:
PHL - FLT 1099 - UNABLE TO CONTROL PRESSURIZATION AFTER TAKEOFF.  FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND FORWARD ENTRY DOOR FALSE LOCKED.  FORWARD ENTRY DOOR ROLLERS WORN.  REPLACED ROLLERS.  (W)


REMARKS:
PIT - FLT 859 - E/MLEFT GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT WHILE GEAR HANDLE WAS UP.  THE AIRCRAFT RETURNED TO FIELD.  MAINTENANCE REPLACED THE LEFT GEAR DOOR POSITION SWITCH.  AIRCRAFT OK FOR SERVICE.  (W)


REMARKS:
CHS - FLT 809 - RETURN TO FIELD DUE TO A LOUD FLAPPING NOISE FROM THE MAIN CABIN DOOR AREA AFTER TAKEOFF.  MAINTENANCE REPOSITIONED THE SEAL.  (W)


REMARKS:
JFK - DURING C-CHECK, FOUND CRACK ON OUTBOARD SIDE OF BULKHEAD, STATION 1363.  REPAIRED BY STOP DRILLING PER SRM 53-11-00, FIGURE 850.  TOTAL CYCLES 22,401.


REMARKS:
JFK - DURING C-CHECK, FOUND BULKHEAD 1363 OUTBOARD FORMER ANGLE CRACKED THROUGH, BULKHEAD AFT SIDE, ABOVE STRINGER 21.INSTALLED DOUBLER REPAIR PER SRM 51-50-02.  TOTAL CYCLES 22,401.


REMARKS:
JFK - DURING C-CHECK, FOUND TOP OF LEFT ELEVATOR DENTED WITH 1.5 INCH CRACK EIGHT AND ONE HALF FEET OUTBOARD OF INBOARDEND; HAS AIRWORTHY REPAIR TO REPLACE AREA ZONE 300.  REPAIRED BY INSTALLING DOUBLER AND FILLER PERMANENT REPAIR, PER SRM 55-20-03, PAGE 202.  TOTAL CYCLES 22,401.


REMARKS:
JFK - DURING C-CHECK, FOUND 2.25 INCH CRACK ON UPPER SURFACE OF NR 2 TE FLAP VANE INBOARD END.  INSTALLED DOUBLER REPAIR PER SRM 57-50-08, PAGE 201.  TOTAL CYCLES 22,401.


REMARKS:
MCI - DURING C-CHECK, FOUND LEFT WING REAR SPAR CHORD CRACKED AT HOLES IN BAY 8, AT FASTENERS 10A AND 13A.  REPLACED INBOARD AND OUTBOARD REAR SPAR WEB AND UPPR SPAR CHORD PER EMLR 65096, REV A.  TOTAL CYCLES 19,545.


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION ON GALLEY DOOR FRAME AT GALLEY FLOOR LEVEL, STATION 829.  REMOVED CORROSION PER MM 51-21-02 AND STANDARD PRACTICE AND REPAIRED PER ARA 8234.  TOTAL CYCLES 19,545.


REMARKS:
ALB - ROW 1 TO 6 EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE FOUND BROKEN WIRE AT ROW 6 BEHIND WINDOW PANEL.  REPAIRED WIRING.  (Z)


REMARKS:
SLT - DURING OP-15 FOUND A ONE INCH CRACK IN RT UPPER PYLON ATTACH ANGLE, FORWARD OF AFT SPAR, STA 1023.  REPAIRED PER SRM 54-04, PAGE 24.  (W)


REMARKS:
STL - DURING OP-15 FOUND A .5 INCH CRACK ON OUTBOARD END OF RT CANTED KEEL RIB, STA 662.  REPAIRED PER SRM 53-03, FIGURE 12.  (W)


REMARKS:
STL - DURING CHECK C FOUND A ONE INCH CRACK IN VERTICAL FIN FRONT SPAR LEFT CAP, STA 1074.  REPAIRED PER SRM 55-02,  FIGURE 26.  (W)


REMARKS:
STL - DURING CHECK C FOUND 1.375 INCH CRACK IN LT WING AFT SPAR LOWER CAP AT INBOARD FLAP HINGE LOWER INBOARD ATTACH BOLT.  REPAIRED PER DOUGLAS DWG J060271-503.  (W)


REMARKS:
PIT - DURING Q-3 INSPECTION, DISCOVERED .25 INCH CRACK LONGERON 17R, STA 965.  SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17.  (X)


REMARKS:
DURING Q-3 INSPECTION, DISCOVERED 2 EACH .50 INCH SKIN CRACKS AT LONGERON 17R, STA 1070.  INSTALLED SKIN DOUBLER REPAIRPER SRM 53-01.  (X)


REMARKS:
PIT - DURING Q-3 INSPECTION, DISCOVERED LEVEL 1 CORROSION AT STA 996 FLOOR SUPPORT, RT LAV.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-10-14.  (X)


REMARKS:
PIT - DURING Q-3 INSPECTION, DISCOVERED .75 INCH CRACK LOWER RT PYLON ATTACH ANGLE AT FORWARD END.  INSTALLED DOUBLER REPAIR PER SRM 54-04, FIGURE 10.  (X)


REMARKS:
CMH - FLT 403 - FLIGHT EN ROUTE PIT TO LAX WHEN, AT FL 310,B SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO AND LOW PRESSURE LIGHT ILLUMINATED.  FLIGHT DIVERTED TO CMH WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR2 ENGINE DRIVEN HYDRAULIC PUMP.  (W)


REMARKS:
STL - DURING CRUISE, LEFT ENGINE FIRE WARNING INDICATION APPEARED ONB LOOP.A LOOP PREVIOUSLY PLACARDED ON MEL.  REPLACED UPPER BARRIER LOOP, MFG. P/N 593823-506.  OP CHECKS ON BOTH LOOPS NORMAL.  CHECK C- 1D - 1-13-94 - MCI.  (W)


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING L/E DAMAGE FROM BIRDSTRIKE.  REPAIRED RIB AT STA 139 PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE LOWER LOBE SKIN CRACK AT BS 373.  REPAIRED PER SWA ACO 3182-53.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM  VERTICAL WEB CRACKED AT BS 344, LBL 28, WL 207.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND FLOORBEAM STABILIZING STRAP CRACKED AT AFT SIDE, BS 312, BL 0.  REPLACED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND Z ANGLE CORRODED AT FORWARD ENTRY DOOR DRAIN.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND COCKPIT WINDOW POST SKIN CRACKED APPROXIMATELY .6875 INCH LONG BEGINNING AT TOP LEFT CORNER OF CAPTAIN'S NUMBER 1 WINDOW EXTENDING OUTWARD AT AN UPWARD ANGLE.  REPAIRED PER SWA RA 1-A53-1156.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND COCKPIT WINDOW POST OUTER SKIN CRACKED.  REPAIRED PER SWA RA 1-A53-1156.


REMARKS:
AFTER TAKEOFF, NOTED PRESSURE LEAK AT CAPTAIN'S NUMBER 1 WINDOW.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REMOVED WINDOW ASSEMBLY, SEALED FRAME AND REINSTALLED WINDOW PER BOEING M/M.


REMARKS:
EXPERIENCED BIRDSTRIKE TO NUMBER 2 ENGINE.  AIRCRAFT RETURNED TO SAT AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRDSTRIKE INSPECTION, NO DEFECTS NOTED.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 882 BELOW S22R, WL 167.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORDS CORRODED AT BS 328, LBL 50, LBL 29, RBL 11, WL 208 ANDAT BS 344, LBL 36, 29, 22, AND 15, WL 208.  REPAIRED PER SWA ACO 1-353-427.


REMARKS:
DURING SCHEDULED CHECK, FOUND LEFT WING L/E FIXED PANEL CRACKED UNDER NUMBER 2 SLAT AT OUTBOARD AUX TRACK.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, RBL 60, WL 193 AT S19R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM SUPPORTS CORRODED AT BS 967 TO 987, RBL 17 AND AT BS 987 TO 1004, LBL 14, WL208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE MOUNTED WING L/E LIGHT ILLUMINATION SUPPORT STRINGERS CRACKED AT BS 527, S16R AND 16L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD SERVICE DOORWAY UPPER FRAME CRACKS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LOWER ANGLED SECTION OF RIB AT L/E STA 208 GOUGED ON RIGHT WING.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 1138, RBL 24, WL 285.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FIXED EDGE OF LEFT WING UPPER SURFACE CRACKED I/B OF AUX TRACK CUTOUT FOR NUMBER 1 SLAT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 16L BELLFRAME CRACKED AT BS 312, BELOW LOWER FORWARD DOOR STOP APPROX 3.75 INCHES LONG.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND T CHORD AFT SIDE OF BULKHEAD CRACKED AT BS 178, RBL 6, APPROX 8 INCHES FROM BOTTOM. REPAIRED PER SWA RA 1-253-1165.


REMARKS:
FLT 192 - PDX - RETURNED FROM FLIGHT ACCOUNT LEFT ENGINE FIRE WARNING CAME ON.  WHEN THROTTLE WAS RETARDED FIREWARNING INDICATION CEASED.  FOUND NOSE COWL ANTI-ICE DUCT RUPTURED.  REPLACED DUCT, MFG. P/N 13277-505 AND REPAIRED SECONDARY DAMAGED WIRING.  OP CHECKS NORMAL.  CHECK C-1D - 1-13-94 - MCI.


REMARKS:
AFTER TAKEOFF, LEFT MAIN GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  ADJUSTED RIGHT GEAR UPLOCK PROXIMITY SWITCH PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND OUTBOARD LEFT WING AUX TRACK CUTOUT CRACKED LOWER SIDE OF L/E SKIN APPROX 8 INCHES FROM NUMBER 2 SLAT.  REPAIRED PER SWA RA 1-252-244.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST SKIN CRACKED AT UPPER OUTBOARD CORNER.  REPAIRED PER SWA RA 1-353-1138.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND UPPER CORNER OF AFT CARGO DOOR HANDLE CUTOUT CRACKED.  REPAIRED PER SWA RA 1-A52-020.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, LEFT SIDE AT S16R WEB AND ANGLE.  REPAIRED PER SWA RA 1-253-1169.


REMARKS:
DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, AT S26R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT BS 344 FRAME BETWEEN STRINGERS 22 AND 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND CREASE BEAM CRACKED IN WEB OF STUD FRAME AT BS 579, RBL 64, WL 201.  REPAIRED PER BOEING DRAWING 65C2511.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND AFT CABIN EMERGENCY FLOOR TRACK LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SC CHECK, FOUND AFT RIGHT CABIN EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SC CHECK, FOUND AFT RIGHT CABIN EMERGENCY EXIT LIGHT AT AFT SERVICE DOOR INOP.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 472 TO 484, ABOVE S17L.  REPAIRED SKIN PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND CRACK AT WING TO BODY DRAG ANGLE RIGHT SIDE, BS 540, S22R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AND SCRATCHED UNDER FORWARD ENTRY DOOR AT BS 300-312.  REPAIRED SKIN PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 910 BETWEEN STRINGERS 24 AND 25R.  REPAIRED SKIN PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND HAT CHANNEL CORRODED AT BS 993, LBL 12 TO 45, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND WEB CORRODED AT BS 380-400, BL 0.  REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND LAVATORY PAN SHEAR WEB ASSEMBLY CORRODED AT BS 1016-1025, LBL 10-25, WL 208.  REPLACED WEB ASSEMBLY PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CRACKED AT BS 178 TO 188, RIGHT SIDE, WL 195, RBL 25.  REPLACED INTERCOSTALPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND L ANGLE CRACKED AT BS 178, WL 196, LBL 24.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM SUPPORT CORRODED AT BS 1006 - 1016, LBL 4.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, RBL 8 AND LBL 9.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORRODED AT BS 947, LBL 14 TO RBL 54, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND L/E SKIN TORN AT CUTOUT FOR OUTBOARD MAIN TRACK FOR NUMBER 4 SLAT.  REPAIRED PER SWA RA 1-257-243.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT CARGO FLOOR BEAM SUPPORT CORRODED FROM BS 771-773, LBL 2.5, WL 156.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORROSION AT BS 1016, LBL 26 TO RBL 35, WL 208 AND AT BS 987, LBL 16 TO RBL 30, WL 208.  REPAIRED UPPER T CHORDS PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM SUPPORT CORRODED FROM BS 986 TO 1006.  REPLACED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR STRUCTURE Z ANGLE  CORRODED AT BS 270 FROM LBL 10 TO RBL 11.  REPLACED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DENTED AT BS 887, RBL 29, WL 170, S24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND NUMBERS 1 AND 3 L/E SLAT SKIN CRACKED ON LOWER SIDE.  REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL AND BOEING DRAWING 65C30133.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 957-970 AT S19-21L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663.75 AT S10L AND R AND AT BS 500D, LBL 58, WL 178, S21L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF FLIGHT NR 29 RETURNED TO EWR DUE TO NR 7 LOADING EDGE SLAT FAILED TO RETRACT.  AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND NR 7 SLAT UPPER RT ROLLER BEARING MISSING.  ATTACHED HARDWARE STILL INTACT IN SLAT TRACK GUIDE.  FOUND OLD BEARING, INSTALLED NEW BEARING.  OPS CHECKED OK.  (Z)


REMARKS:
BOS - FLT 233 - THE GEAR WAS EXTENDED ON FINAL.  THE NOSE GEAR INDICATED RED.  A FLY-BY WAS CONDUCTED AND THE TOWER ADVISED THAT THE NOSE GEAR WAS DOWN AND APPEARED LOCKED.  THE GEAR WAS THEN RECYCLED, BUT THE INDICATION WAS STILL RED.  WHILE THE CREW REVIEWED THE CHECKLIST, THE GREEN LIGHT FOR THE NOSE GEAR ILLUMINATED.  MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH AND CONDUIT.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
CLT - FLT 1435 - AFT SECTION OF FLOOR PATH LIGHTING IN CABIN INOPERATIVE.  ALL EMERGENCY EXIT LIGHTING IN TAIL INOPERATIVE.  MAINTENANCE REPLACED FUSE IN THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CHS - FLT 1178 - THE AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERIES.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 52 - AIRCRAFT DIVERTED TO PIT DUE TO LT GEAR UNSAFE LIGHT ILLUMINATING IN FLIGHT.  MAINTENANCE REPLACED THE DOWNLOCK SWITCH.  OPERATION CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 8960 - UPON RETRACTING THE LANDING GEAR, THE CAPTAIN HEARD AN UNUSAL NOISE.  HE THEN EXTENDED THE LANDING GEAR AND GOT THREE GREEN LIGHTS.  THE AIRCRAFT THEN RETURNED TO CLT.  MAINTENANCE FOUND THE RT NOSE GEAR DOOR EXTENDED.  THEY OPENED BOTH RT AND LT NOSE GEAR DOORS AND INSPECTED.  NO DISCREPANCIES NOTED.  (W)


REMARKS:
PIT - FLT 1704 - A SECTION OF THE FLOOR PATH LIGHTING WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE SOCKET ANDLIGHT ASSEMBLY, REPAIRED THE PATH LIGHTING.  (W)


REMARKS:
SWF - FLT 1522 - AIRCRAFT RETURNED TO FIELD DUE TO STALL WARNING ACTIVATION AT LIFT OFF.  MAINTENANCE FOUND THE LT FLAPTRANSMITTER CONNECTOR CORRODED.  THEY CLEANED THE CONNECTOR AND ELECTRICALLY CHECKED THE FLAP TRANSMITTER SWITCHES.  (W)


REMARKS:
CLT - THE FLOOR LEVEL EMERGENCY LIGHTS IN FIRST CLASS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE SPLICED THE WIRE IN FIRST CLASS FLOOR EMERGENCY LIGHTING.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
MEM - FLT 1541 - THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF.  THE CREW RECYCLED THE GEAR BUT IT STILL DID NOT RETRACT.  THE AIRCRAFT RETURNED TO THE FIELD.  MAINTENANCE FOUND THE RT NOSE GEAR SPRAY DEFLECTOR BOLTS MISSING, AND THE SPRAYDEFLECTOR LOOSE.  THEY INSTALLED BOLTS AND INSPECTED THE DEFLECTOR.  THE AIRCRAFT WAS OK FOR SERVICE.  (W)


REMARKS:
PIT - FLT 1698 - AFTER TAKEOFF, THE NOSE GEAR UNSAFE LIGHT REMAINED ON.  THERE WAS ALSO LOUD WIND NOISE.  THE CREW DECIDED TO RETURN TO PIT.  MAINTENANCE REPLACED THE NOSE GEAR SERVICE VALVE AND SERVICED WITH AIR AND OIL.  ALL INDICATIONS WERE NORMAL.  (W)


REMARKS:
ORD - FLT 1100 - AFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT.  THE CREW DECIDED TO RETURN TO PIT.  MAINTENANCE PERFORMED A NOSE GEAR SWING PER THE DOUGLAS MAINTENANCE MANUAL.  GEAR SWING CHECKED GOOD.  (W)


REMARKS:
ALT - FLT 311 - THE FORWARD HALF OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY.  ALL TRACK LIGHTING CHECKED NORMAL.  (W)


REMARKS:
PIT - FLT 550 - THE FORWARD LOW LEVEL EMERGENCY LIGHT SECTION IS INOPERATIVE.  MAINTENANCE REPAIRED THE LOW LEVEL LIGHTING SECTION.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
SYR - FLT 2299 - RETURN TO FIELD DUE TO RT GENERATOR FLUCTUATING AND DROPPING OFF LINE.  MAINTENANCE REPLACED THE CONSTANT SPEED DRIVE.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 972 - WHEN THE LANDING GEAR WAS EXTENDED DOWN, THE NOSE GEAR WOULD NOT EXTEND.  THE CREW DID A FLY-BY AND THETOWER CONFIRMED THAT THE GEAR WAS NOT DOWN.  THE CREW THEN USED THE EMERGENCY GEAR HANDLE EXTENSION AND THE NOSE GEAR EXTENDED.  ANOTHER FLY-BY WAS PERFORMED AND THE TOWER CONFIRMED THAT THE NOSE GEAR WAS DOWN.  THE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NOSE LANDING GEAR LOCK CYLINDER.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
FLT 648 - STL - DURING APPROACH WHEN LANDING GEAR WAS LOWERED, THE NOSE GEAR UNSAFE WARNING LIGHT REMAINED ON.  FOUND ELECTRICAL WIRING TO DOWNLOCK PROXIMITY SENSOR WIRING BROKEN AT CONDUIT RECEPTACLE.  REPLACED WIRING.  OP CHEKS NORMAL. CHECK C 5-13-94 - PHX


REMARKS:
PHL - FLT 953 - EMERGENCY EXIT LIGHTNOT ARMED ANNUNCIATOR CAME ON DURING TAXI, WHEN SWITCH WAS IN ARMED POSITION.  MAINTENANCE REPLACED OVERHEAD EMERGENCY LIGHT SWITCH IN COCKPIT.  (W)


REMARKS:
BOS - FLT 1989 - DURING CLIMB-OUT, NR 2 IRS DC FAIL ILLUMINATED.  TWO MINUTES LATER NR 1 DC FAIL LIGHT ILLUMINATED.  THE BATTERY VOLTAGE WAS 17 VOLTS.  FLIGHT RETURNED TO BOS WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED SHIP'SBATTERY CHARGER.  REF 94ZZZW2810.


REMARKS:
ON CLIMB-OUT, NUMBER 1 SLAT WOULD NOT RETRACT.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 1 SLAT ACTUATOR PER BOEING M/M.


REMARKS:
DEN - FLT 9016 - RETURNED FROM FLIGHT ACCOUNT, RT ENGINE STALLED, AND LOST POWER SHORTLY AFTER TAKEOFF.  SHUT DOWN ENGINE.  FOUND METAL IN TAILPIPE.  REPLACED ENGINE SN 3230.  CHECK C - 2D - 1-13-94 - MCI.


REMARKS:
PIT - FLT 466 - DURING FLIGHT FROM BDL TO PIT, THE RT OIL STRAINER CLOGGING LIGHT ILLUMINATED.  THE CAPTAIN ELECTED TO SHUTDOWN THE ENGINE.  THE FLIGHT LANDED AT PIT WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE RT ENGINE.  THE AIRCRAFT WAS THEN RETURNED TO SERVICE.  (W)


REMARKS:
AFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT.  AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED LANDING GEAR HYDRAULIC MODULE AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
PIT - DURING Q-1 INSPECTION AND ACCOMPLISHING CORROSION TASK C58-53300, FOUND LEVEL 2 CORROSION AT STA 980-996 THRESHOLD FLOOR BEAM.  MFG REPAIR ANGLE AND STRAP REPAIR PER USAIR TYPICAL REPAIR 53-10-19.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION AND ACCOMPLISHING CORROSION TASK C57-53300, FOUND LEVEL 2 CORROSION AT STA 756 LONGERON 30 END FITTING.  REPLACED LONGERON AND FITTING PER SRM 53-02 FIG 12 SHEET 3 AND 4.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION AND ACCOMPLISHING CORROSION TASK C58-53300, FOUND LEVEL 2 CORROSION AT STA 996 FLOOR BEAM ANGLE.  MFG NEWL ANGLE PER SRM 53-11-3 FIG 6B-1 AND SRM 51-10-1 SHT 5.  (W)


REMARKS:
PIT - Q-1 INSPECTION, FOUND .50 INCH CRACK AT STA 622 OUTBOARD END OF LEFT KEEL FRAME.  INSTALLED REPAIR ANGLE PER SRM 53-03 FIG 12.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTON, FOUND .75 CRACK AT STA 637 OUTBOARD END OF LT KEEL FRAME.  INSTALLED REPAIR ANGLES PER SRM 53-03 FIG 12.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION, 2 CRACKS FOUND TOTALING 10 INCHES FOUND AT STA 965 LEFT SIDE SUB FLOOR WEB AT LONG 18L (CUSP).  MFG WEB PANEL AND SLICED IN AREA PER SRM 53-05 FIG 97.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND 2 INCH CRACK ON STA 617 LONGERON 18R (CUSP) SUBFLOOR WEB.  SPLICED IN NEW SECTION OFWEB PER SRM 53-05 FIG 96/97.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND 1 INCH CRACK IN ATTACH AT STA 945 BETWEEN LONGERONS 15L AND 16L.  INSTALLED ANGLE AND REPAIR SPLICES PER SRM 54-04 FIG 10.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND DAMAGED SKIN (DENTS/GOUGES) BETWEEN STA 843 AND 879 AND LONGERON 26L AND 28L IN SKIN.  INSTALLED FLUSH SKIN REPAIR WITH FINGER DOUBLER PER SRM CH 51 AND USAIR EA 27258.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND ONE .50 INCH CRACK ATSTA 1038 RIGHT FRAME WEB.  INSTALLED DOUBLER AND REPLACED WEB SECTION PER USAIR EA27327.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND .50 INCH CRACK IN AFT CARGO DOOR OPENING-PAN BOTTOM AFT LIP (DOOR JAMB).  WELDED CRACK AND INSTALLED NEW PAN PER SRM 53-05 FIG 44 AND USAIR EA27404.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND .75 INCH CRACK IN FORMER AT STA 622 OUTBRD END OF RIGHT KEEL FRAME.  INSTALLED REPAIR ANGLES PER SRM 53-03- FIG 12.  (W)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND .8750 INCH CRACK IN FORMER AT STA 637 OUTBRD OF RT KEEL FRAME.  INSTALLED REPAIR ANGLES PER SRM 53-03 FIG 12.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND A .75 INCH CRACK IN THE WEB AT STA 1038 BETWEEN LONGERON 12L AND 13L.  INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2 SHEET 3.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND ONE .25 INCH CRACK AT LOWER PYLON ATTACH ANGLE STA 945 LONGERON 15L.  INSTALLED DOUBLER REPAIR SRM 54-04 FIG 10.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, INSPECTION FOUND STA 1074 FRAME CRACKED 1 INCH AT LONGERON 6L.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 30. (W)


REMARKS:
DURING SCHEDULED D CHECK, REPLACED LEFT AND RIGHT FUSELAGE SKINS AT BS 727 THROUGH 907, STRINGERS 20 TO 25 DUE TO BEINGAGED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0696.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND VERTICAL SUPPORT CRACKED AT UPPER FASTENER HOLE AT LEFT KEEL BEAM, BS 727.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND CHORD CRACKED AT BS 178,  WL 195.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0727.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LEFT AND RIGHT WING L/E ILLUMINATION LIGHT SUPPORT STRINGERS  CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND WEB DAMAGED AT BS 1135, WL 260, LBL 21 AND AT BS 1127, WL 260, LBL 21.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD SERVICE DOORWAY  UPPER FRAME CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD ENTRY DOOR SILL CORRODED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 438 TO 448, BETWEEN S22 AND 23L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SPOILERS 6, 7 AND 9 UPPER SURFACES HAVE AREAS OF DISBONDMENT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0740.


REMARKS:
DURING SCHEDULED D CHECK, FOUND NUMBER 4 GROUND SPOILER GRAVEL DAMAGED AND PUNCTURED 4 PLACES.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT FASTENER HOLES, BS 616, LBL 50, WL 201.  REPAIRED PER TRAMCO EWO 94-0728.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR DENTED ABOVE HANDLE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED 1 FOOT BELOW APU INLET DOOR.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 967 TO 987, RBL 17, WL 208 AND AT BS 971 TO 983, LBL 17, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT STRAP CORRODED AT BS 1006 TO 1025, LBL 3.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKATE ANGLE CRACKED AT BS 560, WL 165.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD GALLEY DOOR CUTOUT CRACKED AT BS 327-329, WL 210.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT S4R AND S4L AT BS 400 AND AT BS 500D, RBL 60, WL 193, AT STRINGER 19R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER S25L CORRODED AT BS 860.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AREA OF DISBONDMENT RIGHT WING L/E, OUTBOARD OF NUMBER 5 SLAT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AREA OF DISBONDMENT AT NUMBER 2 SLAT, OUTBOARD AREA.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND 2 FUSELAGE SKIN DENTS AT BS 290-300, BETWEEN S18 AND 19L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, AT S3R AND S2R.  REPAIRED PER TRAMCO EWO 94-0718.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME STIFFENER CORRODED AT BS 328-344, LBL 12, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM WEB CRACKED AT BS 709, LBL 24, WL 204.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND RIGHT CREASE BEAM CRACK AT BS 639, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME PUNCTURED AT BS 767, AT S24R, WL 165.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DENTED AT BS  420, WL 167 ABOVE S23L AND AT BS 827, LBL 29, WL 163.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE PRESSURE BULKHEAD CRACKED AT BS 727, LBL 17, WL 162.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0713.


REMARKS:
MCI - DURING C-CHECK, FOUND A ONE INCH CRACK ON INBOARD SIDE AFT FLANGE OF VERTICAL STIFFENER U-CHANNEL, STATION 983, LBL 30.  STOP DRILLED CRACK AND REPAIRED PER SRM 57-11-00.  TOTAL CYCLES 20,640.


REMARKS:
JFK - RETURNED FROM FLIGHT ACCOUNT SHORTLY INTO CRUISE, THE AFT LOWER CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH BOTTLES.  FOUND NO ABNORMALITY IN THE COMPARTMENT.  REPLACED ALL FOUR SMOKE DETECTORS, MFG P/N 30-231R34B, AND AMPLIFIER MFG P/N 30-303A3.  OP CHECKS NORMAL.  CHECK C-7B, 2-22-94, JFK.


REMARKS:
STL - DURING C-CHECK, FOUND .1875 INCH CRACK ON TOP EDGE OF LONGERON 2R, STATION 642.  REPAIRED PER SRM 53-02.  TOTAL CYCLES 80,313.


REMARKS:
TPA - FLT 1874 - RETURN TO FIELD DUE TO THE L2 DOOR BARRIER STRAP BEING LEFT CAUGHT IN THE DOOR.  MAINTENANCE OPENED THE LEFT AFT SERVICE DOOR, FOUND THE STRAP AND PUT THE STRAP IN ITS PROPER POSITION.  NO DAMAGE WAS FOUND.  AIRCRAFT WAS OK FOR SERVICE.  (Z)


REMARKS:
ORD - FLT NR 1083 - AFTER TAKEOFF THE CREW NOTICED A HOT SMOKEY SMELL IN THE COCKPIT AND BOTH LAV SMOKE DETECTORS ALARMING.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LEFT AND RT WATER SEPARATOR BAGS.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLT NR 1062 - DURING FLIGHT THE AIRCRAFT HAD A SLOW LOSS OF CAIBN PRESSURE AT 35,000 FEET.  CREW ATTEMPTED TO MANUALLY CONTROL CABIN PRESSURE WITH NO SUCCESS. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE CABIN AIR PRESSURE SELECTOR.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - EMERGENCY LIGHTS TRIP EVAC AUTO CONTROL BREAKER.  RESET, TRIPPED AGAIN.  EMERGENCY LIGHTS ILLUMINATED.  MAINTENANCE TIGHTENED SCREWS ON TERMINAL ENDS ON EVAC AUTO CONTROL BREAKER.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
CLT -FLT NR 124 - PRIOR TO DEPARTURE THE EMERGENCY EXIT FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS.  MAINTENANCE REPLACED FLOOR PROXIMITY INVERTER.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
CLT - THE EMERGENCY EXIT DIM CIRCUIT BREAKER WILL NOT STAY RESET.  MAINTENANCE REPLACED THE BATTERY AT THE LEFT OVERWING AND RIGHT REAR SERVICE DOOR.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
IN FLIGHT, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED.  CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN.  AIRCRAFT LANDED AT MSY WITHOUT INCIDENT.  REPLACED NUMBER 1 ENGINE START VALVE PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD CABIN EXITS LIGHTS INOP.  REPLACED TWO EMERGENCY BATTERY PACKS PER BOEINGM/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD CABIN CENTER OVERHEAD EXIT AND BOTH OVERWING LIGHTS INOP.  REPLACED  CENTER LEFT AND RIGHT BATTERY PACKS PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD CABIN  OVERHEAD EXIT LIGHTS INOP.  REPLACED BATTERY POWER SUPPLY AND BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 312, RBL 10, WL 208 AND AT BS 987, LBL 20 TO LBL 55.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU DUCT MOUNT STIFFENER ON BULKHEAD CORRODED.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR SUPPORT BEAM CORROSION AT BS 727 TO 947, LBL 10, 5, AND 16.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CRACKED AT BS 1121, S12R.  REPLACED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU INLET LOWER CHORD CORRODED FROM BS 1101 TO 1138, RBL 36, WL 230.  REPLACEDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND VERTICAL CHORD CORRODED AT BS 1127, RBL 36, WL 240.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU DOOR FRAME EDGE DENTED AND CRACKED FROM RIGHT EDGE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CHORD CORROSION AT BS 1016, WL 208, LBL 20.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
PIT - DURING OVERNIGHT, MAINTENANCE ACCOMPLISHED USAIR CD 53F00762, FOUND STRINGERS NR 7 AND NR 68 CRACKED IN HALF AND A .25 INCH SKIN CRACK AT STRINGER NR 7 LOCATION AT STA 3870.  MANUFACTURED AND INSTALLED NEW SECTION OF STRINGER EA POSITION AND INSTALLED DOUBLER REPAIR FOR SKIN CRACK PER SRM 51-70-02, PG 23, FIG F AND USAIR EA 27391.  REF USAA940716.


REMARKS:
CVG - FLT 239 - PRIOR TO DEPARTURE THE EMERGENCY EXIT LIGHTS ILLUMINATE IN THE OFF AND ON POSITIONS.  MAINTENANCE REPAIRED A LOOSE WIRE AT PIN 3 ON THE EMERGENCY LIGHT SWITCH.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
CLT - FLT 699 - DURING FLIGHT THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE COULD NOT DUPLICATE PROBLEM.  RAN ENGINES TO CRUISE POWER AND CHECKED OPERATION OF PNEUMATIC SYSTEM.  ALL FOUND TO BE WITHIN NORMAL PARAMETERS.  (W)


REMARKS:
CLT - FLT 546 - ON APPROACH THE CREW GOT APU FIRE INDICATION.  DISCHARGED FIRE BOTTLE.  AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT.  MAINTENANCE REPLACED FIRE DECTECTOR CONTROL UNIT.  OPERATION AND BITE CHECK GOOD.  NO EVIDENCE OF FIRE.  REPLACED BOTTLE AND SQUIB.  (W)


REMARKS:
MCO - FLT 1844 - AFTER TAKEOFF THE AIRCRAFT WOULD NOT PRESSURIZE.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND TORN SEAL ON E AND E DOOR.  REPLACED SAME.  GROUND PRESSURIZES NORMAL.  (W)


REMARKS:
PIT - DURING OVERNIGHT, MAINTENANCE ACCOMPLISHED USAIR CD 53F00762, FOUND STRINGERS NR 7 AND NR 68 CRACKED IN HALF AND A .25 INCH SKIN CRACK AT STRINGER NR 7 LOCATION AT STA 3870.  MANUFACTURED AND INSTALLED NEW SECTION OF STRINGER EA POSITION AND INSTALLED DOUBLER REPAIR FOR SKIN CRACK PER SRM 51-70-02, PG 23, FIG F AND USAIR EA 27391.  REF 94ZZZW3001.


REMARKS:
CLT - FLT 1993 - DURING FLT THE SYSTEM NR 2 HYDRAULIC QUANTITY GAUGE LEVEL BEGAN TO SLOWLY DROP INTO THE YELLOW ARC, TORED LINE MINIMUM.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  (W)


REMARKS:
PIT - FLT 978 - STALL WARNING COMPUTER FAILED AFTER LIFT OFF.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.MAINTENANCE REPLACED THE STALL WARNING COMPUTER.  TEST PRECAUTIONS PER MM 27-35-02-400-8114A COMPLETED.  (W)


REMARKS:
GSO - DURING PCI 901 AND 902 CHECK VISUAL INSPECTION, FOUND .281 INCH CRACK FORWARD CARGO DOOR HINGE MOST FORWARD LUG UPPER HINGE HALF.  THIS WAS FOUND WHILE ACCOMPLISHING INSPECTION OF LOWER HINGE HALF WHICH IS NOT THIS JOB CARD.  DEFERRED OM-7 NR 0333796 EA 27029.  (W)


REMARKS:
DURING STRUCTURAL INSPECTION VISIT, DISCOVERED 2 EACH .1250 INCH AND .5 INCH CRACKS IN THE NOSE LANDING GEAR TOP COVER AT STA 2650 SKIN.  INSPECTION PER FOKKER F28 SIP 53-10-10.  STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 13.  (W)


REMARKS:
PIT - DURING STRUCTURAL INSPECTION VISIT, DISCOVERED A .5 INCH CRACK AT AFT UPPER CORNER OF THE FORWARD SERVICE EMERGENCY DOOR FUSELAGE SKIN.  INSPECTION PER FOKKER SIP 53-10-20.  ROUTED OUT CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-02-16.  (W)


REMARKS:
EWR - FLT 2471 - FLIGHT EN ROUTE ORF TO LGA WHEN NR 1 ENGINE OIL TEMPERATURE PEGGED HIGH.  CREW PULLED THROTTLE TO IDLEAND DIVERTED TO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED OIL TEMPERATURE SENSOR AND OIL COOLER.  (W)


REMARKS:
GSO - FLT 2358 - A FLAP ASYMMETRY LOCKOUT OCCURRED AFTER DEPARTURE FROM CLT.  FLIGHT DIVERTED TO GSO WHERE A NO FLAPS LANDING WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT FLAP POSITION TRANSMITTER.  (W)


REMARKS:
PHL - CABIN EMERGENCY EXIT LIGHTS INOPERATIVE.  MAINTENANCE REPLACED BATTERY CHARGER FOR OVERHEAD WING EMERGENCY DOOR LIGHTS.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREAS (4) PLACES STA 312 RBL 12 INCHES, 21 INCHES, 40 INCHES, AND 49 INCHES.   REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - Q-2 CHECK VISUAL INSPECTION, FOUND (2) 1 INCH BY 2 INCHES CORRODED AREAS FLOOR BEAM BS 328, 25 INCHES RBL AND 31 INCHES RBL.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA BS 253 LBL 2 INCHES FORWARD OF NOSE GEARVIEWER.  REPAIRED PER TR 53-10-16.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH AND 1 INCH BY 3 INCH CORRODED AREA O/B SEAT TRACK BS 1008 AND BS 990.  REPAIRED PER SRM 51-30-5.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION (2) PLACES, .75 INCH BY 2 INCHES AND .25 INCH BY 1 INCH BS 986.5 FLOOR BEAM RBL 30 AND 40.  REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES BS 1006 FLOOR BEAM UPPER CAP LBL 12.  REPAIRED PER TR 53-10-05 C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION (2) PLACES 1 INCH BY 1 INCH BS 986.5 TO BS 1006 LBL 12 LBL 2 APPROX.  REPAIRED PER SRM 51-10-06.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES BS 1014, LBL 48.  REPAIRED PER SRM 51-10-06.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 6 INCHES BS 1016 UPPER CAP OF FLOOR BEAM.  REPAIRED PER SRM 53-10-9.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX .5 INCH SQUARE AREA CHAFED.  CEILING WEB IN MAIN WHEEL WELL APPROX STA 665, RBL 20.  REPAIRED PER EA 37616.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION FOUND .75 INCH CRACK, BS 616 RBL 63 WL 201.5 I/B CHORD OF FRAME.  REPAIRED PEREA 37597.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK I/B CHORD BS 616 FRAME LBL 63 WL 201.5.  REPAIRED PER EA37597.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIA BULGE IN SKIN BS 727 AND 18 INCHES AT RT KEEL BEAM.  REPAIRED PER EA 37609.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM WEB CRACKED .5 INCH BS 520 RBL 25 INCHES.  REPAIRED PER EA 37600.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM WEB CRACKED 1 INCH BS LBL 25 INCHES.  REPAIRED PER EA 5335-20 AND SB 737-53-1120.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM WEB CRACKED .5 INCH BS 520 RBL 45 INCHES.  REPAIRED PER EA 37600.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND UPPER CHORD CRACKED 1 INCH IN RADIUS BS 520 LBL 25 INCHES WL 207.75.  REPAIRED PER EA 37600 SB 737-53-1120, REV 1.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AILERON SECTOR WHEEL WELL CUTOUT DOUBLER BS 677 LBL 25 INCHES WL 206.  REPAIRED PER EO 579G632 AND EA 37629.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AILERON SECTOR WHEEL CUTOUT DOUBLER BS 677 RBL 25 INCHES WL 206.  REPAIRED PER EO 579G632.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORRODED AREA STA 284 TO 294 RBL 43 INCHES.  REPAIREDPER SRM 53-10-5.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORRODED AREA STA 328 TO 344 RBL 43 INCHES.  REPLACED PER SRM 53-10-5.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORRODED AREAS (2) PLACES STA 333 TO STA 338 AND STA 355 TO STA 360 RBL 23 INCHES.  REPAIRED PER SRM 53-10-5.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION FOUND .5 INCH BY 2 INCH AND .25 BY 1 INCH CORRODED BS 990 LEFT SIDE.  REPAIREDPER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION, APPROX. 2 INCH BY 8 INCH AREA, BETWEEN STA 976TO 986, STR 26 R.  REPAIRED PER SRM 53-10-3 FIG 1.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 6 INCH AREA CORRODED STRINGER 27 L AT STA 1006 TO 1016.  REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORRODED AREA (3) PLACES S-26 R STA 457, 480, 489.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 47 INCH CORRODED AREA STA 294.5 RBL 0 INCH TO RBL 47 INCHES.REPAIRED PER TR 53-10-04B.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION FOUND 1 INCH BY 24 INCH CORRODED AREA STA 380 S-277 TO 26 R.  REPAIRED PER SRM51-10-1, SRM 51-40-3.  CORROSION TASK NR. C53-2088-01.  CORROSION LEVEL 2.  (W)


REMARKS:
GSO - DURING 'TRANSIT CHECK' VISUAL INSPECTION FOUND .0937 INCH CRACK AFT END OF FORWARD AIRSTAIR EXTERIOR CONTROL HANDLE CUT OUT.  REPAIRED PER 53-30-03, SB 7737-53-4093R3.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH AREA AT SCREW HOLE CORRODED, BS 1006 TO BS 1016, FUSELAGE WALL TO FLOOR WEB.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN AFT LOWER HINGE CUTOUT IN FUSELAGE SKIN FOR FORWARD GALLEY DOOR.  REPAIRED PER SRM 53-30-3.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION AREA BETWEEN BS 804 AND 847 BETWEEN S-25 R AND 23 L.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 CRACKS IN FORWARD PRESSURE BULKHEAD SKIN, .5 INCH AT RBL 5 WL 198, 1 INCH AT RBL 5 WL 201 BS 178.  REPAIRED PER EA 37746.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK IN SERVICE DOOR, BS 294.5 WL 207.5 RBL 55.  REPAIRED PERSRM 51-70-11.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN FORWARD PRESSURE BULKHEAD SKIN AT LBL 5, WL 198, BS 178LBL 5 WL 198.  REPAIRED PER EA 37746.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 4 INCH CORRODED AREA, 100 PERCENT LOSS IN PLACES ON FLOOR SUPPORT BEAM AFT CARGO STA 946 TO 940 LBL 17.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 4 INCH CORRODED AREA, 100 PERCENT LOSS IN PLACES ON FLOOR SUPPORT BEAM AFT CARGO, STA 940 TO 946 RBL 14.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AROUND NUT PLATE HOLE FLOOR SUPPORT BEAMAFT CARGO STA 863 RBL 13.5.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 6 INCH CORRODED AREA AROUND NUT PLATE HOLES AT STA 867 FLOOR SUPPORT BEAM RBL 14.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORRODED AREA 100 PERCENT LOSS IN PLACES STA 783 TO 827 RBL 14 FLOOR BEAM AFT CARGO.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA 30 PERCENT LOSS FLOOR SUPPORT ANGLE BS STA 859 LBL 2.5 AFT CARGO.  REPAIRED PER EA 37783.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH AREA CORRODED FLOOR BOARD SPLICE STRIP STA 859 RBL 18 TO LBL 21.5.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 8 INCH BY 1.5 INCH AREA OF CORROSION BS 344 AND 7 INCHES S 25 L.  REPAIRED PER SRM 53-00--3 FIG 201.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 EACH 1 INCH DIA SPOTS OF CORROSION, S 21 L BS 887 AND 4, AND BS 887 AND 13.  REPAIRED PER EA 37748.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH SPOT OF CORROSION AT SCREW HOLE BS 302 LBL 12.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
PIT - DURING STRUCTUAL INSPECTION VISIT, DISCOVERED A 1.5 INCH CRACK IN THE AFT PRESSURE BULKHEAD AT STA 17065 BELOW FLOOR BEAM NR 3, AND BETWEEN BL 425L AND BL1050L.  INSPECTION PER FOKKER F28 SIP 53-10-03.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR EA 27270.  (W)


REMARKS:
MCI - DURING 'AS' CHECK, FOUND FUSELAGE FRAME ATTACH FITTING LUG BROKEN AT HORIZONTAL BEAM, FS 1243 CASTING, IN RIGHT WHEELWELL.  REPAIRED PER SRM 51-10-01, PAGE 2.  AIRCRAFT TOTAL TIME:  64,224 HOURS; 18,138 CYCLES.


REMARKS:
JFK - FLT 842 - RETURNED FROM FLIGHT ACCOUNT SHORTLY INTO CRUISE, AFT LOWER CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED.  DISCHARGED BOTH BOTTLES.  FOUND NO ABNORMALITY IN THE COMPARTMENT.  REPLACED ALL FOUR SMOKE DETECTORS, MFG P/N 30-231R34B, AND AMPLIFIER MFG. P/N 30-303A3.  OP CHECKS NORMAL.  CHECK B-7B - 2-22-94 - JFK.


REMARKS:
PIT - RON MAINTENANCE NOTICED A 3.5 INCH SKIN CRACK AND SUBSEQUENTLY A 1.5 INCH CRACK IN STRINGER NR 69 AT STATION 4200LEFT NOSE AREA AFT OF AIRCO EXHAUST PORT.  ROUTED OUT SKIN CRACK AND REPAIRED SKIN AND STRINGER PER SRM 51-70-02 FIG 9EAND EA 27213.  REFERENCE USAA940659.


REMARKS:
PIT - FLT NR 1627 - ON TAKEOFF THE MLG DOORS HAD RED AND AMBER ILLUMINATIONS.  THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND THE RETRACT CYLINDER BOLT BROKEN.  REPLACED UPPER AND LOWER LINK FOR SUB ASSY.  OPERATION CHECKS NORMAL PER WORK CARD JEF 32-10-01.  (Z)


REMARKS:
DURING SCHEDULED DOWN TIME FOR APU MODIFICATION, STRINGER NR 69 WAS FOUND TO HAVE .5 INCH CRACK BETWEEN STATION 4240 AND 4360.  ACCOMPLISHED A STRINGER SPLICE REPAIR PER SRM 51-70-02, FIG 9E AND USAIR EA 27214.  (Z)


REMARKS:
PIT - RON MAINTENANCE NOTICED A 3.5 INCH SKIN CRACK AND SUBSEQUENTLY A 1.5 IINCH CRACK IN STRINGER NR 69 AT STATION 4200 LEFT NOSE AREA AFT OF AIRCO EXHAUST PORT.  ROUTED OUT SKIN CRACK AND REPAIRED SKIN AND STRINGER PER SRM 51-70-02 FIG 9E AND EA 27213.  REFERENCE 94ZZZZ1815.


REMARKS:
GSO - DURING PCI 1587 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AFT SIDE OF FRM 1890 JUST BELOW NR 2 WINDOW COCKPIT.REPAIRED PER 0M-7 NR 10496, EA 27199.  (Z)


REMARKS:
CLT - FLT NR 1655 - PRIOR TO DEPARTURE THE EMERGENCY EXIT SIGN ABOVE THE COCKPIT DOOR WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE FWD EMERGENCY ASSEMBLY PER F28 MM.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
CLT - FLT NR 1072 - DURING PREFLIGHT THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED BATTERY POWER PACK.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
RDU - FLT 17 - DURING PREFLIGHT ALL OF THE EMERGENCY EXIT LIGHTS WERE ILLUMINATED WITH THE OVERHEAD COCKPIT SWITCH IN THE ARMED POSITION.  MAINTENANCE FOUND BAD SWITCH.  REPLACED SWITCH PANEL.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
GSO - DURINGTRANSIT CHECK VISUAL VERIFIED BY EDDY CURRENT INSPECTION FOUND .1875 INCH CRACK BOTH FORWARD LUGS ON CENTER CARGO DOOR HINGE.  REPAIRED PER MODIFIED PART NR INSTALLED 1552500. (Z)


REMARKS:
GSO - DURINGTRANSIT CHECK VISUAL VERIFIED BY EDDY CURRENT INSPECTION FOUND .1875 INCH CRACK FORWARD CARGO DOOR HINGELUGS (FORWARD LUG AND SECOND FROM AFT LUG).  REPAIRED PER MODIFIED PART NR INSTALLED 1552500.  (Z)


REMARKS:
PIT - FLIGHT NR 0089 - EXPERIENCED A LOSS OF HYDRAULIC FLUID FROM 'A SYSTEM.  THE AIRCRAFT RETURNED TO FIELD AT PIT AND LANDED WITH ASYMMETRICAL FLAP CONFIGURATION.  MAINTENANCE REPLACED THE FLAP DRIVE HYDRAULIC MOTOR.  LEAK AND OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
TPA - FLT 0221 - ON APPROACH TO TPA, THE NOSE GEAR SHOWED RED AFTER THE GEAR WAS EXTENDED.  THE GEAR WAS RECYCLED.  ALLINDICATIONS NORMAL.  MAINTENANCE LUBRICATED THE NOSE GEAR ASSEMBLY.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
CLT - DURING A SHOP TEST, TWO OF THE 727 LIFE RAFTS (PN R0202A203) WERE FOUND TO BE BELOW ACCEPTABLE INFLATION PRESSURE.  THESE FAILURES WERE DUE TO THE CYLINDERS (PN R0032-12).  (Z)


REMARKS:
CLT - DURING A SHOP TEST, THE 727 LIFE RAFT (PN R0202A203) WAS FOUND TO BE BELOW ACCEPTABLE INFLATION PRESSURE.  MAINTENANCE REPLACED THE BOTTLE LOWER TUBE.  (Z)


REMARKS:
GSO - DURINGTRANSIT CHECK EDDY CURRENT INSPECTION FOUND .1875 INCH CRACK TYPE 3, RIGHT NR 2 WINDOW POST.  REPAIRED PER TYPICAL REPAIR 53-10-01 REV A.  (Z)


REMARKS:
MCI - DURING CHECK C, FOUND A ONE-INCH CRACK ON INBOARD SIDE AFT FLANGE OF VERTICAL STIFFENER U-CHANNEL, STA 983, LBL 30.  STOP DRILLED CRACK AND REPAIRED PER SRM 57-11-00.  AIRCRAFT TOTAL TIME:  56,661 HOURS; 20,640 CYCLES.


REMARKS:
STL - FLT 228 - RETURNED FROM FLIGHT ACCOUNT RIGHT MAIN LANDING GEAR WOULD NOT RETRACT.  REPLACED BUNGEE ACTUATOR, MFG PN 391406-5505.  OP CHECKS NORMAL.  CHECK C-6 4-18-94.  STL.


REMARKS:
DURING CHECK C, FOUND .1875 INCH CRACK ON TOP EDGE OF LONGERON 2R, STA 642.  REPAIRED PER SRM 53-02.  AIRCRAFT TOTAL TIME:  60,461 HOURS; 80,313 CYCLES.


REMARKS:
STL - FLT 393 - ON DESCENT WHEN LANDING GEAR WAS LOWERED, NOSE GEAR DID NOT EXTEND.  AFTER RECYCLING OF THE LANDING GEAR, NORMAL INDICATION WAS FOUND.  REPLACED NOSE GEAR TRANSFER VALVE, MFG PN 69-14106-5.  OP CHECKS NORMAL.  CHECK C-2 - 10-15-93 - MCI.


REMARKS:
BDL - FLT 207 - RETURNED FROM FLIGHT ACCOUNT RT ENGINE FIRE WARNING.  WHEN THROTTLE WAS RETARDED, WARNING INDICATION CEASED.  FOUND NOSE COWL ANTI-ICE DUCT, MFG PN 7958591-501, RUPTURED.  REPLACED DUCT.  OP CHECKS NORMAL.  CHECK C-9 - 11-14-93 - STL.


REMARKS:
DURING TAXI, CABIN OVERWING EMERGENCY EXIT LIGHTS FLICKER.  REPLACED LIGHT BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN  EMERGENCY EXIT LIGHTS INOP.  REPLACED AFT CABIN LIGHT BATTERY PACK PERBOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY  EMERGENCY EXIT LIGHTS INOP.  REPLACED LIGHT BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, RBL 39, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 782, WL 186 BETWEEN STRINGERS 19 AND 20R.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN CREASED FROM BS 920 TO 947, STRINGER 23-24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT SERVICE DOOR FRAME INNER EXTRUSION CORRODED, BS 990, RBL 60, WL 158.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FORWARD SERVICE DOOR FRAME CRACKED AT BS 291.5, RBL 60, WL 208 TO 230.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 16R CRACKED AT BS 500C, WL 212.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, LBL 28, STRINGER 24L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 1006, RBL 13, WL 208.  REPAIRED PER TRAMCO EWO 94-0792 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR SUPPORT BEAMS CORRODED AT BS 727 TO 947, RBL 5, 10, AND BL 0, WL 160.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 294, LBL 5 TO 20.  REPAIRED PER SWA RA 1-353-418.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORROSION AT BS 294, BL 0 AND LBL 10, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, BL 0, LBL 10, WL 208.  REPAIRED PER SWA RA 1-353-427R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1016, RBL 41 TO LBL 41, WL 208.  REPAIRED PER SWA RA 1-353-542.


REMARKS:
DURING SCHEDULED 1/2 CHECK, FOUND FORWARD ENTRY DOORWAY  AFT FRAME SUPPORT ANGLE CRACKED, AFT OF NUMBER 9 STOP FITTING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SC CHECK, FOUND RIGHT WING L/E SKIN TORN AT NUMBER 4 SLAT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND SWA RA 1-257-240.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND AFT CARGO FLOOR BEAM CRACKED AT BS 747, RBL 14.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY EMERGENCY LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND LEFT WING FIXED L/E LOWER SKIN PANEL CRACKED .75 INCH AT STA.5.0.  REPAIRED PER SWA RA1-357-225.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND NUMBER 1 SLAT INBOARD AUX TRACK CUTOUT CRACKED .5 INCH AT UPPER T/E.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DYNAIR W/O 7500-10-Y183.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 902, BETWEEN S17 AND 18L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON S-26 R 10 INCHES BS 1006 - BS 1016 S-26 R.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA BS 1016 LBL 6.  REPAIRED PER SRM 53-10-9.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH DENT IN SKIN.  BS 957 SKIN AT S-19 L.  REPAIRED PER SRM 53-30-3 FIG 6.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH DENT AREA BS 927 BETWEEN S-18 L AND S-19 L.  REPAIRED PER SRM 53-30-3.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK OUTER SKIN BS 727 A PLUS 15 INCHES ABOVE S-17 R.  REPAIREDPER SRM 53-30-03.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 312 FORWARD SERVICE ENTRY LOWER HINGE CUTOUT.  REPAIREDPER EA 37626.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK SEVERAL PLACES.  CREASE BEAM WEB BS 616-639 WL 208 LEFT SIDE.  REPAIRED PER TR 53-10-02.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK BS 639 RIGHT SIDE AT WL 208.  REPAIRED PER TR 53-10-02.(Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK INBOARD CHORD OF BS 639 FRAME RBBL 64 INCHES WL 216.  REPAIRED PER SRM 51-10-1 AND 51-30-2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 559 FRAME LBBL 64 INCHES WL 210.  REPAIRED PER SRM 51-40-3.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA 30 PERCENT LOSS BS 270 BL 0 .  REPAIRED PER T/R 53-20-04.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 RBL 6 INCHES.  REPAIRED PER TR 53-10-11.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECITON, FOUND 1 INCH CRACK LBL 6 INCHES 178 BULKHEAD LBL 6 INCHES.  REPAIRED PER TR 53-10-11.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION BS 986 - BS 1016 LEFT SIDE INTERCOSTAL AT LAVATORY DOOR IN CABIN.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 5 FEET BY 2 INCH AREA CORRODED, STATION 787-847 AT RBL 14 IN AFTCARGO.  REPAIRED PER SRM 53-10-5.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH BY 26 INCH CORRODED AREA, BS 328 FROM LBL 27 INCHES THROUGH LBL 53 INCHES.  REPAIRED PER EA 37721.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 3 INCHES FORWARD SERVICE DOOR.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
MCO - FLT 1166 - FLIGHT EN ROUTE CLT TO NAS WHEN ENTIRE RADAR SCREEN PAINTED YELLOW AT ALL RANGES AND TILT SETTINGS.  FLIGHT DIVERTED TO MCO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED RADAR R/T UNIT.  OPS CHECKS NORMAL.  (Z)


REMARKS:
CLE - FORWARD EMERGENCY EXIT SIGNS INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK.  (Z)


REMARKS:
PIT - AFT LEFT OVERWING EMERGENCY LIGHT INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK.  (Z)


REMARKS:
LGA - FLT 2238 - ON CLIMB-OUT OF LGA, STRONGE SMELL OF O-ZONE IN A/C SYSTEM.  ALL 3 SMOKE DETECTORS ACTIVATED.  FLIGHT CONTINUED TO MCO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE RELEASED RIGHT ENGINE BLEED ON MEL 36-5.  SMELL COMING FROM RIGHT ENGINE BLEED ON EITHER PACK.  REPLACED RIGHT ENGINE.  REMOVED MEL.  (Z)


REMARKS:
CLT - FLT 2148 - ON TAKEOFF OUT OF LGA, UPON GEAR RETRACTION, LEFT GEAR RED LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION.  RECYCLED GEAR.  RED LIGHT REMAINED ON.  ALL THREE GREEN LIGHTS CAME ON.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT GEAR UPLOCK SWITCH.  (Z)


REMARKS:
DAY - FLT 2148 - CABIN FLOOR PATH EMERGENCY EXIT LIGHTS INOPERATIVE.  MAINTENANCE REPLACED BATTERIES AND CHARGERS.  FERRIED AIRCRAFT TO PHL. CYCLED EMERGENCY LIGHTS CIRCUIT BREAKERS AND RECHARGED ALL BATTERY PACKS.  EMERGENCY LIGHTS OPS TEST NORMAL.  (Z)


REMARKS:
PIT - DURING STRUCTURAL INSPECTION VISIT OF SIP 53-10-06, FOUND A 6 INCH CRACK LEFT SIDE AND A 8 INCH CRACK RT SIDE FWDPRESS BULKHEAD LOWER CONNECTION ANGLE BETWEEN STRINGER 3 AND 72 AT FRAME 1550 VISUAL/EDDY CURRENT.  STOP DRILLED CRACK ENDS AND INSTALLED DOUBLERS PER SRM 53-11-00 PG 2 AND USAIR EA 27609.  (Z)


REMARKS:
PIT - DURING SCHEDULED MOD TRACK VISIT, FOUND A .375 INCH CRACK BELOW SERVICE EMERGENCY DOOR AT STRINGER NR 69 STATION 4360 IN THE SKIN. VISUAL EDDY CURRENT.  ROUTED OUT CRACK AND INSTALLED PLUG AND EXTERNAL DOUGLER PER SRM 53-00-02 AND USAIR EA 27553.  (Z)


REMARKS:
SYR - FLT 237 - CLIMBING THROUGH FL210 ENROUTE ALB TO PIT, A LOUD BANG WAS HEARD FROM NR 1 ENGINE, ACCOMPANIED BY SEVERE VIBRATION.  NR 1 ENGINE OVERTEMP LIGHT ILLUMINATED WITH EGT INDICATING 920.  CREW SHUTDOWN NR 1 ENGINE AND DIVERTED TOSYR WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT ENGINE PER USAIR WORK CARD J371-00-01.  (Z)


REMARKS:
PHL - FLT 1259 - THE FORWARD FLOOR LEVEL TRACK EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THEFORWARD BATTERY PACK.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
PIT - THE FORWARD EMERGENCY LIGHTS WERE FOUND TO BE LOW.  MAINTENANCE REPLACED THE BATTERIES.  OPERATIONS CHECKED GOOD. (Z)


REMARKS:
CLT - FLT 0836 - AIRCRAFT DIVERTED TO CLT DUE TO SLAT DISAGREEMENT LIGHT ILLUMINATING.  MAINTENANCE INSTALLED A NEW SLAT TRACK DOOR AT NR 3 SLAT NR 7 TRACK ON RIGHT SIDE.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
MCI - DURING OP-16, FOUND KEELSON FORMER CRACKED AT LT SIDE OUTBOARD END, FS 715, LBL 31.  REPAIRED FORMER BY INSTALLING DOUBLER PER ARA 8511.  AIRCRAFT TOTAL TIME:  37,630 HOURS; 33,843 CYCLES.


REMARKS:
MCI - DURING OP-16, FOUND LOWER FUSELAGE RIGHT CANTED KEEL IN KEELSON FORMER CRACKED, BS 716, RBL 31.  REPAIRED FORMER BY INSTALLING DOUBLER PER ARA 8511.  AIRCRAFT TOTAL TIME:  37,630 HOURS; 33,843 CYCLES.


REMARKS:
IN FLIGHT, EXPERIENCED LOW FREQUENCY VIBRATION.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND RIGHT O/B GEAR DOOR ATTACH BOLTS LOOSE.  RETORQUED SAME AND PERFORMED GEAR RETRACTION TEST OK.  AIRCRAFT MAINTENANCE FERRIED TO HOU AND EXPERIENCED SAME VIBRATION.  INSPECTED AND FOUND PLAY IN LEFT ELEVATOR TRIM TAB.  REPLACED BEARINGS, BUSHINGS,  RIGGED, AND PERFORMED TEST FLIGHT PER BOEING M/M.


REMARKS:
IN FLIGHT, NUMBER 1 ENGINE HAD OIL PRESSURE/QUANTITY LOSS.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT LANDED AT BWI WITHOUT INCIDENT.  INSPECTED AND FOUND OIL LEAKING FROM OIL FILTER HOUSING.  REPLACED FILTER, CAP O-RING AND INSPECTED METAL CHIP DETECTORS.  SERVICED SYSTEM TO FULL AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
DURING SCHEDULED MAINTENANCE CHECK, FOUND NOSE GEAR WELL CEILING PRESSURE BULKHEAD CRACKED.  REPAIRED PER SWA RA 1-253-1164.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 967, RBL 30 TO 45, WL 208.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 25L GOUGED AT BS 506, LBL 31, WL 159.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM NUTPLATE HOLES CORRODED AT BS 312, LBL 7 TO RBL 8, WL 208.  REPAIRED PER SWA RA 1-353-421 R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM NUTPLATE HOLES CORRODED AT BS 244.5, RBL 38 TO 45, WL 208.  REPAIRED PER SWA RA 1-353-418 R2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND CHORDS ABOVE AND BELOW APU INLET PLENUM CORRODED AT BS 1112 AND 1129, RBL 12, WL 247 AND 231.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LEFT FORWARD EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTING AT AFT CABIN  AREA INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND RIGHT SECONDARY FAIRING STRUCTURE BELT FRAME SEVERED.  REPAIRED PER SWA RA 1-A53-489.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND WEB CRACKED AT BS 639, AT S16 AND 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED ALONG FLOOR LEVEL, BS 639.  REPLACED FRAME PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME SUPPORT STRAP CRACKED, BS 639, BETWEEN S16 AND 17L.  REPLACED STRAP PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER VHF ANTENNA.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME DENTED AT BS 727A, WL 160, RBL 34.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 993, RBL 47.5, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CHAFED AT BS 878-885, BETWEEN STRINGERS 1 AND 2.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR UPPER FORWARD FRAME CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 639, LBL, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT AFT SIDE OF FRAME AT S10R AND S10L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 230, WL 227, LEFT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED 4 PLACES FROM BS 366 TO 377, BETWEEN S4 AND 6L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AND SCRATCHED UNDER FORWARD ENTRY DOOR.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
ON CLIMB-OUT AT 5,000 FT, EXPERIENCED NUMBER 1 ENGINE COMPRESSOR STALL.  AIRCRAFT RETURNED TO LAX AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND ENGINE COMPRESSOR BLADE DAMAGE.  REPLACED ENGINE ASSEMBLY AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
DAB - FLT 2381 - BIRD STRIKE TO RIGHT ENIGNE ON TAKEOFF.  FLIGHT RETURNED TO DAB WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE ACCOMPLISHED BIRDSTRIKE INSPECTION.  FOUND STRIKE IN NR 2 FAN ONLY, WITH BLADES 5 THROUGH 12 SHINGLED.  NO DAMAGE OR CORE INGESTION FOUND.  DESHINGLED BLADES.  (Z)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1006, RBL 29 TO LBL 29, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 52 TO LBL 52, WL 208.  REPAIRED PER SWA RA 1-353-542.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN CHAFED AT BS 860 BETWEEN STRINGERS 1 AND 2L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT AT BS 500B+10, STRINGER 4L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT AT BS 390, 410, 490, 500+10, 500A, 500A+10, AND 500B+10, STRINGER 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS ON THE LOWER ROW OF HORIZONTAL FASTENERS OF THE SKIN LAP RUNNING FORE AND AFT, FROM BS 380 TO BS 440, BS 490, 500+10, 500A, 500A+10, 500B+10, 520, AND 530, STRINGER 10L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT AT BS 390, 400, 410, 430, 450, 470, 480, 490, 500, 500+10, 500A, 500A+10, AND 500B+10, STRINGER 10R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT AT BS 380, 390, 420, 440, 470, AND 480, STRINGER 14L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT, AT BS 370, AND 450, STRINGER 14R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016,  FOUND CRACKS ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT, AT BS 590 AND 630, STRINGER 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016,  FOUND CRACK ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT AT BS 777, STRINGER 4L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS ON LOWER ROW OF HORIZONTAL FASTENERS OF SKIN LAP RUNNING FORE AND AFT AT BS 727A+10, 727B+10, 747, 757, 777, 817, AND 827, STRINGER 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS AT BS 380, 390, 400, AND 410, BETWEEN STRINGERS 10R AND 11R, COMMON TO TEAR STRAPS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND A .35 INCH BY .07 INCH GOUGE ON THELOWER EDGE OF STRINGER 10L HAT SECTION, BS 445.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FOUND FORWARD ENTRY DOOR AND COCKPIT EMERGENCY EXIT LIGHTS INOP.  REPAIRED BROKEN WIRE BEHIND BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DIMPLED FROM PREVIOUS REPAIR AT BS 1055-1080, STRINGERS 13-15L.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND 1 STRAP AND 2 L ANGLES CRACKED AT BS 347, LBL 54, WL 216, S16L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED UNDER EXISTING REPAIR AT BS 300, S21R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORROSION AT BS 947, RBL 48 TO 53.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
MCI - DURING CHECK-C FOUND .50 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER SUPPORT ANGLE TO FUSELAGE AND .25 INCH CRACK IN REPAIR ANGLE ON TOP OF SUPPORT, NEAR SAME LOCATION.  INSTALLED REPAIR DOUBLER PER SRM 53-05, FIGURE 23A.  AIRCRAFT TOTAL TIME:  34,902 HOURS; 18,686 CYCLES.


REMARKS:
LAX - FLT 125 - RETURNED FROM FLIGHT ACCOUNT NR 3 ENGINE SPOOLED DOWN.  FOUND GEAR TEETH PIECES ON CHIP DETECTORS.  REPLACED ENGINE SN 4499.  ENGINE TOTAL TIME:  40,097 HOURS; 13,982 CYCLES.  CHECK C-5C - 8-12-94 - MCI.


REMARKS:
MCO - FLT 396 - MADE UNSCHEDULED LANDING ACCOUNT NR 2 ENGINE WAS SHUT DOWN DUE TO VIBRATION.  REPLACED ENGINE SN 4021.ENGINE TOTAL TIME:  47,672 HOURS; 32,271 CYCLES.  CHECK C-4 - 12-20-93 - MCI.


REMARKS:
STL - FLT 300 - DURING FLIGHT, SINGLE SERVE NR 5 FOOD CART IN LOWER GALLEY EMITTED SMOKE AT PLUG.  REPLACED CART, MFG. PN 88801-1.  OP CHECKS NORMAL.  CHECK C-3B - 8-14-94 - JFK.


REMARKS:
STL - DURING OP-15, FOUND TANK ACCESS 1305 CRACKED AT SKIN DOUBLER LIP, OUTBOARD AFT CORNER, TOP SIDE OF INBOARD WING AREA.  REPAIRED PER SRM 57-03, PAGE 49, FIGURE 23.  AIRCRAFT TOTAL TIME:  66,612 HOURS; 73,171 CYCLES.


REMARKS:
DURING FLIGHT, D-ZONE SINGLE SERVE FOOD CART EMITTED SMOKE FROM INTERIOR HEATING PADS.  REPLACED CART, MFG. PN 88801-1. OP CHECKS NORMAL.  CHECK C-8B - 3-21-94 - JFK.


REMARKS:
PHL - FLT 108 - DURING CRUISE, MADE EMERGENCY DESCENT DUE TO LOSS IN CABIN PRESSURE CONTROL.  OXYGEN MASKS DEPLOYED AUTOMATICALLY.  NO ANAMOLY WAS FOUND.  PRECAUTIONARY REPLACED AUTO AND MANUAL CONTROLLERS, AND OUTFLOW VALVES.  OP CHECKS NORMAL. CHECK C-1 - 12-26-93 - MCI.


REMARKS:
STL - FLT 425 - RETURNED FROM FLIGHT, AFTER TAKEOFF FIREWARNING OCCURRED ON RT ENGINE.  REDUCTION OF THROTTLE TO IDLE CAUSED WARNING TO CEASE.  FOUND 13TH STAGE ENGINE PNEUMATIC DUCT CRACKED.  REPLACED DUCT, MFG (P/N 5958765-503).  OPS CHECKS NORMAL.  CHECK C 4-18-94 - STL.


REMARKS:
FLT 840 - JFK - ON APPROACH WHEELWELL FIREWARNING WAS INDICATED, ALONG WITH NR 4 GENERATOR RELAYS TRIPPING.  NO ANOMALIES WERE FOUND, OTHER THAN DEFECTIVE GENERATOR.  REPLACED GENERATOR, MFG (P/N 28B26313A), OPS CHECKS NORMAL.  CHECK C-9B -  1-22-94 - JFK.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE FOLLOWING AREAS: BS 390, 410, 420, 490, AND 381 TO 388, AT STRINGER 4L COMMON TO TEAR STRAPS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 400, 410, 420, 430, 450, 470, 500, 500A+10, 500B, 500B+10 AND 500B+ 13, AT STRINGER 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 380, 410, 420, 440, 450, 460, 470, 480, 490, 500+10, 500A,500A+10, 500B, 500B+10, 520, 530, AT STRINGER 10L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 370, 380, 400, 410, 420, 430, 440, 450, 460, 470, 480, 490, 500, 500+10, 500A, 500A+10, 500B, 500B+10,  AND 520, AT STRINGER 10R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 380, 390, AND 400, AT STRINGER 14L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 380, 390, 410, AND 470, AT STRINGER 14R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 568.5, 568.5 TO 578, 578, 578 TO 587.5, 587.5, 587.5 TO 597, 606.46, 627.46, 675, 685, 695, 706, AND 715, AT STRINGER 4L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 559, 568.5, 568.5 TO 578, 587.5, 597, 597 TO 606, 606, AND626, AT STRINGER 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 877, 867, 857, 847, 837, 807, AND 727B+10, AT STRINGER 4L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 727B+10, 747, 797, AND 847, AT STRINGER 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND CRACKS IN THE LOWER ROW OF HORIZONTAL FASTENERS RUNNING FORE AND AFT, COMMON TO INNER SKIN AT BS 757, 837, AND 857, AT STRINGER 10R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING BOEING FATIGUE INSPECTION OF FUSELAGE SKIN LAPS FROM BS 259.5 TO 1016, FOUND STRINGER HAT SECTION CRACKED STARTING FROM LOWER EDGE OF STRINGER EXTENDING UPWARD INTO CENTER OF STRINGER HAT SECTION, BS 537.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM UPPER CHORD NUTPLATE HOLE CORROSION AT BS 312, BL 0.  REPAIRED PER SWA RA 1-353-421.


REMARKS:
DURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD STIFFENER CHANNEL CORRODED AT BS 1017, BL 0, WL 190.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED CHECK, FOUND FORWARD GALLEY DOOR FRAME CRACKED.  REPAIRED PER SWA RA 1-252-197.


REMARKS:
MCI - DURING OP-16, FOUND KEELSON FORMER CRACKED AT LEFT SIDE OUTBOARD END, FS 715, LBL 31.  REPAIRED FORMER BY INSTALLING DOUBLER PER ARA 8511.  AIRCRAFT TOTAL TIME:  37,630 HOURS; 33,843 CYCLES.


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA, BS 520.  REPAIRED PER SRM 51-10-1.  CORROSIONTASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREAS AFT CARGO BS 827-867, ABOVE S-26 R.  REPAIREDPER SRM 53-10-5 FIG 11 SHT 2.  CORROSION TASK NR C53-208-201.  CORROSION LEVEL 2.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, BS 620 LBBL 54 INCHES WL 208.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH GOUGE IN TEAR STRAP, JUST ABOVE S-25 R AT BS 777 INSIDE CARGO BIN.  REPAIRED PER  SRM 53-30-1.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, BS 178 BULKHEAD RBL 5 INCHES WL 202.  REPAIRED PER TR 53-10-11FIG 11.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 6 INCH CRACK, OUTER SKIN BS 378 AFT SIDE EQUIPMENT COOLING FAN EXH.  REPAIREDPER TR 53-30-04 PRINT NR 65C31930 S/B 737-53-1117.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, BS178 BULKHEAD LBBL 5 INCHES WL 202.  REPAIRED PER TR 53-10-11.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND S-4 L TIE CLIP CRACKED, BS 1104.  REPAIRED PER SRM 51-10-1.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK, BS 328 LOWER AFT CORNER SERVICE DOOR.  REPAIRED PER SRM 53-30-3FIG 26.  (W)


REMARKS:
MIA - FLT 1042 - EN ROUTE TO BWI, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED.  THE CREW DECIDED TO DIVERT TO MIA.  OHM OUT ALL OVERHEAT LOOPS, ALL CHECKED NORMAL PER MM.  PULLED DOWN AFT BAGGAGE BIN WALLS AND CLEANED CONNECTORS.  FOUND LOOP CHAFING ON BRACKET NEAR DUCT, FOUND TWO DUCTS LEAKING, FWD PART OF KEEL BEAM.  PERFORMED HIGH POWER RUN UP FOR 25 MINUTES, NO DEFECTS NOTED.  (W)


REMARKS:
DTW - FLT 1206 - UPON TAKEOFF FROM DTW, THE CAPTAIN NOTICED THE LEFT OIL FILTER LIGHT ON DUE TO CLOGGING.  HE CUT THE POWER BACK ON THE NR 1 ENGINE, BUT THE LIGHT CONTINUED.  THE CAPTAIN ELECTED TO RETURN TO DTW.  MAINTENANCE REPLACED THE OIL FILTER SWITCH.  RAN ENGINE 80 PERCENT, CHECKS GOOD.  (W)


REMARKS:
BOS - FLT 194 - FLIGHT DIVERTED TO BOS, WHEN THE CABIN BECAME FILLED WITH A SMOKEY SMELL.  MAINTENANCE ISOLATED THE PROBLEM TO BE ANA SUMP OIL LEAK IN THE LEFT ENGINE.  AFTER TROUBLESHOOTING, THE MOST PROBABLE CAUSE FOR THE LEAK WAS DETERMINED TO BE A CRACKED NR 3 STATIONARY AIR OIL SEAL.  MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE.  THE FINAL  DETERMINATION OF THE OIL LEAK IS PENDING ENGINE DISASSEMBLY.  (W)


REMARKS:
BDA - FLT 853 - AFTER TAKEOFF, THE RIGHT PACK TRIPPED, THEN SHORTLY AFTER A FIREWARNING ON THE NR 3 ENGINE.  THE CREW RETARDED THE THROTTLE LEVER TO IDLE AND FIREWARNING WENT OUT.  THE FLIGHT RETURNED TO BDA AFTER DUMPING FUEL.  MAINTENANCE REPLACED THE EIGHTH STAGE SUPPLY DUCT ASSEMBLY, NO LEAKS WERE FOUND.  (W)


REMARKS:
PIT - FLT 498 - ON CLIMB-OUT, BIRD STRIKE ON RIGHT ENGINE, RIGHT ENGINE VIBRATION EXCEEDED 5.0.  FLIGHT RETURNED TO PIT, WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE ACCOMPLISHED BIRD STRIKE/FOD INSPECTION PER MAINTENANCE MANUAL 71-00-47.  REPLACED DAMAGED BLADES NR 14, 15, AND OPPOSITE BLADES NR 33 AND  34.  (W)


REMARKS:
DCA - FLT 2480 - ON APPROACH DCA, UNABLE TO GET A GREEN LIGHT ON LEFT MAIN GEAR.  SWITHCHED BULBS, STILL NO GREEN LIGHT, CYCLED GEAR AND GOT GREEN LEFT MAIN LIGHT ON.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPAIRED LAMP HOLDER SOCKET, LEFT MAIN GEAR GREEN LIGHTS NORMAL.  (W)


REMARKS:
IND - FLT 2130 - FLIGHT EN ROUTE TO MCI, WHEN NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED.  WHEN NR 2 THROTTLE WAS SET AT IDLE, THE LIGHT EXTINGUISHED.  FLIGHT DIVERTED TO IND, WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CORE DETECTOR, UPPER FAN COWL DETECTOR, AND FIRE WALL DETECTOR AS PRECAUTIONARY.  REPLACED LOWER FAN COWL DETECTOR.  (W)


REMARKS:
IND - FLT 1819 - FLIGHT EN ROUTE TO LAX, AIRCRAFT ELEVATOR TRIM CAUSED A NOTICEABLE VIBRATION.  FLIGHT DIVERTED TO IND,WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE CHECKED ELEVATOR TRIM CONTROLS IN PEDISTAL, ELEVATOR TRIM, STAB CONTROL CABLES, AND STABILIZER TRIM JACKSCREW SETTING.  ALL FOUND WITHIN LIMITS AND OK.  UNABLE TO DUPLICATE EVENT.  (W)


REMARKS:
PIT - FLT 1104 - WHILE CLIMBING OUT OF PIT AT 13000 FEET, THE AFT CARGO DOOR WARNING LIGHT ILLUMINATED.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE RELEASED AFT CARGO DOOR WARNING LIGHT ON MEL 52-3.  FOUND SENSOR TARGET SPRING ROD OUT OF BRACKET.  REASSEMBLED AND LUBED BRACKET ROD AND GUIDE, OPERATION OK.  (W)


REMARKS:
SFO - FLT 2106 - BIRD STRIKE ON RIGHT ENGINE ON TAKEOFF.  FLIGHT RETURNED TO SFO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED FAN BLADES NR 2, 3, 4, 5, 36, 22, 21, 23, 24, AND 17.  ALSO REPLACED RIGHT ENGINE OIL COOLER.  (W)


REMARKS:
TPA - FLT 2216 - UNABLE TO PRESSURIZE AIRCRAFT ON TAKEOFF.  FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND MAIN ENTRANCE DOOR FALSE LOCKED, RE-CLOSED DOOR.  (W)


REMARKS:
DURING Q-4 CHECK, FOUND LEVEL 2 COROSION AT STA 929, LEFT BETWEEN LONGERON 21 AND 22 LEFT BELTFRAME.  CORROSION WAS CLEANED AND TREATED, A SECTION OF BELTFRAME WAS REPLACED AS PER ARM 53-03 FIG 2A.  (CORROSION DUE TO OLD LAV SPILL).  (W)


REMARKS:
DURING Q-4 CHECK, FOUND LEVEL 2 CORROSION AT STA 889 BELTFRAME, FROM LONGERON 18 LEFT TO 24 FEET.  CORROSION WAS CLEANED AND TREATED, AND A REPAIR STRAP INSTALLED AS PER EA 27668.  (CORROSION FROM OLD LAV SPILL).  (W)


REMARKS:
GSO - DURING SCHEDULED MAINTENANCE CHECK VISUAL, FOUND ONE INCH CRACK AT STA 736 ABOVE STR 19 L.  REPAIRED PER SRM 53-30-3 FIG 6.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND ,5 INCH BY 19 INCHES CORROSION STA 967-986.5.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 10R CRACKED AT FASTENER HOLE.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND PREVIOUS REPAIR DOUBLER CORRODED AT BS 1088, LBL 7 TO RBL 7.  REPLACED DOUBLERAND CHORD PER TRAMCO EWO 94-0842, 94-0868 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 825, LBL 23.5, WL 156.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, S4R AND 4L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FRAME HAT CHANNEL CORRODED AT BS 305, LBL 11 TO LBL 45, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


