# SDR

REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER DAMAGED AT BS 334, S10R, AND STRINGER CRACKED AT BS 294, AT S4R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 265, BETWEEN S17R AND S18L, BS 282, S15L, BS 827, BETWEEN S9 AND 10R, BS 920, WL 204, S17-18L, BS 342 AND 350, BETWEEN S20 AND 21R, BS 355, BETWEEN S18R AND 19R, AT BS 338, S18R, BS 1064, AT S22R, BS 378, BETWEEN S19 AND 20R, AND BS 920, BETWEEN S17 AND 18L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN CREASED AT BS 767 TO 820, AT S24 TO 26L, AND BS 460, FROM S28L TO S28R, AT SHEAR TIE LOCATION.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN S27 R AND L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED FROM LOWER EDGE TO FASTENER HOLE, BS 294, WL 208, RBL 55.  REPLACED FRAME PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND TOP CHORD Z-ANGLE CORRODED AT BS 270, RBL 2 LBL 10, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND NR 5 SLAT SKIN LOWER T/E SKIN CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DRAWING BAC 65C30133.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 616, S8L, AND AT BS 663.75 AT S10L AND R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED FROM BS 390 TO 400, BETWEEN S19 AND 20R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 328 LBL 49 WL 208, BS 294 LBL 10 TO RBL 10 WL 208, BS986.5 WL 208 RBL 57 TO LBL 57, BS 312 LBL 10 RBL 10 WL 208, AND AT BS 344 RBL 10 TO LBL 40 WL 208.  REPLACED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178 RBL 5.5 WL 198.  REPAIRED PER TRAMCO EWO 95-0337.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED AT REINFORCING STRAP, LBL 5.7.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN WEB AT BS 726, STRINGER 18A RIGHT SIDE.  REPAIRED PER SWA RA 1-553-1286.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 4 TO RBL 2.  REPAIRED PER SWA RA 1-553-1277.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 5.0.  REPAIRED PER SWA RA 1-553-1282.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 5.0.  REPAIRED PER SWA RA 1-553-1279.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 21.0.  REPAIRED PER SWA RA 1-553-1278.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 48 TO RBL 53.  REPAIRED PER SWA RA 1-553-1283.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 15.  REPAIRED PER SWA RA 1-553-1280.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 25.75 TO 43.  REPAIRED PER SWA RA 1-553-1284.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 8 TO LBL 10.  REPAIRED PER SWA RA 1-553-1275.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 8.  REPAIRED PER SWA RA 1-553-1274.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 639 S1 S2L AND S2R, BS 616 S6L, BS 480 S8R, BS 727A S26L AND S25R, BS 500D S19R, BS 616 S2L, BS 616 S1 AND S5R, BS 887 S25R, BS 277 S15R, BS 663 S10L AND R, AND AT BS 520 S16L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE CRACKED AT BS 328 WL 174, BETWEEN S20 AMD 21L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 969, 2 INCHES ABOVE S19L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277 S16L WL 217.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGED AT BS 727 PLUS 11, S7R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR MOPSILL CORRODED FROM BS 277 TO 360 WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPT FRAME DENTED AT BS 500 RBL 46 WL 169, BETWEEN S22 AND 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOORWAY LOWER AFT CORNER SKIN CRACKED AT BS 344 RBL 65 WL 211.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL AND BOEING DRAWING 65C27287-11.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND HORIZONTAL WEB TIES CRACKED AT BS 360 LBL 61 WL 274 AND AT WL 253.5.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908 S4R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMEROUS SKIN GOUGES AT BS 360 TO 368, S4L TO 5L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOORWAY LOWER FWD FRAME SECTION CRACKED AT LOWER I/B CORNER, BS 294.5 WL 208RBL 55.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR OUTER SKIN CRACKED ABOVE LOWER HINGE CUTOUT FWD CORNER, BS 300 WL 228 RBL 65.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 998 TO 1003, BETWEEN S13 AND 14L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
CLT 2234 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE REMOVED INSULATION FROM OUTFLOW VALVE AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER.  REFERENCE USAA950381.


REMARKS:
GSO - FLT 8002 - FLIGHT EN ROUTE MLB TO BWI WHEN THROTTLES SPLIT.  AIRCRAFT DIVERTED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT ENGINE PRBC.  RAN ENGINE, OPS CHECK GOOD.  (W)


REMARKS:
CLT - FLT 1263 - AFTER TAKEOFF GSP, LEFT LANDING GEAR RED LIGHT REMAINED ON.  CREW RECYCLED NO HELP.  LIGHT FLICKERED OFF AND ON THROUGHOUT FLIGHT.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE ADJUSTED LEFT GEAR UPLOCK SENSOR.  SENSOR TEST PER MM 32-61-0 CHECKS OK.  (W)


REMARKS:
CLT 2234 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE REMOVED INSULATION FROM OUTFLOW VALVE AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER.  REFERENCE 95ZZZW782.


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND LEVEL II CORROISON REF CPCP TASK NR C58-5330 STATION 1322 RIGHT LAV FLOORBEAM. REMOVED CORROSION TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER, REPAIR ANGLES AND STRAP PER USAIR TYPICAL REPAIR 53-10-19.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN FRAME STATION 160 AT CENTER OF AIRCRAFT IN E/E COMPARTMENT.STOP DRILLED CRACK AND INSTALLED SPLICE REPAIR AND DOUBLER PER SRM 53-03 FIG 2A.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND A GOUGE BEYOND LIMITS AT STATION 1174 AND 1193 LOWER FLANGE OF BEAM, AFT CARGOCEILING STRUCTURE.  ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR ANGLES PER SRM 53-05 FIG 86.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.375 INCH CRACK AT STATION 1322 LONGERON 17 LEFT.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-03 FIG 32.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND 2 INCH CRACK AT STATION 1290-1300 CUSP MEMBRANE LEFT SIDE LONGERON 18L.  SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 97.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK AT STATION 1305 RT SIDE CUSP MEMBRANE.  SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 97.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND CORROSION AT STATION 807 LONGERON 28-30 RIGHT IN SKIN.  REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 53.  (W)


REMARKS:
PIT - DURING SCHEDULED SIP INSPECTION REF 53-10-05, FOUND .5 INCH CRACK CENTER LINE BEAM VI FORWARD PRESSURE BULKHEAD.STOP DRILLED CRACK ENDS AND INSTALLED TWO ANGLE DOUBLERS PER USAIR EA 30058.  (W)


REMARKS:
PIT - DURING SCHEDULED SIP VISIT REF 53-10-20, FOUND .5 INCH CRACK UPPER FORWARD CORNER OF THE SERVICE EMERGENCY DOOR APERTURE CUTOUT.  EDDY CURRENT INSPECTION.  REMOVED DAMAGED AREA AND INSTALLED FILLER PLUG AND DOUBLERS PER SRM 53-0216.(W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF SCHEDULED PRODUCTION CONTROL ITEM NR 105, FOUND 13/16 INCH CRACK AT TOP FORWARD CORNER OF FWD CARGO DOOR FRAME AT STA 370 BELOW LONGERON 19.  VISUAL INSPECTION AND HFEC.  INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-05 FIG 68.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 15 INCH AREA OF SURFACE CORROSION, STATION 947 TO 967 AT RBL 46.  REPAIRED PER SRM 51-10-9.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH BY .017 DEEP CORROSION, STATION 312 RIGHT SIDE NEXT TODOOR SILL.  REPAIRED PER TR BG 53-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
CLT - THE CAPTAINS WINDSHIELD LOST TAPING AND SEALER AT 12,000 FEET.  THE SEALANT OBSTRUCTED THE VIEW OF THE WINDSHIELD.  FLIGHT RETURNED TO CLT.  MAINTENANCE RESEALED THE CAPTAINS WINDSHIELD.  (M)


REMARKS:
FLT NR 5 - JFK - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO FIRE WARNING.  DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES.  FOUND INTERGRATED DRIVE GENERATOR, MFG P/N 28B26313A, FAILURE AND OVERHEAT DAMAGE TO PLUMBING AND ELECTRICAL WIRING.  REPLACED ENGINE S/N 4131.  INVESTIGATION INTO NR 2 ENGINE SHUTDOWN DUE TO FIREWARNING, REVEALED INTEGRATED DRIVE GENERATORFAILED DUE TO INSUFFICIENT LUBRICATION SUPPLY.  ENGINE S/N 4131 WAS REPAIRED AND RETURNED TO SERVICE.  (W)


REMARKS:
FLT 280 - LAX - AFTER TAKEOFF NR 2 ENGINE STALLS.  REDUCED POWR NR 2 ENGINE.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE S/N 1422.  ENGINE OPERATION CHECKS NORMAL.  S/D - INVESTIGATION INTO ENGINE S/N 1422 COMPRESSOR STALLS, REVEALED A 6TH STAGE COMPRESSOR BLADE, MFG P/N 771706, FRACTURED DUE TO IMPACT CAUSING THREE OTHER 6TH STAGE BLADES TO FRACTURE RESULTING IN HEAVY DOWN STREAM DAMAGE TO LOW PRESSURE AND HIGH PRESSURE COMPRESSORS.  ENGINE REPAIRED AND RETURNED TOSERVICE.  (W)


REMARKS:
ABQ - FLT 1473 - FLIGHT EN ROUTE PHX TO CLT WHEN CABIN PRESSURIZATION WARNING SOUNDED.  FLIGHT DIVERTED TO ABQ WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND CARGO NET LODGED IN FORWARD CARGO DOOR.  REMOVED NET AND CLOSED DOOR.  OPS CHECK OK.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH BS 747 TO BSL 767 LBL 24 INCHES.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES BS 967 LBL 24.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH DIAMETER CORROSION AT SCREW HOLE, BS 975 RBL 18.  REPAIRED PERSRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 180 INCHES OF CORROSION BS 727C TO BS 827 S-25L.  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 1.5 INCH BY 2 INCH CORRODED AREA BS 987 LBL 50.  REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 4 SQUARE INCH BS 987 LBL 50 TO RBL 50.  REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-10-01A, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.75 INCH DIAMETER CORROSION BS 947 LBL 4.  REPAIRED PER EA 39037.  REPAIRED PER EA 39037.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 927 TO BS 1006 AT AFT ENTRY DOOR.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02,  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 967-986.5 AT AFT SERVICE DOOR.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES BS 967 RBL 18 INCHES.  REPAIRED PER SRM 53-60-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH BS 947 TO 967 LBL 18 INCHES.  REPAIRED PER SRM 53-60-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 3 INCH BY 3 INCH CORROSION TOP FLANGE AREA BS 947 TO BS 967 LBL 60 INCHES.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROISON AT SCREW HOLES, BS 787-767 S-25R.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 36 INCH BY 3 INCH CORRODED AREA BETWEEN BS 294 AND 344 RBL 55.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 947-967 48 INCHES LBL AT AFT ENTRY DOOR.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG BY 2 INCH WIDE CORROSION TOP OF INTERCOSTAL BS 312 TO BS 328 RBL 12 INCHES.  REPAIRED PER SRM 53-10-01.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 40 INCH CORRODED AREA AFT CARGO STRAP BS 787-847.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (W)


REMARKS:
DURING C-CHECK INSPECTION, FOUND INTERCOSTAL Z-CHANNEL CORRODED OUT OF LIMITS FORWARD AND AFT OF FLOOR BEAM AT BS 1050,BL 12L.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND 5 INCH CRACK ON SKIN KEEL BEAM AREA BETWEEN STA 930 AND STA 940 RIGHT.


REMARKS:
DURING C-CHECK INSPECTION, FOUND INTERCOSTAL UPPER ATTACH ANGEL CRACKED FIVE PLACES BETWEEN FLOOR BEAM 950A AND 950B, B.L.O.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM AT BS 1090, B.L.O., CORRODED OUT OF LIMITS (4 INCH AREA).


REMARKS:
DURING C-CHECK INSPECTION AND C.P.C.P. INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CORRODED AT BS 500, STR 27L (APPROXIMATELY 3 INCH AREA).  CORROSION OUT OF LIMITS.


REMARKS:
DURING C-CHECK INSPECTION, FOUND NR 2 SLAT ACTUATOR INBOARD TRUNNION MOUNT LUG CRACKED.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM INTERCOSTAL FROM BS 344 - BS 360 AT BL 10R CORRODED.  FABRICATED REPLACEMENT INTERCOSTAL OF 7075-T6, DASH 090 T-ANGLE PER SRM 51-40-3.  TREATED AND PRIMED PER SRM 51-10-2.  INSTALLEDPER SRM 51-30-2.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SKIN BULGED AT STA 1070, STR 28R.  FOUND STRINGER SECTION (10 INCH) CORRODED.  REMOVED DAMAGED SECTION, FABRICATED REPAIR SECTION PER SRM 53-10-3.  TREATED AND PRIMED AND INSTALLED PER SRM 51-10-2 AND SRM 53-10-3.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND INTERCOSTAL CORRODED AT BS 1070, JUST INSIDE L2 DOOR, CORRODED BEYOND LIMITS.  FABRICATED REPLACEMENT INTERCOSTAL USING 7075-T6, .040 INCH PER SRM 51-10-1.  TREATED.  PRIMED, INSTALLED PER SRM 51-10-2, SRM 51-30-2, AND SOP 20-50-1.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK BENEATH NR 1 GALLEY FROM BS 344 - BS 380 AT BL 22R AND BL 52R. REMOVED DAMAGED SECTIONS.  FABRICATED REPLACEMENT SEAT TRACK SECTIONS.  TREATED AND RPIMED PER SRM 51-10-1, SRM 51-10-2.  INSTALLED PER SRM 51-30-2.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK AT BS 420 - BS 450, BL 52R, CORRODED.  REMOVED SEAT TRACKS, FABRICATED REPLACEMENT TRACKS IAW SRM 51-10-1.  TREATED, PRIMED, AND INSTALLED PER SRM 51-10-2 AND SRM 53-10-5.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK AT BS 380 - BS 400, BL 24R, CORRODED.  REMOVED SEAT TRACKS, FABRICATED REPLACEMENT TRACKS IAW SRM 51-10-1.  TREATED, PRIMED, AND INSTALLED PER SRM 51-10-2 AND SRM 53-10-5.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM AT BS 344 FROM BL 10R TO BL 45R CORRODED.  FABRICATED REPLACEMENT UPPER CHORD FROM BAC1505-100617, 7075-T3 EXTRUSION PER SRM 51-30-5.  TREATED AND PRIMED PER SRM 51-10-2.  INSTALLED PER SRM 53-10-8.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM CORRODED AT STA 328 - BL0 18L.  REMOVED DAMAGED SECTION.  FABRICATED REPAIRS PER BOEING REPAIR PLAN M-7272-95-0282.  TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED PER M-7272-95-0282 AND SRM 51-30-2.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM CORRODED AT BS 380, BL 0-10L, AND BL 10-40R.  REMOVED DAMAGED SECTION OF FLOOR BEAM UPPER CHORD.  FABRICATED REPAIRS WITH 7075-T6; .050 INCH, AND 7075-T6; .080 INCH, MATERIAL PER SRM53-10-8 AND BOEING REPAIR FAX M-7272-95-0287.  TREATED AND PRIMED PER SRM 51-10-2.  INSTALLED PER SRM 51-30-2 AND SRM 53-10-8, FIGURE 3.


REMARKS:
DURING INSPECTION OF AD 91-06-06, FOUND STR 19L AT BS 675 EXFOLIATED ON INBOARD LOWER FLANGE.  REMOVED DAMAGED AREA OF STRINGER.  FABRICATED STRINGER SPLICE FROM BAC 1498-125, 7075-T6 STRINGER MATERIAL AND NEW STRINGER TIE FROM .040 INCH, 7075-T6.  TREATED MATERIALS, PRIMED, AND INSTALLED IAW SRM 51-20-1, SRM 53-10-3, SRM 51-10-2, AND SRM 51-30-2.


REMARKS:
DURING BOEING C.P.C.P. INSPECTION, FOUND SKIN BULGE AT STR 26R, STA 359.  CUT OUT DAMAGED STRINGER SECTION.  SKIN NOT DAMAGED.  FABRICATED REPAIR FILLER AND DOUBLER FROM 7075-T6.  TREATED PARTS AND PRIMED, AND INSTALLED IAW SRM 51-40-4, SRM 51-20-2, SRM 51-20-4, AND SRM 51-30-2.


REMARKS:
DURING C-CHECK INSPECTION, FOUND CORROSION DAMAGE ON UPPER CHORD OF THE BS 400, FLOOR BEAM FROM RBL 9.1 TO RBL 11.6.  CUT OUT DAMAGED AREA, FABRICATED SHIMS, AND REPAIR ANGLES.  TREATED AND INSTALLED PER BOEING REPAIR FAX M-7272-95, AND SRM 53-10-8, DATED JANUARY 16, 1995.


REMARKS:
DURING C-CHECK INSPECTION, FOUND INTERCOSTAL BETWEEN STA 1090 - STA 1100, STR 6L, GOUGED ON INBOARD FLANGE.  BLENDED DAMAGE OUT OF LIMITS PER SRM 53-10-1, FIGURE 1.  FABRICATED REPAIR DOUBLER, FROM 7075-T6, .071 INCH, TREATED, PRIMED, AND INSTALLED PER SRM 51-40-3, FIGURE 1, SRM 51-10-2, S.O.H.M. 20-41-02.


REMARKS:
DURING C-CHECK INSPECTION OF AD 91-06-06 PER KIWI INTERNATIONAL AIRLINES EA 2753S001 PTS II AND III, FOUND SKIN CORRODED AT LAP STR 19R, STA 490.  CUT OUT DAMAGED AREA (3 INCHES), FABRICATED REPAIR DOUBLERS, TREATED, PRIMED, INSTALLED, ANDSEALED PER SRM 53-30-3, FIGURE 5, SRM 53-30-03, FIGURE 3, SRM 51-20-4, SRM 51-30-5, AND SRM 20-49-03.


REMARKS:
STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN.  TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR ANDHAZE DISSIPATED, RETURNED TEMPERATURE CONTROL TO NORMAL RANGE.  REPLACED TEMPERATURE CONTROL AMPLIFIER, (P/N 607146-2-2) AND WATER SEPARATOR COALESCER, (P/N 179460-8-1).  AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL.  CHECK C-12 - 1-11-95 - STL.  REF 95ZZZZ251.


REMARKS:
STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN.  TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR ANDHAZE DISSIPATED, RETURNED TEMPERATURE CONTROL TO NORMAL RANGE.  REPLACED TEMPERATURE CONTROL AMPLIFIER, (P/N 607146-2-2) AND WATER SEPARATOR COALESCER, (P/N 179460-8-1).  AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL.  CHECK C-12 - 1-11-95 - STL.  REF 95ZZZZ250.


REMARKS:
FLT 558 - ATL-BNA - RETURNED TO ATL DUE TO A LEFT MAIN GEAR GREEN LIGHT ON.  DURING APPROACH TO ATL NO NOSE DOWN LOCK INDICATION.  REMOVED AND REPLACED LEFT GEAR DOWN LIMIT SWITCH AND LIGHT BULBS FOR NOSE GEAR DOWN LOCK LIGHT.  (W)


REMARKS:
ATL/BDL - FLT 450 - AIRCRAFT RETURNED TO GATE DUE TO THE LOSS OF FUEL OUT OF THE RIGHT WING TIP VENT.  REPLACED BOTH FLOAT VALVES IN LEFT WING AND REPLACED FORWARD AND AFT FUEL PUMP VOLUTES.


REMARKS:
PBI\IAD - FLT 466 - CREW EXPERIENCED AN 800 POUND FUEL IMBALANCE FROM RIGHT WING TO LEFT.  AIRCRAFT LANDED IN IAD WITHOUT INCIDENT.  IAD MAINTENANCE FILLED AIRCRAFT FULL OF FUEL AND RAN ALL PUMPS.  NEXT, TAXIED AIRCRAFT USING BRAKES AND THROTTLE ABRUPTLY, NO LOSS OF FUEL.  COULD NOT DUPLICATE.


REMARKS:
FLT 290-1 - RDU-IAD - RETURNED TO RDU WITH THE E/E DOOR OPEN LGHT ON.  CLOSED E/E DOOR, LIGHT WENT OUT.  (W)


REMARKS:
FLT 518 - EN ROUTE FROM ATL-PHL, EXPERIENCED ERRATIC VOLTS AND FREQUENCIES ON NR 2 GENERATOR.  CREW DISCONNECTED CSD.  PLACED ON MEL 24-1-1, MEL LOG PAGE NR 3037.  (W)


REMARKS:
FLIGHT NR 392 - EN ROUTE FROM FLL-ATL - HAD TO DISCONNECT NR 2 CSD DUE TO ERRACTIC VOLTS AND FREQUENCIES.  REMOVED AND REPLACED GENERATOR CONTROL PANEL.  (W)


REMARKS:
EMERGENCY ESCAPE PATH LIGHTING AT ROWS 14 THROUGH 21 INOP.  FOUND BROKEN SPLICE IN OVERHEAD AT AFT BATTERY PACK/CHARGER.  REPLACED SPLICE, OPS CHECKED OK.  (W)


REMARKS:
FLT NR 542 - PBI - ATL, INBOUND TO ATL PILOT REPORTED TO DISPATCH THAT LEFT MAIN FUEL TANK INDICATOR READS 3800 LBS LESS THAN RIGHT MAIN TANK AND DECLARED EMERGENCY WITH LEFT TANK DEPLETED.  FOUND LT TANK EMPTY AND FOUND CENTER TANK WITH 5400 LBS OF FUEL.  TRANSFERRED FUEL FROM CENTER TANK TO LT TANK.  RAN PUMPS IN LT TANK FOR TWO HOURS, NO TRANSFER OBSERVED, NO EXT LEAKS ON AIRFRAME OR ENGINE NOTED.  FUELED LT AND RT MAIN TANKS TO FULL, CENTER TANK EMPTY PER STICKS AND DISPATCHED ON LOCAL ACCEPTANCE FLIGHT FOR FURTHER EVALUATION.  ACCEPTANCE FLT AND OPS CHECK GOOD.


REMARKS:
DURING ROUTINE SHOP INSPECTION, FOUND 1 INCH CRACK IN OUTER COMBUSTION CHAMBER CASE REAR FLANGE.  REPLACED CASE.  NOTE: CRACKED CASE SCRAPED.  (X)


REMARKS:
PIT - FLT 0214 - EN ROUTE FROM CLT TO MKE, AIRCRAFT LOST APU AND ITS GENERATOR.  AIRCRAFT DIVERTED TO PIT.  MAINTENANCESERVICED THE RIGHT IDG WITH OIL.  OPERATIONS CHECKED GOOD. (M)


REMARKS:
FLT 248 - EN ROUTE FROM ATL TO MDW DIVERTED TO IND, CREW FELT VIBRATIONS FROM THE NR 2 ENGINE AND HAD 2 COMPRESSOR STALLS AS WELL.  AIRCRAFT LANDED WITHOUT INCIDENT.  REMOVED AND REPLACED NR 2 ENGINE (RT SIDE).


REMARKS:
ON APPROACH EWR, FLT NR 10, NR 1 ENG SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMPERATURE PER A 6-7.  FOUND FUEL HEAT VALVE FAILED OPEN.  REMOVED AND REPLACED VALVE PER 73-14-11.  PERFORMED INSPECTION AND GROUND RUN OPS CHECK OK AS PER PW MM 72-00, PG 518D.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH AREA OF CORROSION BS 305 AT LBL 36.  REPAIRED PER 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA CORROSION FLOORBOARD SUPPORT ANGLE 294.5 TO 312 LBL 12.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 137 INCH CORRODED AREA BS 727 D TO BS 945 AT RBL 14 INCHES.REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED AREA INBOARD END RT LAVATORY FORWARD WALL HAT CHANNEL AFT CABIN.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 7 INCH AREA CORRODED BS 957 RBL 25 TO RBL 50.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 967 LBL 40.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
LGA - FORWARD ENTRY EMERGENCY LIGHT INOPERATIVE.  MAINTENANCE REPLACED LIGHT ASSEMBLY IN FORWARD ENTRY AREA.  OPS CHECKOK.  (M)


REMARKS:
MEM - FLT 0358 - THE CREW RECEIVED AN ENGINE VIBRATION READING FROM THE NR 2 ENGINE.  THE CAPTAIN CUT THE ENGINE BACK TO IDLE AND DECLARED AND EMERGENCY.  FLIGHT LANDED WITH NO FURTHER INCIDENTS.  MAINTENANCE REMOVED THE SPINNER DUE TO THEPRESENCE OF MOISTURE AND REINSTALLED.  (M)


REMARKS:
PHL/ATL - FLT 547 - THE RIGHT FLYING DOOR SEPARATED FROM THE AIRCRAFT, FLYING DOOR HINGE BROKEN.  REPLACED FLYING DOOR HINGE ASSY.


REMARKS:
AFTER TAKEOFF, UNABLE TO CONTROL CABIN PRESSURIZATION USING AUTO, STANDBY OR MANUAL.  AIRCRAFT RETURNED TO LAS AND MADEAN UNEVENTFUL LANDING.  INSPECTED AND PERFORMED BITE TEST, ALL SYSTEMS NORMAL PER BOEING M/M.  RIGHT PACK THEN TRIPPED ON GROUND AND WOULDN'T RESET.  REPLACED TURBINE INLET SENSOR PER BOEING M/M.


REMARKS:
CLT - FLT NR 0424 - WHILE EXTENDING THE GEAR FOR LANDING, THE NOSE GEAR UNSAFE LIGHT AND NOSE GEAR DOOR OPEN LIGHT ILLUMINATED.  CAPTAIN FLEW BY THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN.  AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY.  MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH AND THE WIRING CONDUIT.  THE GEAR WAS CYCLED SEVERAL TIMES.OPERATIONS CHECKED GOOD.


REMARKS:
BWI - FLT NR 0451 - EN ROUTE TO CLT, THE APU FAILED.  THE CAPTAIN COULD NOT RESTART.  THE DECISION WAS MADE TO DIVERT TO BWI.  MAINTENANCE REPLACED THE APU FUEL SOLENOID VALVE AS A PRECAUTION AND THE FUEL FILTER.  OPERATIONS CHECKED GOOD.


REMARKS:
CLT - EXTERIOR AFT EMERGENCY LIGHTS AT BOTH AFT DOORS INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACKS AND CHARGER.


REMARKS:
FLT NR 7001 - ATL-ATL - PILOT TRAINER, ON APPROACH TO ATL HAD A RT GEAR UNSAFE IND, VISUALLY CHECKED GEAR BY TOWER AND PERISCOPE, LANDED.  ATL MAINTENANCE INSTALLED GEAR PINS ON TAXIWAY.  TAXI TO RAMP.  FOUND PUSHED PIN ON RT GEAR DOWN SWITCH, REPAIRED PIN, GEAR CHECKS OK PER MM 32-00.  (M)


REMARKS:
CLT - FLT 1257 - FLIGHT EN ROUTE FLL TO DCA WHEN WEATHER RADAR FAILED.  AIRCRAFT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED WEATHER RADAR TRANSCEIVER.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND LEVEL 2 CORROSION.  REF, TASK NR C58-5330 STATION 996 LEFT FLOORBEAM.  MANUAL FLOORBEAM CAP ANGLE FROM 7075-T6 EXTENSION AND INSTALLED REPAIR ANGLE PER SRM 53-05 FIG 72.  (M)


REMARKS:
BOS - FLT 0051 - THE COCKPIT EMERGENCY LIGHTS WOULD NOT TEST.  MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES.  (M)


REMARKS:
BWI - FLT NR 0451 - EN ROUTE TO CLT, THE APU FAILED.  THE CAPTAIN COULD NOT RESTART.  THE DECISION WAS MADE TO DIVERT TO BWI.  MAINTENANCE REPLACED THE APU FUEL SOLENOID VALVE AS A PRECAUTION AND THE FUEL FILTER.  OPERATIONS CHECKED GOOD.(M)


REMARKS:
PIT - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE RELAMPED THE LIGHTS AND REPLACED THE BATTERIES IN THE BATTERY PACK NR 1.  OPERATIONS CHECKED NORMAL.  (M)


REMARKS:
BOS - FLIGHT 0120 - WHILE ON ROTATION, THE CREW FELT A BUMP THEN NOTICED THE FORWARD CARGO DOOR LIGHT ILLUMINATED.  THECAPTAIN DECIDED TO RETURN TO BOS.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE PRESSURIZED THE AIRCRAFT AND CHECKED FOR LEAKS.  NONE WERE FOUND.  REMOVED CARGO NETTING OBSTRUCTING THE TARGET SWITCH.  OPERATION OF THE CARGO DOOR AND SEALS CHECKED GOOD.  (M)


REMARKS:
JFK - FLT 968 - ON INITIAL CLIMB-OUT OF LGA, 'A' SYSTEM HYDRAULICS FAILED.  FLIGHT DIVERTED INTO JFK WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED TEE FITTING AT RIGHT THRUST REVERSER PRESSURE SWITCH, 'A' SYSTEM HYDRAULICS RETURN, PRESSURE AND CASE DRAIN FILTERS, AND NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS.  (M)


REMARKS:
CLT - EXTERIOR AFT EMERGENCY LIGHTS AT BOTH AFT DOORS INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACKS AND CHARGER. (M)


REMARKS:
CLT - FLT NR 2195 - ON TAKEOFF FROM DCA EN ROUTE MSY, FUEL LEAK NOTICED ON LEFT WING AT ENGINE COWLING.  FLIGHT DIVERETED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  SECURED SCREW IN PANEL AT LEFT ENGINE TOP COWL AND RESEALED TANK,CHECKS OK.  (M)


REMARKS:
TPA - FLT 1569 - ON CLIMB-OUT OF TPA, NR 1 ENGINE OVERHEAT LIGHT CAME ON.  FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NOSE COWL ANTI-ICE DUCT.  (M)


REMARKS:
CLT - FLT NR 0424 - WHILE EXTENDING THE GEAR FOR LANDING, THE NOSE GEAR UNSAFE LIGHT AND NOSE GEAR DOOR OPEN LIGHT ILLUMINATED.  CAPTAIN FLEW BY THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN.  AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY.  MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH AND THE WIRING CONDUIT.  THE GEAR WAS CYCLED SEVERAL TIMES.OPERATIONS CHECKED GOOD.  (M)


REMARKS:
CVG - FLIGHT 0404 - CREW RECEIVED AN ERRATIC 'RIGHT OIL STRAINER CLOGGING' ANNUNCIATOR LIGHT BUT DID NOT EXTINGUISH WITH THE THROTTLE TO IDLE.  THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED.  THE FLIGHT DIVERTED TO CVG.  SINGLE ENGINE TIME WAS APPROXIMATELY 15 MINUTES.  MAINTENANCE DRAINED THE OIL TANK AND INSTALLED A NEW RIGHT MAIN OIL FILTER.  THEENGINE OIL WAS SERVICED.  NO LEAKS WERE FOUND.  (M)


REMARKS:
ROC - FLT NR 0581 - THE LEFT ENGINE FAILED AS THE GEAR WAS RETRACTED.  THE CREW RETURNED TO ROC.  FLIGHT LANDED WITHOUTFURTHER INCIDENT.  REPLACED FUEL PUMP.  (M)


REMARKS:
PHL - THE EMERGENCY FLOOR LIGHTING BATTERY PACKS WERE FOUND TO BE INOPERATIVE AT ROWS 1, 4, 6, 9, 13, 19, 25, 26, AND 29.  MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHTING BATTERY PACKS.  (M)


REMARKS:
CLE - THE MAIN ENTRANCE DOOR OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
GSO - FLT NR 2622 - AFTER TAKEOFF FROM CLT EN ROUTE ALB, STAB TRIM WHEEL MADE A LOUD GRINDING NOISE.  AUTOPILOT TRIM WAS THE SAME.  FLIGHT DIVERTED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED BEARINGS FOR STAB TRIM MAINSHAFT IN PEDESTAL.  STAB TRIM OPERATES NORMAL IN BOTH MANUAL AND ELECTRIC MODE.  (M)


REMARKS:
BWI - FLT 126 - FLIGHT EN ROUTE MCO TO DCA WHEN ANTI-SKID INOP LIGHT ILLUMINATED.  FLIGHT DIVERTED TO BWI DUE TO RUNWAYLENGTH.  MAINTENANCE REPLACED ANTI-SKID CONTROL UNIT.  (M)


REMARKS:
FLT 522 - SMOKE SMELL AFT OF EMERGENCY OVERWING EXITS.  INSPECTION OF LIGHTS, SPEAKERS, CALL BUTTONS AND WIRING IN OVERWING EXIT AREAS AND BEHIND PANELS.  NO DEFECTS NOTED MM 25-00.  (M)


REMARKS:
FLIGHT 528 - AFT PBE WAS FOUND TO BE FAULTY AND DETERIORATED.  MAINTENANCE REPLACED PBE IN AFT OVERHEAD BIN RIGHT SIDE,THE LAST BIN, P/N 4566M37-B-042NN S/N OFF E9446743 S/N ON E9547745.


REMARKS:
DURING CLIMBOUT, EXPERIENCED SYSTEM A HYDRAULIC PRESSURE LOSS.  AIRCRAFT RETURNED TO ONT AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND HYDRAULIC LINE TO RIGHT MAIN GEAR UPLOCK ACTUATOR RUPTURED.  REPLACED LINE AND SERVICED SYSTEM PER BOEING M/M.


REMARKS:
DURING CLIMBOUT, EXPERIENCED SYSTEM A HYDRAULIC PRESSURE LOSS.  AIRCRAFT RETURNED TO ELP AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND A SYSTEM HYDRAULIC PUMP INOP. REPLACED AND SERVICED SYSTEM PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE FRAME AT BS 520, FAILSAFE ATTACH ANGLE HAS TOOLING MARK DAMAGE AT S16R AFTOF RT WING SCANNING LIGHT HOUSING.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND CRACK EXTENDING FROM BENEATH RT UPPER TORQUE TUBE SUPPORT FITTING IN O/B CHORD, BS 1156 BULKHEAD.  REPAIRED PER SWA ACO 473-53.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CRACKED AT UPPER CHORD FWD FLANGE RADIUS AT RBL 45.5.  REPAIRED PER SWA ACO 583-53-R3.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT LIGHTENING HOLE ON TOP SIDE OF APU CAVITY.  INSTALLED WEB REPAIR PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE AT BS 344 AT BL 0.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND SHEAR TIE CRACKED AT BS 598, FWD SIDE S17L, BELOW CREASE BEAM.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 663, AT INBOARD EDGE OF VERTICAL SUPPPORT ANGLE, RBL 24.75.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND BOEING DRAWING 691A0032.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT BS 599, AT FLOOR LEVEL.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE FRAME CRACKED BELOW WING ROOT, BS 540.  REPAIRED PER SWA ACO 518-53.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOOR BEAM ATTACH POINT, BS 360, BL 0.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOOR BEAM ATTACH POINT, BS 360, BL 0.  REPAIRED PER BOEING STR.


REMARKS:
ACY - UPON LANDING, 3 EACH MAIN WHEEL ASSEMBLY TIRES BURST.  REMOVED AND REPLACED NR 1, NR 2, NR 3, AND NR 4 MAIN WHEELASSEMBLIES PER MM 32-45-01.  (X)


REMARKS:
DURING SCHEDULED TERM CHECK, FOUND A 1.7 FUSELAGE SKIN CRACK AT S23R, BS 727D AND AT S23R, MEASURING 1.6 LONG.  REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A CHECK, FOUND A 1.8 CRACK AT NOSE WHEEL WELL VERTICAL WEB RIGHT SIDE BELOW FWD ACCESS PANEL CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A-CHECK, FOUND NOSE GEAR RETACT ACTUATOR SUPPORT VERT WEB CRACKED AT RADIUS.  REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 320 AND S20R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND WEB AND FAILSAFE CHORD DAMAGE AT BS 344 AND S21R.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND BELTFRAME CRACKED 17 BELOW FLOORBEAM AT BS 328, RIGHT SIDE BETWEEN S20 AND 21R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 27R CORRODED AT FWD END AT BS 907.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOORWAY AFT CORNER WEB DAMGED AT L/E LOWER CORNER BS 492.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOORBEAM ATTACH POINT AT BS 360 AND BL 0.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT SIDE WEB CRACKED .5 AT FLANGE TO FUSELAGE SKIN, FLOOR LEVEL, BS 599.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
MCI - FLT 117 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG GREEN LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR AND GREEN LIGHT CAME ON.  REPLACED LANDING GEAR LEVER RELAY R2-28, MFG PN 9274-3643.  NLG OPERATION AND INDICATION CHECKED NORMAL.  CHECK C - 3-1-95 - STL.


REMARKS:
STL - FLT 631 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG GREEN LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR AND SWAPPED LIGHT BULBS.  ON SECOND APPROACH, GREEN LIGHT CAME ON.  REPLACED NLG DOWNLOCK SWITCH, MFG H14-6.  NLG INDICATION AND OPERATION CHECKED NORMAL.  CHECK C - 3-1-95 - STL.


REMARKS:
STL - FLT 324 - AFTER TAKEOFF, SHUT DOWN NR 2 ENGINE, SN 4468, DUE TO HIGH AVM ON BOTH A AND B VIBRATION CHANNELS.  CHECKED OIL SYSTEM CHIP DETECTORS, LUBRICATED FAN BLADES; PERFORMED FAN TRIM BALANCE.  ENIGNE OPERATION CHECKED NORMAL.  CHECK C-9B - 2-1-95 - JFK.


REMARKS:
ORF - FLT 694 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE GEAR GREEN, DOWN, AND LOCKED LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR.  FOUND WIRE, C216B24, WITH HIGH RESISTANCE AND INTERMITTENTLY OPEN.  REPLACED WIRE, G216B24, BETWEEN CONNECTOR P1-133 PIN 6 AND S3-49 TERMINAL STRIP.  NOSE LANDING GEAR OPERATION AND INDICATION SYSTEM CHECKED NORMAL.  CHECK C - 3-1-95 - STL.


REMARKS:
EWR/TPA - FLT 39, AFTER TAKEOFF, UNABLE TO PRESSURIZE AIRCRAFT.  AIRCRAFT RETURNED TO EWR.  FOUND LT FLOW CONTROL VALVEFAILED IN CLOSED POSITION DUE TO 3 BROKEN WIRES.  REPAIRED WIRES AND C/P REPINNED.  PRESSURE CHECKED PER MM 21-00-01 AND MM 21-31-00.  OPS CHECK NORMAL.  (X)


REMARKS:
FLT NR 466 - PBI-IAD - CREW EXPERIENCED AN 400 LB FUEL IMBALANCE FROM RIGHT WING TO LEFT.  AIRCRAFT LANDED IN IAD WITHOUT INCIDENT.  IAD MAINTENANCE FILLED AIRCRAFT FULL OF FUEL AND RAN ALL PUMPS.  NEXT, TAXIED AIRCRAFT USING BRAKES AND THROTTLE ABRUPTLY, NO LOSS OF FUEL.  COULD NOT DUPLICATE.


REMARKS:
FLT NR 513 - ATL-MCO - AFTER AIRCRAFT WAS ON CLIMB-OUT FROM ATL, ANOTHER AIR CARRIER REPORTED FUEL COMING FROM THE RIGHT WING TIP.  AIRCRAFT IMMEDIATELY RETURNED FOR LANDING.  TRANSFERRED FUEL FROM LEFT TANK TO RIGHT TANK WHICH STOPPED SIPHONING OF FUEL.  TRIED TO DUPLICATE CONDITIONS UNSUCCESSFULLY.  PERFORMED TEST FLIGHT, SYSTEM CHECKS OK.  (M)


REMARKS:
FLT 154 - AFTER AIRCRAFT STARTED IT CLIMB-OUT FROM MSY, THE NR 2 ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED.  CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO MSY WITHOUT INCIDENT.  REMOVED ADN REPLACED THE NR 2 ENGINE.


REMARKS:
FLT NR 179 - AFTER LANDING IN ATL, CREW SHUTDOWN NR 2 ENGINE FOR SINGLE ENGINE TAXI.  BOTH AFT LAV SMOKE DETECTORS STARTED SOUNDING.  FLIGHT ATTENDANT REPORTED TO THE PILOTS AND CAPTAIN SHUTDOWN THE RIGHT PACK OFF.  ONE SMOKE DETECTOR SHUTOFF.  NO SMOKE OR FLAMES WERE REPORTED BY THE CREW.  RAN BOTH ENGINE AND PACKS, CHECKED AIRCRAFT CABIN AND TAIL COMPARTMENT, CHECKED AFT CABIN BALLAST AND NOTED NO OVERHEAT CONDITION OR INOP ITEMS.


REMARKS:
CLT - EXTERIOR EXIT LIGHTS AT THE AFT ENTRY DOORS ARE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER ASSY.  REFERENCE USAA950531.


REMARKS:
MIA - SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 24 AND 25 DO NOT ILLUMINATE.  MAINTENANCE REPAIRED A BROKEN WIRE AT ROW 24.  RELEASED EXIT LIGHT ON ROW 25 ON MEL 33-19A.  REPLACED CHARGER (P/N RPSIB) AND BATTERY PACK. (M)


REMARKS:
CLT - EXTERIOR EXIT LIGHTS AT THE AFT ENTRY DOORS ARE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER ASSY.  (M)


REMARKS:
CLT - FLT 44 - FLIGHT EN ROUTE FLL TO LGA WHEN NR 1 ENGINE PARAMETERS BEGAN FLUCTUATING.  CREW DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 1 ENGINE MEC.  PERFORMED TRIM RUN AND LEAK CHECK, OPS CHECKS OK.  AIRCRAFT OK FOR SERVICE.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND DOOR SILL SKIN CORRODED BS 794-847 IN AFT CARGO DOOR CUTOUT.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 2 INCH CORRODED AREA, BS 328 FLOORBEAM, RBL 14 AND RBL 21.  REPAIRED PER TR 53-10-03 AND SRM 53-10-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 60 INCH CORRODED AREA S-17L, BS 312-372 (FORWARD ENTRY DOOR SILL ANGLE).  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TOTAL AREA OF CORROSION .25 INCH BY 10 INCH, 6 INTERCOSTALS CORRODED AND NUTPLATE HOLES BS 294-344, 3 AT LBL 11 BS 294-344, 3 AT RBL 11 BS 294-344.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION OUT OF LIMITS .25 INCH BY 10 INCHES ON INTERCOSTAL AT BS 947 THROUGH 967 RBL 10 INCHES.  REPAIRED PER SRM 51-10-0.  CORROSION TASK NR C53-108-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA ON INTERCOSTAL AT CABIN BS 907 THROUGH 947 RBL 10 INCHES.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION (FULL WIDTH OF T-CAP) STATION 986.5 FLOORBEAM FROM 44 LBL TO 44 RBL.  REPAIRED PER SRM 51-70-13 EA 39205.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCH BY 5 INCH CORROSION ON FLOORBEAM AT STATION 947, RBL 12.REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-02, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 5 INCH AREA ON FLOORBEAM, CORRODED AT STATION 947, LBL 12.  REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA CORRODED ON FLOOR SUPPORT AT STATION 947 TO STATION 967, LBL 50.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 1 INCH TOTAL CORROSION ON INTERCOSTAL, BETWEEN BS 967 AND BS 947 LBL 16 INCHES.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-10-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 7 INCH BY 1 INCH CORROSION ON INTERCOSTAL BETWEEN BS 947 AND BS 967 RBL25 INCHES.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT STATION 967 TO 986.5, LBL 17.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 10 INCHES CORRODED AREA ON FLOORBEAM AT STATION 967 RBL 9 TO RBL 36.  REPAIRED PER EA 39247.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 36 INCHES OF CORROSION, AFT ENTRY THRESHOLD.REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION 2 INCHES BY 30 INCHES 'Z' ANGLE IN THRESHOLD OFAFT SERVICE DOOR.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-2, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH DIAMETER AND 3 INCH DIAMETER SPOTS OF CORROSION 40 TO 50 PERCENTLOSS TO .375 INCH DIAMETER 100 PERCENT LOSS 3 INCH BY 4 INCH CORROSION BS 807 TO BS 845 ON DOOR SILL BELOW AFT CARGO DOOR.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA ON FLOOR HAT CHANNEL, BS 308 (AFT BULKHEAD FOR FORWARD LAVATORY).  REPAIRED PER SRM 51-10-1 FIG 1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH AREA OF CORROSION ON INTERCOSTALS BS 328 THROUGH BS 344 RBL 12 AND LBL 12.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK, 5.25 INCH BY 2 INCH CORRODED AREA BS 540, RBL 6.5 (LOWER FLANGE OF KEEL BEAM).  REPAIRED PER EA 5369-20 EA 39273 EA 39272.  CORROSION TASK NR C53-212-01.  CORROSION LEVEL 2.(M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 15 INCH TOTAL CORROSION, CORROSION AT SCREW HOLES ON FLOORBEAM AT BS 312 LBL 12 INCHES THROUGH RBL 24 INCHES.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 SQUARE INCHES OF CORROSION OF FLOORBEAM AT STATION 344 BL 0 TO LBL 12.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 15 INCH CORRODED AREA ON INTERCOSTAL AT BS 312 THROUGH BS 328.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
PIT - DURING AN FC-6 CHECK INSPECTION, FOUND .75 INCH CRACK IN RIGHT NR 2 WINDOW POST (TYPE 3) REF SIP 53-10-08.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-10-01 REV A.  (M)


REMARKS:
PIT - DURING AN FC-6 CHECK INSPECTION, FOUND 2 DENTS IN THE FORWARD SIDE OF THE AFT CARGO COMPARTMENT DOOR FRAME IN AREA OF HOLD OPEN ROD SUPPORT.  INSTALLED DOUBLER REPAIR PER SRM 53-02-16 PG 4.  (M)


REMARKS:
PIT - DURING SCHEDULED SIP VISIT INSPECTION, FOUND .375 INCH CRACK IN THE SED APERATURE AT THE FORWARD UPPER CORNER REFSIP 53-10-20 OUTSIDE LAYER OF SKIN (EDDY CURRENT INSPECTION).  CUT OUT CRACKED AREA AND INSTALLED FILLER AND DOUBLER REPAIRS (2 EACH) PER SRM 53-02-16 PG 7, 8 AND 9.  (M)


REMARKS:
DURING CLIMBOUT FROM LIT,  CREW EXPERIENCED NR 1 ENGINE LOW OIL PRESSURE INDICATION WITH ASSOCIATED WARNING LIGHT.  CREW PERFORMED NR 1 ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT RETURNED TO LIT AND MADE AN UNEVENTFUL LANDING.  INSPECTED ENGINE. REPLACED NR 1 ENGINE OIL PUMP, ENGINE GEARBOX ASSEMBLY, AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.  OIL PUMP P/N:  734340.  S/N OFF:  AV2800.  S/N ON:  AV3829.


REMARKS:
DURING CLIMBOUT FROM ELP, NR 4 L/E SLAT WOULD NOT FULLY RETRACT.  INDICATED IN TRANSIT.  CYCLED SYSTEM TWICE, NO HELP.AIRCRAFT RETURNED TO ELP AND MADE AN UNEVENTFUL LANDING.  REPLACED NR 4 L/E SLAT ACTUATOR PER BOEING M/M.


REMARKS:
DURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED THREE PLACES AT BS 227.8, BETWEEN S13 AND 16L.  REPAIRED PER DALFORT XEA X2-53-154.


REMARKS:
DURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED  AT AFT LOWER CORNER OF FORWARD AIRSTAIRS DOORWAY CUTOUT AT THREE PLACES AT BS 227.8, BETWEEN S13 AND 16L.  REPAIRED PER DALFORT XEA X2-53-154.


REMARKS:
DURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED  AT AFT LOWER CORNER OF FORWARD AIRSTAIRS DOORWAY CUTOUT AT DOUBLER.  REPAIRED PER DALFORT XEA X2-53-153.


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


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND A HOLE IN STRINGER 27L ON INNER J FLANGE, BS 1047.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM AT STATION 328 RBL 48.  REPAIRIED PER 53-10-03.CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
ATL-MDW - FLT 79 - ON CLIMB-OUT, NR 8 LEADING EDGE SLAT SHOWS INTRANSIT WHEN FLAP ARE RAISED.  AIRCRAFT RETURNED TO ATL.  REMOVED AND REPLACED NR 8 LEADING EDGE SLAT ACTUATOR AS PER MM 27-31-32.  OPS CHECK OK.  (M)


REMARKS:
FLT NR 537 - EN ROUTE TO TPA - AFTER TAKEOFF THE FORWARD ACCESSORY COMPARTMENT DOOR LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO ATL.  RESET FORWARD ACCESSORY COMPARTMENT DOOR.


REMARKS:
MCO-ATL - FLT NR 22 - DURING CLIMB-OUT, NR 2 ENGINE N1 ACCELERATED TOWARD RED LINE, THROTTLE RETARDED AND N1 STABILIZEDAT 80 PERCENT.  NO RESPONSE TO THROTTLE MOVEMENT.  ENGINE SHUTDOWN NORMAL AFTER AIR RETURN TO MCO.  REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL FOR NR 2 ENGINE PER MM 73-21-2 AND MM 73-11-1, OPS CHECK OK.


REMARKS:
NR 2 ENGINE FAILED CREATING A FIRE THAT DESTROYED AIRCRAFT.  MOVED AIRCRAFT FROM RUNWAY TO EAL HANGAR AREA FOR FURTHER INVESTIGATION INTO THE CAUSE OF ENGINE FAILURE.  7TH STAGE DISK DISINTEGRATED.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT AT LOWER OUTER SKIN.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM WEB CRACKED AT BS 709, BL 0 WL 204.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT LOWER EDGE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN DAMAGED 6 INCHES ABOVE LOWER HINGE CUTOUT OUTER EDGE AND CRACKED AT RIVET HEAD 1 INCH ABOVE LOWER CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807 AND BS 887, AT S9L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 344, S8R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER HAT SECTION SUPPORT AT BS 867, S9L AND AT BS 907, S9L.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, S10L AND S10R, AND AT BS 1138, S13L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NR 3 SLAT CRACKED AT T/E SKIN O/B OF ACTUATOR AND NR 4 SLAT CRACKED AT LOWER T/E SKIN, I/B OF ACTUATOR.  REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 727E PLUS 13 BETWEEN S2 AND 3L, AT BS 796, S3L, AT BS 278, BETWEEN S2 AND 3L, AT BS 488, S3L, AT BS 847 AND 858, S3L, AND AT BS 727D PLUS 3.75, ABOVE S3L.  REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT AT LOWER I/B CORNER.  REPAIRED PER BOEING BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, LBL 11.4 AND AT WL 212, LBL 4.7.  REPAIRED PER BOEING BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, S4L.  REPLACED PER BOEING BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 27 AND 31.5.  REPLACED PER SWA RA 1-353-542.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE FROM BS 860 TO BS 887, BETWEEN S2L AND S2R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


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


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSLAGE SKIN DENTED AT BS 1054, S17-18R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED CHECK, FOUND NOSE GEAR WHEELWELL LEFT VERTICAL WEB CRACKED JUST BELOW LEFT FWD ACCESS PANEL CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED CHECK, FOUND NOSE GEAR RETRACT ACTUATOR SUPPORT VERTICAL WEB CRACKED JUST BELOW LEFT FWD ACCESS PANEL CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
ABORTED TAKEOFF DUE TO MASTER CAUTION INDICATING FWD ENTRY DOOR OPEN.  RETURNED TO GATE.  INSPECTED AND FOUND DOOR SECURED AND LOCKED.  PLACED DOOR WARNING ON MEL 52-2.  INSPECTED TIRES/BRAKES AND CONTINUED PER BOEING M/M.


REMARKS:
ON APPROACH, CREW EXPERIENCED A-SYSTEM PRESSURE LOSS.  AIRCRAFT LANDED WITHOUT INCIDENT.  INSPECTED AND FOUND AN AILERON PCU LINE RUPTURED.  REPLACED LINE, FLUSHED SYSTEM, AND INSPECTED FILTERS PER BOEING M/M.


REMARKS:
NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED.  ENGINE POWER WAS REDUCED TO IDLE, NO HELP.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT LANDED AT ABQ WITHOUT INCIDENT.  INSPECTED ENGINE FILTER, NO DEFECTS NOTED.  CLEANED FILTER, PLACED INDICATOR ON MEL 79-2, AND CONTINUED PER BOEING M/M.


REMARKS:
EMERGENCY PATH LIGHTING WOULD NOT COME ON WITH COCKPIT SWITCH FOUND ON MAINTENANCE CHECK RON ATL.  REPAIRED BROKEN WIREFROM S1-177 TO S1-387.


REMARKS:
MIA - FLT NR 1166 - THE EPR GAUGE FOR THE NR 2 ENGINE FAILED AFTER TAKEOFF.  THE FLIGHT DIVERTED TO MIA.  REPLACED PT2 LINE AND TIGHTENED PT7 LINE.  (M)


REMARKS:
PIT - FLIGHT 0856 - AIRCRAFT RETURNED TO PIT DUE TO THE LEFT AILERON BINDING.  NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY.  MAINTENANCE LUBED THE LATCHED CONTROL MIXER ASSEMBLY AND RECHECKED THE AILERON TAB DEFLECTION FORCE LEFT AND RIGHT WING.  (M)


REMARKS:
DAY - FLT NR 0152 - FLIGHT DIVERTED TO DAY DUE TO THE NR 2 ENGINE OIL PRESSURE DECREASING.  CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE OIL TANK DUE TO LEAKAGE.  LEAK CHECKED GOOD.  (M)


REMARKS:
PIT - FLT 0728 - AFTER TAKEOFF, THE TOWER NOTICED A PIECE OF THE MED TRIM FLAPPING.  FLIGHT RETURNED TO PIT.  MAINTENANCE CUT THE LOOSE INTERIOR TRIM THAT WAS HANGING OUTSIDE OF THE DOOR.  OPERATIONAL GOOD.  (M)


REMARKS:
CLT - FLT NR 1287 - THE EMERGENCY FLOOR PATH LIGHTING BETWEEN ROWS 6 AND 11 WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPAIRED A DAMAGED WIRE ON THE FLOOR TRACK LIGHT.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
BWI - FLT 2101 - AT FL 370 - THE AIRCRAFT LOST THE RIGHT PACK.  CREW DESCENDED TO FL 250.  THE AIRCRAFT COULD NOT MAINTAIN CABIN ALTITUDE AND THE PRESSURIZATION WAS LOST.  CREW MADE AN EMERGENCY DESCENT TO 10,000 FEET.  THE CABIN ALTITUDE THEN ROSE TO 15,000 FEET AND THE PASSENGER OXYGEN MASKS DEPLOYED.  THE AIRCRAFT LANDED IN BWI WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE LEFT COOLING TURBINE.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
PHL - FLT 1150 - CREW RETURNED TO PHL DUE TO A LOUD FLAPPING NOISE.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE FUONDPART OF THE RAIN SEAL NOT SECURED.  THEY REMOVED THE RAIN SEAL.  AIRCRAFT CHECKED GOOD.  (M)


REMARKS:
PHL - FLT NR 1468 - PRIOR TO FLAP EXTENSION, THE RIGHT HYDRAULIC QUANTITY DROPPED TO TWO QUARTS.  EMERGENCY WAS DECLARED.  THE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR LEAKING AT THE CYLINDER AND REPLACED THE CYLINDER.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
CLT - FLT 1170 - CAPTAIN ADVISED THAT THE APU GENERATOR WAS LOST AT APPROXIMATELY 40 MILES OUT OF CLT.  FLIGHT RETURNEDTO CLT.  FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT.  REPLACED GCU.  (M)


REMARKS:
PIT - DURING SCHEDULED INSPECTION USAIR PCI 289 CD 53F00762, FOUND A .5 INCH CRACK IN STRINGER 68 RT SIDE AFT OF FRAME 3870.  INSTALLED SPLICE REPAIR TO STRINGER 68 PER SRM 51-70-06.  (M)


REMARKS:
PIT - DURING SCHEDULED INSPECTION OF USAIR CD 53F00762 HFEC INSPECTION OF STRINGERS NR 6, 7, 68 AFT OF FRAME STATION 3870, FOUND .5 INCH CRACK (RADICAL) AT STRINGER NR 68 RT SIDE FRAME 3870.  INSTALLED SPLICE REPAIR TO STRINGER 68 RT SIDE AFT OF FRAME STATION 3870 PER SRM 51-70-06.  (M)


REMARKS:
IND - DURING BX CHECK VISIT AND SCHEDULED PRODUCTION CONTROL ITEM USAIR EO NR 5388D292F EDDY CURRENT INSPECTION OF EXTERNAL FUSELAGE SKIN FOUND A CRACK IN LONGERON NR 3R STATION 756.  REMOVED CRACKED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 FIG NR 2.  (M)


REMARKS:
CLT - FLT 263 - UNABLE TO PRESSURIZE AIRCRAFT.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND CANNON PLUG LOOSE ON THE OUTFLOW VALVE.  CLEANED AND SECURED CANNON PLUG.  (M)


REMARKS:
CAK - FLT 0237 - ON APPROACH, THE COMPUTER REPORTED ERRONEOUS GEAR NOT DOWN MESSAGES.  A FLYBY WAS PERFORMED.  THE CAPTAIN DECLARED AND EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE SENSOR.  OPERATIONSCHECKED GOOD.  (M)


REMARKS:
SDF - FLIGHT NR 0438 - ON INITIAL RETRACTION, THE RIGHT GEAR UNSAFE LIGHT ILLUMINATED.  AFTER RE-EXTENDING THE GEAR THEGEAR DOOR OPEN LIGHT ILLUMINATED.  THE CREW DECIDED TO RETURN TO SDF.  MAINTENANCE REPLACED THE RIGHT GEAR DOWNLOCK SWITCH.  DOOR OPERATION CHECKED NORMAL.  (M)


REMARKS:
DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .75 INCH CRACK TOP PYLON TO FUSELAGE ATTACH ANGLE STATION 1019 LEFT PYLON. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 10.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR RT SIDE FUSELAGE AT STATION 294-313 LONGERON 18R AND21R.  INSTALLED CLASS I REPAIR PER SRM 53-04 FIG 12B.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR RT FUSELAGE SKIN AT STATION 965 LONGERON 14R.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 32.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK BRACKET STATION 692 JUST OUTBOARD OF KEEL BEAM FORWARD OF MAIN GEAR DOOR ACTUATOR UPPER ATTACH POINT.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .5 INCH CRACK RT FORWARD EMERGENCY EXIT WINDOW TOP AFT STOP.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 965 LONGERON 13L AT TOP HI-LOCK.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR.  INSTALLED FUSELAGE NOSE SKIN RADOME HINGE AREA STATION 37.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 77.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION OUTBOARD WEB OF FLOORBEAM WHERE IT ATTACHED TO BELTFRAME STATION 996.  CORROSION TASK NR C58-53300.  REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 72 AND USAIR EA NR 30252.  (M)


REMARKS:
CLT - FLT 0456 - WHILE CLIMBING OUT OF CLT, FLIGHT ENCOUNTERED A COMPERSSOR STALL.  THE CAPTAIN POWERED BACK TO IDLE THEN UP AGAIN AND GOT ANOTHER COMPRESSOR STALL.  FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT.  REPLACED ENGINE ASSEMBLY.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND DENT IN BOTTOM OF BULKHEAD STATION 965 RT.  INSTALLED DOUBLER REPAIRPER SRM 53-03 FIG 19.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR LEFT FUSELAGE SKIN STATION 965 BETWEEN LONGERON 13L AND 14L.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 32.  (M)


REMARKS:
CLT - FLT 97 - FLIGHT EN ROUTE PIT TO MIA WHEN RADAR QUIT WORKING.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENACNE REPLACED R/T UNIT.  RADAR WORKED NORMAL.  (M)


REMARKS:
PIT - FLT 1069 - AFTER DEPARTURE FROM PIT, CREW WAS UNABLE TO TURN RADAR ON.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED R/T UNIT.  RADAR WORKED NORMAL.  (M)


REMARKS:
CLT - FLT 955 - FLIGHT EN ROUTE BWI TO BHM WHEN LEFT WING BODY OVERHEAT LIGHT CAME ON.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED OVERHEAT ACCESSORY UNIT.  OPS CHECK NORMAL.  (M)


REMARKS:
PHL - FLT NR 63 - CREW NOTICED FLUCTUATION IN NR 1 ENGINE DURING CLIMB-OUT OF PHL.  FUEL FLOW/EPR AND N1 FLUCTUATIONS WERE NOTED ALONG WITH A SLIGHT OIL PRESSURE FLUCTUATION.  CREW RETURNED TO PHL WITH NR 1 ENGINE AT IDLE.  MAINTENANCE REPLACED FUEL PUMP AND FUEL CONTROL UNIT PER M/M 73-21-2.  RAN ENGINE AND LEAK CHECKS GOOD.  (M)


REMARKS:
JAX - FLT 104 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF.  FLIGHT RETURNED TO JAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NOSE LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC FLEX LINE.  (M)


REMARKS:
EWR - FLT 371 - LOUD BANGING NOISE ON CLIMB-OUT.  WARNING STRAP CAUGHT IN FORWARD GALLEY SERVICE DOOR.  FLIGHT RETURNEDTO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REMOVED STRAP FROM FORWARD GALLEY SERVICE DOOR.  INSPECTED DOOR AND FUSELAGE, NO DAMAGE FOUND.  (M)


REMARKS:
BWI - FLT 2190 - FLIGHT EN RUOTE ORD TO PHL, WHEN NR 2 ENGINE FILTER BYPASS LIGHT CAME ON AND NR 2 ENGINE SHUTDOWN.  FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED OIL FILTER BYPASS SWITCH AND ENGINE OIL FILTER.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 16L BS 500 C PLUS 4 INCHES.  REPAIRED PER EO 5393X228.  (M)


REMARKS:
ORF - FLT 694 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE GEAR GREEN, DOWN, AND LOCKED LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR.  FOUND WIRE, G216B24, WITH HIGH RESISTANCE AND INTERMITTENTLY OPEN.  REPLACED WIRE, G216B24, BETWEEN CONNECTOR P1-133 PIN 6 AND SE-49 TERMINAL STRIP.  NOSE LANDING GEAR OPERATION AND INDICATION SYSTEM CHECKED NORMAL.  CHECK C - 3-1-95 - STL.


REMARKS:
MCI - DURING OP-17, FOUND CORROSION IN FORWARD CARGO BELLY SKIN, STA 680 TO STA 686, BETWEEN STR 28R AND STR 27L.  REPAIRED PER SRM 53-30-3, FIGURE 3A, SHEETS 1-3.  AIRCRAFT TOTAL TIME:  37,842 HOURS; 23,911 CYCLES.


REMARKS:
DURING CHECK C, FOUND A 1.25 INCH RADIAL CRACK AT TOP LEFT SIDE OF AFT VENTRAL DOOR JAMB, RUNNING CIRCUMFERENTIALLY IN RADIUS OF DASH 13 ANGLE.  STOP DRILLED PER EMLR NR 65704 AND REPLACED FASTENERS PER SRM CHAPTER 51 AND TWA STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  43,613 HOURS; 43,279 CYCLES.


REMARKS:
MCI - DURING CHECK C, FOUND CORROSION AT AFT EDGE OF AFT SERVICE PANEL, STA 1183.  REPAIRED PER ARA NR 9346.  AIRCRAFT TOTAL TIME:  40,176 HOURS; 26,185 CYCLES.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON LONGERON 30, AT 6 FASTENERS BETWEEN STA 484 AND STA 503.  REPAIRED PER SRM 53-02, FIGURE 14,  AIRCRAFT TOTAL TIME:  66,307 HOURS; 81,289 CYCLES.


REMARKS:
STL - DURING CHECK C, FOUND .0312 INCH CRACKS COMING OUT OF 4 RIVET HOLES, STA 160 TO STA 200, LONGERON 22L.  REPAIRED PER ARA 65706.  AIRCRAFT TOTAL TIME:  61,210 HOURS; 72,666 CYCLES.


REMARKS:
LGW - FLT 720 - DURING CRUISE, SMOKE AND ELECTRICAL ODOR EMITTED FROM OVERHEAD LIGHT NEAR FIRST CLASS GALLEY.  FOUND BROKEN LAMP BASE, MFG PN 1695, IN SOCKET.  REMOVED LAMP BASE AND INSTALLED NEW LAMP.  LIGHT OPERATION CHECKED NORMAL.  CHECK C-2 - 10-19-94 - MCI.


REMARKS:
STL - DURING OP-15, FOUND .75 INCH CRACK BETWEEN 5 AND 6 HOLE FORWARD END OF RIGHT TRAPEZOIDAL PANEL.  INSTALLED NEW PANEL PER SRM 57-09.  AIRCRAFT TOTAL TIME:  66,307 HOURS; 31,289 CYCLES.


REMARKS:
MCI - DURING AIRCRAFT SERVICE NR 4, FOUND A .75 INCH CRACK AND A 1 INCH CRACK AT LBL 60, STA 948.  REPAIRED BY INSTALLING DOUBLER PER ARA 9335.  AIRCRAFT TOTAL TIME:  64,349 HOURS; 43,814 CYCLES.


REMARKS:
MCI - DURING AIRCRAFT SERVICE NR 4, FOUND A 1 INCH CRACK AT LBL 57, STA 940.  REPAIRED BY INSTALLING DOUBLER PER ARA 9335.  AIRCRAFT TOTAL TIME:  64,349 HOURS; 43,814 CYCLES.


REMARKS:
DURING MAINT FERRY FLIGHT AFTER RUDDER CHANGE, AIRCRAFT LOST A-SYSTEM HYDRAULICS.  AIRCRAFT RETURNED TO PAE AND MADE ANUNEVENTFUL LANDING.  INSPECTED AND FOUND A-SYSTEM SHUTTLE VALVE LEAKING.  REPLACED AND SERVICED SYSTEM PER BOEING M/M.


REMARKS:
WEATHER RADAR ANTENNA BECAME INOPERATIVE.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  REPLACED RADAR ANTENNA MOTOR AND OPERATIONAL CHECKED PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, NUMBER 1 NOSE GEAR TIRE TREAD SEPARATED.  AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING.  REPLACED BOTH NOSE GEAR WHEEL ASSEMBLIES AND INSPECTED AIRCRAFT FOR DAMAGE PER BOEING M/M.


REMARKS:
STL - FLT 651 - DURING LANDING, SMOKE APPEARED IN COCKPIT.  FOUND AUTO GROUND SPOILER ACTUATOR, MFG PN 1040T100-5, HAD OVERHEATED CAUSING SMOKE.  REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL.  CHECK C - 8-16-94 - STL.


REMARKS:
ONT - FLT 221 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND.  CYCLED LANDING GEAR AND NOSE GEAR EXTENDED.  FOUND NOSE LANDING GEAR TRANSFER CYLINDER, MFG PN 69-14106-5, WITH INTERNAL MALFUNCTIONS.  REPLACED TRANSFER CYLINDER AND NOSE LANDING GEAR, OPERATION CHECKED NORMAL.  CHECK C-2 - 9-18-94 - MCI.


REMARKS:
DURING CRUISE, EXPERIENCED INTERMITTENT FIRE WARNING ON NR 3 ENGINE WHICH CEASED UPON POWER REDUCTION AND RECURRED DURING DESCENT INTO SJC.  INSPECTION REVEALED A CLAMP ON THE COWLING CONTACTING THE FIRE SENSOR ELEMENT.  REPOSITIONED CLAMPON COWLING AND SYSTEM CHECKED OK.  AIRCRAFT RETURNED TO SERVICE.


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND LEVEL 1 CORROSION STATION 980 FLOOR BEAM RIGHT LAVATORY, TASK NR C57-53300.  INSTALLED FILLER AND SUPPORT ANGLE PER SRM 53-10-14.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK AT HI-LOK AT LONGERON 3 LEFT STATION 180.  INSTALLED SPLICE REPAIR PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK FUSELAGE SKIN RIGHT AFT NOSE GEAR DOOR AFT HINGE AREA.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER USAIR TYPICAL REPAIR 53-30-19.  (M)


REMARKS:
CLT - FLT 129 - UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHERINCIDENT.  MAINTENANCE FOUND MLG AIR SAFETY SENSOR TO TARGET CLEARANCE EXCESSIVE.  ADJUSTED SENSOR PER MM 32-09-01.  OPS CHECK NORMAL.  (M)


REMARKS:
MCI - DURING OP-17, FOUND RIGHT WING RIB CRACKED AT STR 9, STA 686.  REPAIRED PER SB 57-A159 AND SSRM 57-20-201.  AIRCRAFT TOTAL TIME:  38,173 HOURS; 24,723 CYCLES.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B BETWEEN S4 AND 5L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND BS 1156 BULKHEAD LEFT CHORD CRACKED 1.5 INCHES IN LENGTH AND RUNNING VERTICALLY.  REPAIRED PER SWA ACO 473-53 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND APU AIR INLET O/B WEB CRACKED 1 INCH LONG WITH A HOLE .25 INCH WIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FAIRING SUPPORT BELT FRAME CRACKED 2 INCHES BELOW AIR DUCT.  REPAIRED PER SWA ACO 518-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND COMPRESSION CHORDS CRACKED AT BS 663.75, LBL 24.75 AND AT RBL 24.75.  REPAIRED PER BOEING DRAWING 691A0032 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT SERVICE DOORWAY WEB BELOW ASSIST HANDLE CRACKED AT UPPER END.  REPAIRED PER SWAACO 471-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, FWD OF S2 AT RADIUS.  REPAIRED PERSWA ACO 587-57.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED AT BS 540 AT TOP FAIRING SUPPORT FRAME.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FLOOR BEAM SUPPORT STRAP CRACKED AT RBL 31 IN E AND E COMPARTMENT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED B/C3 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED IN AFT LOWER CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT OF AFT SERVICE DOOR.  REPAIRED PER BOEING S/B 737-53-1074 AND STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED CHECK, FOUND NOSE WHEELWELL LEFT VERTICAL WEB CRACKED 3.1 INCHES, BELOW FWD LEFT ACCESS PANEL.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AT 35,000 FT, CREW EXPERIENCED NUMBER 2 ENGINE FLAME-OUT.  SUCCESSFULLY RESTARTED ENGINE AT 15,000 FT.  AIRCRAFT DIVERTED TO ELP AND MADE A NORMAL LANDING.  TROUBLESHOT AND BORESCOPED ENGINE, NO DEFECTS NOTED.  REPLACED ENGINE FUEL SHUTOFFVALVE, ENGINE MEC AND FUEL PUMP.  CHECKED START LEVER SWICTH, CDP LINE AND ALL LINES ON ENGINE.  FUEL S/O VALVE:  P/N 61163, S/N 128 MEC:  P/N 8063208, S/N 60 FUEL PUMP P/N 7086002, S/N 18348.


REMARKS:
TPA/ATL - FLT 120 - UPON GEAR EXTENSION, THE LEFT MAIN GEAR DID NOT HAVE A DOWN AND LOCK INDICATION.  CAPTAIN DECLARED AN EMERGENCY AND LANDED WITH GEAR DOORS DOWN.  NO FURTHER PROBLEMS REPORTED.  REPLACED DOWNLOCK SWITCH CANNON PLUG P1-132 AND NEW PINS ON ALL WIRES.  PERFORMED GEAR RETRACTION AND EXTENSION.  OPS CHECK NORMAL PER MM 32-50.


REMARKS:
FLT 198 - HAD AN IMPROPER LANDING GEAR INDICATION ON LEFT MAIN GEAR BEFORE LANDING.  REPAIRED THE WIRING AT THE LEFT MAIN GEAR DOWN LIMIT PLUG P-132.   OPS CHECK OKAY.


REMARKS:
PIT - FLT 8554 - DURING TAKEOFF AT ROTATION, THE AC LOST ALL INSTRUMENTATION.  THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO PIT.  MAINTENANCE REINSTALLED THE PITOT AND STATIC LINES.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
BDL-ATL - FLT 449 - ON TAKEOFF, LT ENGINE A LOOP ILLUMINATED, LT OIL STRAINER CLOGGING LIGHT ILLUMINATED, OIL PRESS DROPPED TO 35 PSI, WITH TEMP RAPIDLY RISING THROUGH 120 DEGREES ENGINE OPERATED AT IDLE FOR REMAINDER OF FLIGHT.  FOUND NOSE COWL ANTI-ICE DUCT BLOWN WHICH DAMAGED OIL PRESS DIFFERENTIAL SWITCH.  REMOVED AND REPLACED ANTI-ICE DUCT AND OIL PRESS SWITCH.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 12 INCHES FORWARD SERVICE DOOR THRESHOLD.  REPLACEDZ-ANGLE.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .75 INCH DIA AREAS OF CORROSION, STA 328 FLOORBEAM UPPER FLANGE BL 0 TORBL 56.  REPAIRED PER SRM 53-10-51, FIG 205.  REPLACED T-CAP LBL 32 TO RBL 56 PER SRM 53-10-51 FIG 205.  CORROSION TASKNR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION 2 INCHES BY 55 INCHES STA 937 TO STA 996 RT.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION  1 INCH BY 4 INCH, 75 PERCENT LOSS STA 947 TO STA 967 RBL 52 INCHES ON FLOORBEAM.  REPAIRED PER SRM 51-10-2, INSTALLED NEW BEAM.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 55 INCHES STA 940 TO STA 995 LT.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STA 967 TO STA 986 LBL 17 INCHES.  REPAIRED PER SRM 51-10-02, REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW PART.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


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


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STA 950 LBL 52 INCHES.  REPAIRED PER SRM 51-10-02, REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW ONE.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 3 INCH CORROSION, BS 500 PLUS 6 INCHES BL 0.  REPLACED CHANNEL WITH NEW CHANNEL SRM 51-10-02.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCHES BY 1 INCH OF CORROSION BS 987.0 BL 40 LT T-CAP SECTION OF FLOORBEAM.  FABRICATED NEW T-CAP, STRAP AND REPAIR ANGLES AND INSTALLED SAME.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM 2 INCHES BY 42 INCHES, STA 344 BL 0 TO LBL 42 INCHES.  REMOVED T-CAP SECTION AND REINSTALLED SAME WITH DOUBLER ANGLES AND SPLICE STRAPS.  TR 53-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM 1 INCH BY 12 INCHES STA 328 RBL 6 TO LBL 63.  REPLACED UPPER T-CAP, TR 53-10-3.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH, TWO HOLES THROUGH ANGLE CORROSION FORWARD ENTRY DOOR SILL Z-ANGLE.  REPLACED Z-ANGLE SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 10 INCHES BY 10 INCHES CORROSION AREA ON FLOOR PAN AT LT LAVATORY DUMP CHUTE CUTOUT BS 1016 LBL 5.  INSTALLED WEB SKIN REPAIR SRM 51-70-13 FIG 1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH AND 1 INCH BY 6 INCH AREA CORRODED TOP OF FLOOR SUPPORT BS 1006 TO 1016, 36 INCHES LBL.  FABRICATED NEW WEB AND SUPPORT ANGLE, SRM 51-10-1, SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SHIM AT I/B END OF AFT LT LAVATORY FORWARD BULKHEAD WALL SUPPORT HAS CORRODED SCREW HOLE.  INSTALLED NEW INTERCOSTAL/SHIM.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED SCREW HOLE FLOORBEAM BS 986.5, 43 INCHES LBL.  INSTALLED UPPERT-CAP REPAIR, ENTIRE LENGTH TR 53-10-05.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORRODED AREA AND 2 CORRODED SCREW HOLES AFT LT LAVATORY DOORWAY, BS 1006 TO 1016.  INSTALLED NEW INTERCOSTAL SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.(W)


REMARKS:
INT - DURING Q-5 CHECK INSPECTION, FOUND 2 INCHES BY 6 INCHES CORRODED AREA, BS 1006 TO 1016 RT AFT LAVATORY DOORWAY FLOOR SUPPORT.  INSTALLED NEW INTERCOSTAL SUPPORT SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 4 CORRODED SCREW HOLES, RT AFT LAVATORY FLOOR SUPPORT BS 986.5 PLUS 7 INCHES TO 1006 13 INCHES RBL.  REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW ONE, SRM 51-10-02 PG 15.  CORROSION TASK NRC53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT -  DURING Q-5 CHECK INSPECTION, FOUND 1 INCH SQ CORRODED AREA S28R RT KEEL BEAM STA 506 O/B SIDE.  INSTALLED REPAIRANGLE EA 39374.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK INSPECTION, FOUND INTERCOSTAL, 2 CORRODED SCREW HOLES BS 986.5 TO BS 1006 13 INCHES LBL.  FABRICATED NEW INTERCOSTAL SRM 51-10-02 PG 15.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND INTERCOSTAL, 3 SCREW HOLES CORRODED BS 967 TO 986.5 18 INCHES LBL.  REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL, SRM 51-10-02 PG 15.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION 1 INCH BY 2 INCH SEAT TRACK AT STA 360 RBL 54.FABRICATED NEW SEAT TRACK SRM 51-10-02 PG 15.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 CORRODED SCREW HOLES RT AFT LAVATORY FLOOR SUPPORT BS 986.5 PLUS 7 INCHES TO 1006 36 INCHES RBL.  FABRICATED NEW SUPPORT SRM 51-10-02 PG 15.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
BWI - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE.  MAINTENANCE REPAIRED WIRING AT ROW 1C FLOOR LIGHTS.  REPLACED FORWARD FLOOR EMERGENCY LIGHTS BATTERY CHARGER.  REF USAA950608.


REMARKS:
PIT - FLT 1662 - AFTER DEPARTURE, CREW WAS UNABLE TO TRIM STABLIZER WITH THE YOKE SWITCHS.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED STAB TRIM MAIN ELECTRIC ACTUATOR.  OPS CHECK NORMAL.  (W)


REMARKS:
SAN - FLT 1152 - ON CLIMBOUT, NR 2 ENGINE OVERHEAT LIGHT CAME ON.  THROTTLE REDUCED TO IDLE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO SAN WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPOSITIONED CORE ENGINE DETECTOR.  RAN ENGINE AT TAKEOFF AND CLIMB SETTINGS, LIGHT REMAINED OFF.  (W)


REMARKS:
CLE - THE RT FORWARD SLIDE LIGHT INOPERATIVE.  MAINTENANCE FOUND SOCKET ASSEMBLY CORRODED.  REPLACED SOCKET ASSEMBLY, OPS CHECKED GOOD.  (W)


REMARKS:
BWI - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE.  MAINTENANCE REPAIRED WIRING AT ROW 1C FLOOR LIGHTS.  REPLACED FORWARD FLOOR EMERGENCY LIGHTS BATTERY CHARGER.  REF 95ZZZW801.


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 6 INCHES CORROSION S27L BS 948.8.  REPAIRED PER SRM 53-10-8.  CORROSIONTASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 20 INCHES CORROSION S21R BS 847 TO 867.  REPAIRED PER SRM 53-10-3 DETAIL 7.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
BWI - FLT 7004 - UNABLE TO PRESSURIZE AC AFTER TAKEOFF.  FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND DOOR SEALS ON BOTH CARGO DOORS OUT OF CHANNELS.  SECURED SEALS, AC PRESSURIZED NORMALLY.  (W)


REMARKS:
MCO - FLT 1018 - ON CLIMBOUT, LT WING BODY OVERHEAT LIGHT ILLUMINATED.  FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED LT ENGINE PYLON OVERHEAT SENSOR.  (W)


REMARKS:
CLT - FLT 1702 - ON CLIMBOUT, B-HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED AND QUANTITY LEVEL BEGAN TO DROP.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE CHANGED B-SYSTEM HYDRAULIC ELECTRIC PUMP LINE FROM ACCUM TO B-SYSTEM RETURN MODULE AND REPLACED B-SYSTEM ENGINE PUMP.  (W)


REMARKS:
LGA - FLT 505 - THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK, OPERATION OFLIGHTS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 348 - AFTER TAKEOFF, THE APU FIRE LIGHT ILLUMINATED.  THE CAPTAIN DISCHARGED THE BOTTLES AND THE LIGHT EXTINGUISHED.  FLIGHT RETURNED TO PIT.  MAINTENANCE FOUND THE APU FIRE DETECTION WIRE CHAFED THROUGH.  THE DETECTION ELEMENT, FIRE BOTTLE AND FIRE WIRE WAS REPLACED.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
RIC - FLT 2151 - ON CLIMBOUT, NR 1 ENGINE FIRE WARNING LIGHT AND OVERHEAT LIGHT ILLUMINATED, NR 1 ENGINE WAS SHUTDOWN.CREW FIRED THE BOTTLES INTO NR 1 ENGINE AND DIVERTED TO RIC WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 1 ENGINE PRSOV DUE TO LEAK AT SHAFT SEAL.  GROUND RUN LEAK CHECK GOOD.  (W)


REMARKS:
MCO - FLT 738 - CABIN ALTITUDE STARTED CLIMBING AT 9OO FPM AND REACHED 10,000 FT CABIN ALTITUDE, ALERT HORN SOUNDED.  FLIGHT DIVERTED TO MCO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED PRESSURE CONTROLLER, PRESSURE SELECTOR, AND OUTFLOW VALVE.  OPS CHECK NORMAL.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 30 INCHES STA 986 LBL, 12 INCHES TO FRAME.  REPAIRED PER EA 39362, T-CAP SECTION REPLACED PER EA 39362.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .75 INCH BY .75 INCH AREA OF CORROSION, STA 986.5 FLOORBEAM UPPER WEB RBL 4.  REPAIRED PER SRM 53-60-51 FIG 201, DOUBLER INSTALLED PER SRM 53-60-51 FIG 201.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCH STA 986 RBL, 25 INCHES TO FRAME.  REPLACED T-CAP PER EA 39362, REPAIRED PER EA 39362.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .75 BY .75 AREA OF CORROSION STA 986.5 FLOORBEAM WEB RBL 43.  REPAIRED PER SRM 53-60-51 FIG 201, DOUBLER INSTALLED PER SRM 53-60-51 FIG 201.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2. (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION FOUND APPROX 1 INCH BY 7 INCH AREA CORRODED STA 312 ON FLOORBEAM BL 0 RBL 7.  REPAIRED PER TR 53-10-03, CUT OUT CORRODED SECTION OF UPPER T-CAP AND SPLICED IN NEW SECTION.  THERE WAS LESS THAN ONE POUND ADDED FOR REPAIR.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
CLT - THE NR 2 ASPIRATOR ON LIFE RAFT, SERIAL NR TJ260 FAILED TEST.  MAINTENANCE REPLACED THE SLIDE ASPIRATORS.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 16 INCH CORROSION BS 312 TO BS 328 RBL 12.  REPLACED WITH PREFAB INTERCOSTAL SRM 51-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
DCA - FLT 1454 - UNABLE TO PRESSURIZE AC.  FLIGHT RETURNED TO DCA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE PRESSURIZED AC WITH APU AND BOTH ENGINES.  AC PRESSURIZED NORMALLY.  (W)


REMARKS:
ROC - FLT 2274  - UPON GEAR RETRACTION ON TAKEOFF, A-SYSTEM QUANTITY WENT TO ZERO AND A-SYSTEM LOW PRESSURE LIGHTS CAMEON.  FLIGHT RETURNED TO ROC WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND HYDRAULIC LINE LEAKING AT RTMAIN GEAR UPLOCK CYCLINDER.  REPLACED LINE.  (W)


REMARKS:
CLT - FLT 166 - AT APPROX FL 301, THE LT PACK WENT OUT MAKING A LOUD NOISE.  CREW DECIDED TO DIVERTED TO CLT.  MAINTENANCE REPLACED THE LT PACK ASSEMBLY, OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 446 - ON TAKEOFF, CREW RECEIVED AN ALERT MESSAGE OF A NR 1 HYDRAULIC SYSTEM FAILURES.  CAPTAIN DECLARED AN EMERGENCY AND LANDED IN CLT.  MAINTENANCE FOUND THE NR 1 ENGINE, NR 1 HYDRAULIC PRESSURE SWITCH CONTACTS FAULTY AND RPLACED THE SWITCH.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
RDU - FLT 109 - THE CABIN PRESSURE WOULD NOT CLIMB WITH ALTITUDE.  THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO RDU.  MAINTENANCE INSTALLED A NEW VALVE AT THE RT SIDE EXTERNAL AIR CONNECTION.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND 1 CRACK AT BS 178, BULKHEAD BETWEEN WL 218 AND S2L.  REPAIRED PER SWA RA 1-253-1320.


REMARKS:
AFTER GEAR RETRACTION, RIGHT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED.  CYCLED GEAR AND LIGHT EXTINGUISHED, THENILLUMINATED AGAIN.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  REPLACED GEAR PROXIMITY SENSOR, RIGHT GEAR UPLOCK SWITCH AND SEALS AT PRIORITY VALVE PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP.  REPLACED AFT BATTERY PACK AND REWIRED TRACK LIGHTING PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKS AT LEFT FUSELAGE JUST FWD AND BELOW EMERGENCY OVERWING EXIT LIGHT UNDER T/E FLAPS AT BS 727D, AT S23LT AND RT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND FWD SERVICE DOOR HINGE CUTOUT CRACKED, LOWER AREA.  REPAIRED PER SWA RA 1-352-224.


REMARKS:
AFTER TAKEOFF, NUMBER 2 L/E SLAT WOULD NOT RETRACT.  AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING.  REPLACEDNUMBER 2 L/E SLAT ACTUATOR PER BOEING M/M.


REMARKS:
DURING CLIMBOUT, EXPERIENCED NUMBER 2 ENGINE COMPRESSOR STALL.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND REPLACED NUMBER 2 ENGINE PER BOEING M/M.


REMARKS:
DURING CLIMBOUT, EXPERIENCED BIRD STRIKE TO NUMBER 2 ENGINE.  AIRCRAFT RETURNED TO HRL AND MADE AN UNEVENTFUL LANDING.INSPECTED AND FOUND 6 FAN BLADE TIPS BENT.  REPLACED BLADES AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND WEB CRACKED AT FASTENER HOLE IN UPPER RIGHT CORNER OF BS 178 BULKHEAD.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 534 AND 530, AT S14L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND FUSELAGE SKIN DOUBLER CRACKED JUST BEHIND RADOME AT 12 O'CLOCK POSITION.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS AT FWD ENTRY AND FWD SERVICE DOORS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


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


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FOUR CABIN TRACK LIGHTS INOP.  REPLACED LIGHTS PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND ONE CABIN TRACK LIGHT INOP.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
BDL/ATL - FLT 449 - AIRCRAFT RETURNED TO BDL DUE TO AFT AIRSTAIRS LIGHT CAME ON THE ANNUNCIATOR PANEL.


REMARKS:
RDU - FLT 298 - EN ROUTE, EXPERIENCED SPOTS ON THE RADAR INDICATOR.  AIRCRAFT RETURNED TO ATL DUE TO BAD WEATHER, RADARREQUIRED FOR FLIGHT THROUGH KNOWN WEATHER.  FOUND CANNON PLUG ON THE BACK OF THE ANTENNA EXTREMELY LOOSE, RECONNECTED AND REPLACED RADAR INDICATOR AS PRECAUTIONARY.


REMARKS:
ATL/MIA - FLT 591 - RETURNED TO ATL BECAUSE THE A/C WOULD NOT PRESSURIZE.  RESECURED THE E AND E DOOR.


REMARKS:
FLT 574 - AFTER TAKEOFF, LEFT HYDRAULIC TEMP HIGH LIGHT CAME ON.  AIRCRAFT RETURNED TO ATLANTA.  REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP.  P/N AS66411LS, S/N OFF 165614, S/N ON 179506.  OPS CHECK GOOD, NO LEAKS FOUND IAW MM CHAPTER 29-10-5.


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH STA 947 TO STA 967 RBL 17 INCHES.  REPAIRED PER SRM 51-10-1, REPLACED NEW BEAM.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION .5 INCH BY 2 INCH, SEAT TRACK STA 340 RBL 45.  INSTALLED NEW SECTION OF SEAT TRACK SRM 53-00-52 FIG 202.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1.5 INCH CORRODED AREAS AROUND CLIP NUT HOLES, BS 948LBL 11 TO RBL 49, CABIN FLOORBEAM.  REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
BWI - FLT 1120 - UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF.  FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED NOSE GEAR ACTUATOR.  (W)


REMARKS:
ONT - FLT 54 - RETURNED FROM FLIGHT ACCOUNT NR 3 ENGINE OIL BYPASS LIGHT CAME ON AND OIL TEMPERATURE ROSE.  FOUND METALIN MAIN OIL SCREEN.  REPLACED ENGINE SN 1543.  ENGINE TOTAL TIME:  34,195 HOURS; 22,195 CYCLES.  CHECK C-2 - 1-4-95 - MCI.  INVESTIGATION INTO NR 3 ENGINE, SN 1543, OIL BYPASS LIGHT ILLUMINATING AND OIL TEMPERATURE RISE, REVEALED NR 3 BEARING, MFG P/N 804509, FAILED.  REPLACED NR 3 BEARING AND REPAIRED RELATED COMPONENTS.  ENGINE S/N 1543 REPAIRED AND RETURNED TO SERVICE.


REMARKS:
BOS-BWI - FLT 1187 - AFTER TAKEOFF, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED.  FLIGHT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RT DUCT ASSEMBLY BETWEEN THE FLOW CONTROL VALVE AND HEAT EXCHANGER,LEAK AND OPERATIONS CHECKED GOOD.  (W)


REMARKS:
DCA-BWI - FLT 1178 - THE LT MAIN TIRE BLEW ON TAKEOFF, FLIGHT DIVERTED DUE TO THE GEAR DOWN.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LT O/B WHEEL ASSEMBLY (P/N 3910063507.  SPIN CHECKS GOOD.  (W)


REMARKS:
BUF - FLT 1463 - CAPTAIN RECEIVED AN OIL STRAINER CLOG LIGHT, IT DID NOT EXTINGUISH WHEN THE ENGINE WAS THROTTLED BACK TO IDLE.  THE LT ENGINE WAS THEN SHUTDOWN AND THE FLIGHT DIVERTED TO BUF.  FLIGHT LANDED WITHOUT INCIDENT.  SINGLE ENGINE TIME WAS 14 MINUTES.  MAINTENANCE REPLACED THE NR 1 ENGINE OIL PRESSURE DIFFERENTAIL PRESSURE SWITCH.  LEAK CHECKED NORMAL.  (W)


REMARKS:
CLT - FLT 514 - ON TAKEOFF, THE AC FAILED TO PRESSURIZE.  FLIGHT RETURNED TO CLT.  MAINTENANCE PERFORMED BITE CHECKS ONTHE CONTROLLERS.  ALL CHECKED GOOD.  (W)


REMARKS:
IND - DURING SCHEDULED SID INSPECTION REF:  PSE 53.09.009 AND 53.09.010, FOUND A 1 INCH CRACK IN LONGERON 3L AT STATION680.  CUT OUT DAMAGE AND INSTALLED SPLICE REPAIR PER USAIR EA 39338 AND SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA STR 1076 LONGERON 14R ON BELTFRAME.  BLENDED OUT CHAFED AREA, TREATED/PRIME, INSTALLED DOUBLER REPAIR UNDER FLANGE PER SRM 53-03 FIG 2A.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA AT STA 1059 LONGERON 20R ON BELTFRAME.  BLENDED OUT AREA, TREATED AND PRIMED INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 2A.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2.5 INCH CHAFED AREA AT STA 1059 LONGERON 14R BELTFRAME.  BLENDED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 2A.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION TO FWD CARGO DOOR JAMB WEB FWD LOWER CORNER AT STA 362.500 CPCP TASK C51-53300.  CUT OUT CORRODED AREA AND INSTALLED NEW SECTION OF WEB AND INSTALLED DOUBLER PER USAIR EA 30429.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION 6 INCH AREA PANEL NR 20 IN SUPPORT ANGLE AT STA 255, CENTER LINE, AREA PREVIOUSLY REWORKED.  CPCP TASK NR C58-53303.  SPLICED IN NEW SECTION OF ANGLE PER USAIR TYPICAL REPAIR 53-10-21A.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK BETWEEN STA 465 AND 484 LONGERON 24R TO 25R SKIN.  CUT OUT DAMAGED SKIN AND INSTALLED A FLUSH REPAIR PER USAIR EA 30543.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LIGHTNING STRIKES FROM STA 389 TO 408 BETWEEN LONGERONS 28R AND 29R SKIN.  INSTALLED INTERNAL DOUBLERS 4 INCH BY 6.5 AND 4 INCHES BY 8 INCHES PER SRM 53-04 VIEW E.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AFT CARGO DOOR JAMB BEAM.  PREVIOUS REWORK, CPCP TASK C57-53300.  SPLICED IN NEW JAMB BEAM SECTION PER SRM 53-05 FIG 63.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION BETWEEN STA 313 TO 370 RT I/B SEAT TRACK, PREVIOUS REWORK.  CPCP TASK C58-53306.  CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG L/F.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION BETWEEN STA 1007 TO 1155 RT TIE DOWN RAIL IN AFT CARGO, PREVIOUS REWORK.  CPCP TASK C57-53300.  SPLICED IN NEW SECTION OF TIE DOWN RAIL PER USAIR TYPICAL REPAIR 53-20-09A.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AFT CARGO LT SIDE BETWEEN STA 1155 TO 1211, PREVIOUS REWORK. CPCP TASK C57-53300, TIE DOWN TRACK.  CUT OUT CORRODED AREA, INSTALLED FILLER AND DOUBLER PER USAIR TYPICAL REPAIR 53-20-09A.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECITON, FOUND LEVEL 1 CORROSION BETWEEN STA 655 TO 712 LT SIDE TIE DOWN RAIL FWD CARGO.  PREVIOUS REWORK NOT A CPCP TASK.  CLEANED CORROSION AND INSTALLED DOUBLER REPAIR STRAP PER USAIR TYPICAL REPAIR 53-20-09A.(W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION FWD CARGO DOOR JAMB PAN.  CORROSION TASK NR C51-53300, PREVIOUSLY REWORKED.  REMOVED CORROSION AND SPLICED IN NEW SECTION OF PAN PER SRM 53-05 FIG 44.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT CARGO TIE DOWN RAIL STA 617 TO 655 LONGERON 28L.  CORROSION TASK C51-53300.  CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER REPAIR PER USAIR TYPICAL REPAIR 53-20-09 FIG 1.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION BETWEEN STA 1380 AND 1401 LONGERON 25R TO LONGERON 30 TAIL INTERIOR FLANGE.  CORROSION TASK C58-53301.  REMOVED CORROSION AND INSTALLED REPAIR ANGLE DOUBLERS PER SRM 53-01 FIG 2.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AROUND 2 HOLES IN FLOORBEAM RT LAV.  CORROSION TASK NR C58-53300.  REMOVED CORROSION AND INSTALLED FILLER, STRAP AND ANGLE REPAIR PER USAIR TYPICAL REPAIR 53-10-19.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION IN FLOORBEAM WEB AT STA 1338 RT O/B.  CORROSION TASK C58-53305.  CUT OUT CORRODED AREA AND INSTALLED WEB REPAIR PER SRM 53-05 FIG 79 SHT 1.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .5 INCH CRACK IN LOWER WINDOW PAN STA 902 RT SIDE.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND BURNISH MARK, GOUGED .18 INCH DEEP AT STA 945 LONGERON 9R IN SKIN.  INSTALLED DOUBLER INTERNAL REPAIR PER SRM 53-04 FIG 38.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND BELTFRAME CRACKED .75 INCH LONG AT STA 1332 LONGERON 17L.  REMOVED CRACKED SECTION OF BELTFRAME AND SPLICED PER SRM 53-03 FIG 32.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND SEAT TRACK AT STA 200 AND 248 RT O/B WORN BEYOND LIMITS PER SRM 53-05 FIG 4B.SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND CRACK 1.5 INCH LONG AT STA 210 AND LONGERON 15L IN DOOR JAMB MEMBRANE WEB.  CUT OUT DAMAGED WEB AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-01 FIG 2 SHT 4.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND CRACK .75 INCH AT STA 237 ON LONGERON 17R.  SPLICED IN NEW SECTION OF LONGERONPER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND SKIN DENTED AND DAMAGED BEYOND LIMITS BETWEEN STA 229 AND 246 LONGERONS 15L AND 18L.  CUT SKIN PANEL AND SPLICED IN NEW SECTION PER SRM 53-04 FIG 6 AND USAIR EA 30336.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .625 INCH CRACK STA 408 ON LONGERON 17R.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.25 INCH CRACK STA 1437 LT SIDE BELOW LONGERON 3L IN FUSELAGE SKIN.  CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-04 FIG 27.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH CRACK IN THE STA 1480 UPPER PYLON ATTACH ANGLE RT SIDE.  STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER TO ANGLE PER SRM 54-04 FIG 10 SHT 3.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.5 INCH CRACK AT STA 1463 LT SIDE VERTICAL STAB TO FUSELAGE ATTACH ANGLE.  CUT OUT CRACKED SECTION OF ANGLE, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-05 FIG 23A AND USAIR EA NR 19449.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK IN ANGLE AT STA 1338 TOP CENTER OF AFT PRESSURE BULKHEAD FWD SIDE.  STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 PG 9.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND HOLE CHAFED IN LONGERON 8R AT STA 1401 AND 1418.  CUT OUT CHAFED SECTION AND INSTALLED NEW SECTION OF LONGERON.  SPLICED PER USAIR TYPICAL REPAIR 53-10-17.  (W)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .3125 INCH CRACK STA 1380 LT SIDE ABOVE LONGERON 14L IN FUSELAGE SKIN.  CUT OUT AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 18.  (W)


REMARKS:
PHL - FLT 260 - AFTER TAKEOFF, THE RT AIR CONDITIONING PACK FAILED CAUSING THE AC TO LOSE PRESSURIZATION.  FLIGHT RETURNED TO PHL.  MAINTENANCE REPLACED THE RT AIR CONDITIONING SUPPLY PRESSURE INDICATOR SYSTEM.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
IND - FLT 977 - AT FL 350, THE RT HYDRAULIC PRESSURE LIGHT ILLUMINATED AND THE HYDRAULIC QUANTITY DROPPED TO ZERO.  THECAPTAIN DECLARED AN EMERGENCY AND LANDED IN IND.  MAINTENANCE REPLACED THE HYDRAULIC PUMP AND FILTERS.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
TPA/ATL - FLT 59 - IN-FLIGHT, LOST A-HYDRAULIC FLUID.  AIRCRAFT RETURNED TO TPA.  REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND FILTERS.  OPS CHECK AND RAN NR 1 ENGINE, CHECK OK PER MM 29-11-33.  REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP AND FILTERS, PRECAUTIONARY, AND OPS CHECK OK PER MM 29-11-33.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 2 EACH, .1250 INCH CRACKS IN FUSELAGE SKIN AT STA 89 NEAR RT NOSE GEAR DOOR.  INSTALLED MFG NEW SKIN REPAIR PER SRM 53-01, FIGURE 2, SHEET 3.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .1875 INCH CRACK IN FUSELAGE SKIN AT STA 100 AFT OF RT NOSE GEAR DOOR AFT HINGE.  INSTALLED MFG NEW SKIN AND INSTALLED REPAIR PER SRM 53-01, FIGURE 2, SHEET 3.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION FOUND .1250 INCH CRACK IN RIGHT NAV LONGERON 17R STA 965.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK AT VERTICAL STAB L.E. BOTTOM 7TH RIB.  INSTALLED NESTED DOUBLER REPAIR PER SRM 55-01.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LONGERON 4L AT STA 637.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK TOP C/L ANGLE ABOVE AFT PAX ENTRY DOOR ON FWD SIDE OF PRESSURE DOME, STA 996.  INSTALLED ANGLE AND DOUBLER REPAIR PER SRM 53-01, FIGURE 2.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 12 INCH CRACK IN STA 180 WEB 9923484-7.  CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER DAC DWG 9923484.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 2 CRACKS, .1250 INCH EACH, IN STA 207, LT SIDE TOP OF BOTTOM WINDOW BELT BEAM. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-03, FIGURE 36.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 2 INCH CRACK IN CUSP MEMBRANE, STA 617, LONGERON 18L.  MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LONGERON 4L, STA 160.  INSTALLED SPLICE REPAIR OF LONGERONPER SRM 53-02, FIGURE 2, VIEW BB.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND CORROSION, STA 237, FLOOR SUPPORT CENTER, LT SIDE.  FABRICATED NEW SUPPORT ANDSPLICED IN ANGLE REPAIR PER USAIR TYPICAL REPAIR 53-10-21A.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK IN FORWARD CARGO FLOOR SUPPORT CLIP, STA 598, LONGERON 27L.  MFG NEW CLIP AND INSTALLED PER SRM 53-01.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK IN CUSP MEMBRANE, STA 596, LONGERON 18R.  MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LEFT PYLON TOP ATTACH ANGLE AT STA 980.  CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 54-04, FIGURE 10.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION FOUND LEVEL 1 CORROSION AT GALLEY FLOOR PAN, STA 180 TO STA 205, RT SIDE, PREVIOUS REWORK.  REF:  CRCP TASK C46-53303.  INSTALLED NEW SECTION OF FLOOR SUB-PAN PER SRM 53-01.  (X)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND LEVEL 1 CORROSION CPCP TASK NR C58-53300, LT LAV THRESHOLD ANGLE, STA 983, PREVIOUS REWORK.  INSTALLED DOUBLER REPAIR PER SRM 53-01.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.75 INCH CRACK, STA 1287 - STA 1367, RT SIDE CUSP MEMBRANE.  CUT OUT SECTION OF CUSP MEMBRANE AND INSTALLED SPLICE REPAIR PER SRM 53-05, FIGURE 97.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH CRACK FWD UPPER CORNER OF M.E.D. IN FUSELAGE SKIN (X-RAY).  INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR PER SRM 53-05, FIGURE 25A AND USAIR, EA 30427.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .6250 INCH CRACK IN RT WING LEADING EDGE OUTBOARD OF VORTILON.  STOP DRILLED CRACK AND INSTALLED DOUBLER AND SUPPORT ANGLE REPAIR PER SRM 57-068, FIGURE 9.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND INTERCOSTAL AND DOUBLER MISDRILLED AT STA 886 AND STA 905, LONGERON 16L.  FABRICATED AND HEAT TREATED NEW SECTION OF INTERCOSTAL AND INSTALLED DOUBLERS PER SRM 53-01, SRM 51-10-2A.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACKS AT ATTACH POINTS IN LONGERON 17L AT STA 237, 256, 275, 294, 313, 332, 370, AND 427.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2A.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN UPPER FWD CORNER OF WINDOW PAN AT STA 946 LT.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-30-06.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK UPPER FORWARD CORNER STA 886, LT WINDOW PAN.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN WINDOW PAN STA 929 UPPER FWD CORNER RT.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN WINDOW PAN UPPER FWD CORNER AT STA 888 RT.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06.  (X)


REMARKS:
CLE - THE FORWARD CEILING EMERGENCY LIGHTS WOULD NOT SHUT OFF.  MAINTENANCE REPLACED THE POWER SUPPLY.  OPERATIONS CHECKED GOOD.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 2.50 INCH CRACK STA 1268 - STA 1307, LT SIDE CUSP MEMBRANE.  CUT OUT SECTION OF CUSP MEMBRANE AND SPLICED IN REPAIR PER SRM 53-05, FIGURE 97.  (X)


REMARKS:
MCO - FLT NR 1136 - UPON TAXIING FOR DEPARTURE, THE LEFT BRAKE SEIZED.  SUBSEQUENTLY, THE NR 1 TIRE WENT FLAT.  CAPTAINDECIDED TO RETURN TO THE GATE.  MAINTENANCE REPLACED THE NR 1 BRAKE ASSEMBLY, AND THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES P/N 32935.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
EMERGENCY FLOOD LIGHTS OVER FORWARD FLIGHT ATTENDANT SEAT TO ILLUMINATED SLIDES AND RI LIGHT STAYS ON.  PLACED EMERGENCY EXTERIOR LIGHTS ON MEL 33.20.


REMARKS:
FLT 120 - TPA-ATL - ON APPROACH TO ATL DID NOT HAVE GEAR WARNING HORN.  FOUND CANNON PLUG LOOSE ON NOSE GEAR UPLOCK SWITCH.  CLEANED CANNON PLUG AND SECURED.  ALL GEAR LIGHTS OPERATE NORMALLY IAW MM 32-60.


REMARKS:
FLT NR 591 - ATL-MIA - RETURNED TO ATL BECAUSE THE AIRCRAFT WOULD NOT PRESSURIZE.  RESECURED THE E/E DOOR.  (M)


REMARKS:
BWI - FLT 0589 - ON TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT.  FLIGHT RETURNED TO BWI.  MAINTENANCE REPLACED THE ASSIST SPRING.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
FLT NR 134 - FLL-ATL - AFTER TAKEOFF THE FLIGHT CREW NOTICED THE OIL QUANTITY DROP TO 4 QTS.  THEY RETURNED TO FLL.  MAINTENANCE FOUND A LOOSE OIL CAP.  RESERVICED AND SECURED THE CAP, THE FLIGHT PROCEEDED WITHOUT FURTHER DELAY.  (M)


REMARKS:
IN ATL, EMERGENCY LIGHTING SYSTEM WOULD NOT COME ON WITH FLIGHT DECK SWITCH.  MAINTENANCE FOUND WIRE SHORTED ON SWITCH ASSY.  REPAIRED WIRE PER MM 33.


REMARKS:
FLT NR 481 - IAD-MCO - AT TAKEOFF FLT CREW NOTICED E/E DOOR LIGHT CAME ON.  CREW RETURNED TO IAD.  MAINTENANCE SECURED DOOR LATCH AND DISPATCHED FOR CONTINUED SERVICE.


REMARKS:
FLT 190 - ATL-FLL - AIR RETURN TO ATL DUE TO THE PRIMARY AND SECONDARY TRIM INOP IN NOSE DOWN POSITION.  CLEANED STUDS NR 1503 AND 1511 PRIMARY TRIM RELAY TERMINALS.  OPS CHECK GOOD PER MM 27-00.  PRIMARY AND SECONDARY TRIM CHECK GOOD.


REMARKS:
STL - FLT 246 - AFTER TAKEOFF, LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION.  FOUND NOSE LANDING GEAR OLEO STICKING IN THE COMPRESSED POSITION.  REPLACED NOSE LANDING GEAR SEALS, MFG KIT P/N A03772REVH.  NOSE GEAR OPERATION CHECKED NORMAL.  CHECK C - 6-30-94 - STL.


REMARKS:
STL - DURING OP-15, FOUND .1250 INCH CRACK IN LONGERON 29R, STA 218.  REPAIRED BY REPLACING LONGERON PER SRM 51-10-0, PAGES 1 AND 2, AND STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  66,307 HOURS; 81,239 CYCLES.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A ONE-INCH CRACK IN AFT CARGO BIN BOTTOM AT AFT CORNER OF DOOR OPENING, WHICH WAS ALSO BENT, STA 750.  REPAIRED PER EMLR 65708.  AIRCRAFT TOTAL TIME:  60,441 HOURS; 77,859 CYCLES.


REMARKS:
ATL - FLT 166 - SMOKE IN COCKPIT ON APPROACH TO ATL.  FOUND TO BE FORWARD GALLEY COFFEE MAKER OVERHEATING.  REMOVED COFFEE MAKER AND PLACED ON MEL.


REMARKS:
ATL/IAD - FLT 454 - WHEN ON FINAL APPROACH, DECLARED AN EMERGENCY DUE TO THE VOLT/AMP METER HAVING AN ELECTRICAL FAULT AND SMOKING ON THE FLIGHT DECK.  REPLACED VOLT/AMP METER.


REMARKS:
DAB - FLT 1202 - LEFT ENGINE LOST POWER CLIMBING THROUGH 15,000 FEET.  FLIGHT CREW ACCOMPLISHED ENGINE SHUT DOWN AND RETURNED TO DAB WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT ENGINE.  (X)


REMARKS:
EN ROUTE TO MDW, EXPERIENCED B-SYSTEM PRESSURE DROP.  AIRCRAFT DIVERTED TO IND AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND PRESSURE INDICATOR INOP, DEFERRED INDICATOR AND CONTINUED PER MEL 29-3.


REMARKS:
AFTER TAKEOFF, EXPERIENCED APU FIRE WARNING.  CREW ACTIVATED APU FIRE BOTTLE, FIRE WARNING LIGHT EXTINGUISHED.  AIRCRAFT RETURNED TO LBB AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION.  REPLACED FIRE CONTROL PANEL AND FIRE DETECTION UNIT PER BOEING M/M.


REMARKS:
WHILE TAXIING, CREW NOTED A BRAKE DRAGGING SENSATION, AIRCRAFT RETURNED TO GATE.  INSPECTED AND FOUND DAMAGE TO LEFT MAIN GEAR AXLE AND NUMBER 1 WHEEL AND BRAKE ASSEMBLY.  REPLACED LEFT MAIN GEAR INNER CYLINDER, NUMBER 1 AND 2 WHEEL/BRAKE ASSEMBLIES AND ANTI-SKID TRANSDUCERS PER BOEING M/M.


REMARKS:
DURING DESCENT INTO ELP, EXPERIENCED NUMBER 1 ENGINE FAILURE.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT ELP.  INSPECTED AND FOUND NUMBER 1 ENGINE TOWER SHAFT FAILURE.  REMOVED AND REPLACED ENGINE ASSEMBLY PER BOEING M/M.


REMARKS:
ON TAKEOFF FROM LBB, NUMBER 3 MAIN GEAR WHEEL ASSEMBLY SEPARATED FROM BRAKE ASSEMBLY.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT ABQ.  INSPECTED AND FOUND THE REASON FOR SEPARATION WAS DUE TO FAILED WHEEL BEARING.  REPLACED NUMBER 3 AND 4 MAIN GEAR WHEEL ASSEMBLIES, NUMBER 3 BRAKE ASSEMBLY AND ANTI-SKID TRANSDUCER PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500 PLUS 6, STRINGER 23R AT BS 860 STRINGER 26L BETWEEN BS 909 AND 916 STRINGER 24R AND AT BS 330 STRINGER 25L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500D, S19R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR AFT FRAME CRACKED AT BS 492 RBL 39 WL 162.  REPAIRED PER TRAMCO EWO 95-0497 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CHAFING DAMAGE FROM  BS 867 TO 887 BETWEEN S2 LT AND RT.  REPAIRED PER TRAMCO EWO 95-0497 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 316 BELOW S17L AND AT BS 332 BETWEEN S19 AND 20L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 1016 LBL 5 WL 208 AND AT BS 294 AT LBL12 WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 3 SLAT LOWER T/E SKIN CRACKED AT I/B END.  REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 178 WL 189 BL 0.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 95-0494.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND NOSE WHEEL WELL CEILING PANEL OPENING CRACKED 2.125 AT AFT INBOARD RADIUS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO DOOR FWD AND AFT LOWER FRAME WEBS DAMAGED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312 LBL 14.  REPAIRED PER SWA RA 1-553-1327 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947 LBL 10 AND 5 AT BS 986.5 LBL 15 AND RBL 6.  REPAIRED PER SWA RA 1-553-1329 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND A/C RAM AIR INLET WEB T-CHORD CRACKED JUST BELOW UPPER DRAG ANGLE AT BS 539.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND CRACK IN UPPER FWD CORNER OF FWD ENTRY DOOR LOWER CAM PLATE SUPPORT CASTING.  REPAIREDPER SWA RA 1-353-1331 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED B/C CHECK, FOUND RIGHT O/B FLOORBEAM STRAP AT FWD END OF E AND E COMPT BROKEN.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5 RBL 42 AND 45.  REPAIRED PER SWA RA 1-553-1325  ANDBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727 RBL 3.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
ICT - FLT 65 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 1206, DUE TO HIGH OIL PRESSURE AND INCREASING OIL TEMPERATURE.REPLACED ENGINE OIL FILTER AND ENGINE OIL PRESSURE RELIEF VALVE.  ENGINE OPERATION AND LEAK CHECK NORMAL.  ENGINE TOTALTIME:  21,726 HOURS; 10,984 CYCLES.  OP-16 - 8-17-94 - MCI.


REMARKS:
JFK - FLT 903 - DURING CRUISE, SHUT DOWN NR 3 ENGINE, SN 4285, DUE TO OIL LOSS, FOUND VENT LINE TO OIL PRESSURE TRANSMITTER LEAKING.  REPLACED VENT LINE, MFG PN 65B90115-169.  ENGINE OPERATION AND LEAK CHECK WAS NORMAL.  ENGINE TOTAL TIME 65,051 HOURS AND 13,468 CYCLES.  CHECK C2 - 1-29-95 - MCI.


REMARKS:
STL  - FLT 340 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 2143, DUE TO ENGINE SURGED AND THROTTLE WOULD NOT CONTROL ENGINE POWER.  REPLACED ENGINE FUEL PUMP, MFG PN 378200 AND FUEL CONTROL.  MFG PN 743602-4.  ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME 39,260 HOURS AND 41,358 CYCLES.  CHECK C - 3-1-95 - STL.  REFERENCE CONTROL NR 95ZZZX4259.


REMARKS:
STL - FLT 720 - DURING TAKEOFF, SHUT DOWN NR 1 ENGINE, SN 4173, DUE TO UNCOMMANDED THRUST LEVER MOVEMENT TO IDLE AND REVERSER OPERATING LIGHT ILLUMINATION FOR FIVE SECONDS.  CHECKED ENGINE CONTROL SYSTEM AND OPERATION WAS NORMAL.  DEACTIVATED THRUST REVERSER PER MEDP.  ENGINE TOTAL TIME:  77,759 HOURS; 13,914 CYCLES.  CHECK C-3 - 10-29-94 - JFK.


REMARKS:
SYR - FLT 1518 - EN ROUTE BTV TO PIT, NR 2 ENGINE FLAMED OUT DURING FUEL CROSSFEED, RIGHT PUMPS OFF, LEFT PUMPS ON, CROSSFEED OPEN.  FLIGHT CREW ACCOMPLISHED INFLIGHT RESTART AND DIVERTED TO SYR.  SINGLE ENGINE TIME WAS 7 MINUTES.  MAINTENANCE REPLACED AUX FUEL CONTROL UNIT, NR 2 ENGINE MEC AND FUEL PUMP.  ACCOMPLISHED FUEL SYSTEM VACUUM FEED TEST.  OPS CHECKED GOOD.  (M)


REMARKS:
PHL - FLT 385 - HIGH OIL TEMPERATURE ON TAKEOFF FROM PHL.  CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO PHL WHERE LANDINGWAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE OIL TEMPERATURE TRANSMITTER.  (M)


REMARKS:
SAN - FLT 1412 - ON CLIMB-OUT, SQUEAL WAS HEARD OUT OF THE L1 DOOR.  AT FL 330 IN CRUISE, CABIN PRESSURE BEGAN TO CLIMB.  FLIGHT RETURNED TO SAN WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED FORWARD ENTRY DOOR TOP HINGECOVER.  (M)


REMARKS:
FLT NR 10, MCO-EWR - AFTER TAKEOFF PASSING 10,000 FEET, LOWER AFT BDY OVERHEAT, NR 1 WING ANTI-ICE VALVE LIGHTS CAME ON, STANDBY LIGHTS ILLUMINATED.  NR 1 WING BLEED VALVE, NR 1 PK VALVE AND LE VALVE CIRCUIT BREAKERS POPPED.  NR 1 ENGINE SHUT DOWN PRECAUTIONARY.  AIRCRAFT RETURNED TO MCO.  REMOVED AND REPLACED BLOWN 13TH STAGE DUCT AND WING ANTI-ICE VALVE FROM NR 1 ENGINE, LEAK CHECK OK AS PER MM 30-10-00.  FOUND WIRES, C/P'S DAMAGED TO FLW CONT MODULE S/O VALVES TO STANDBY PUMP AND TAI FOR WING SENSOR OUT NR 1 ENGINE REWIRED AND INSTALLED NEW C/P'S ON VALVES, PUMP SENSOR.  OPS CHECK AND INSPECTED OK AS PER MM 72-10-01.  (M)


REMARKS:
FLT NR 286 - ATL-MCO - UPON LANDING GEAR EXTENSION ON APPROACH TO MCO THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED.  FLIGHT CREW AND ATC CONFIRMED GEAR EXTENSION AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS.  MAINTENANCE FOUND LOOSECANNON PLUG ON DOWNLOCK SWITCH.  RESECURED AND CLEARED OPERATIONAL CHECKS OK.


REMARKS:
PHX - DURING CRUISE, AFT GALLEY FORWARD OVEN EMITTED SMOKE.  SHUT OFF OVEN, SMOKE DISSIPATED.  FOUND CHARRED PAPER FROMFOOD CONTAINER.  CLEANED OVEN AND OPERATION CHECK NORMAL.


REMARKS:
DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4806, DUE TO OIL FILTER DIFFERENTIAL PRESSURE LIGHT ILLUMINATION.  FOUND CARBON IN OIL FILTER.  REPLACED OIL FILTER, DRAINED AND REPLENISHED ENGINE OIL.  ENGINE OIL FILTER DIFFERENTIAL PRESSURE SYSTEM CHECKED NORMAL.  ENGINE TOTAL TIME 49,276, TOTAL CYCLES 16,099.


REMARKS:
DURING DESCENT SHUT DOWN RIGHT ENGINE, S/N 1605, DUE TO ENGINE DID NOT REDUCE TO IDLE WHEN THRUST LEVER WAS MOVED TO IDLE POSITION.  FOUND FUEL CONTROL HAD INTERNAL MALFUNCTION.  REPLACED FUEL CONTROL, MFG P/N 743602-5.  ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME 27,452, TOTAL CYCLES 23,975.


REMARKS:
DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4144, DUE TO OIL PRESSURE FLUCTUATION AND LOW OIL QUANTITY.  FOUND OIL PRESSURE TRANSMITTER, MFG P/N 35674403-3001, CRACKED.  REPLACED OIL PRESSURE TRANSMITTER.  ENGINE LEAK CHECKED AND OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME 70,948, TOTAL CYCLES 13,869.


REMARKS:
DURING HOLDING PATTERN RIGHT ENGINE DID NOT RESPOND TO THROTTLE AND ENGINE ROLLED BACK TO IDLE. TURNED OFF EEC.  CHECKED ENGINE OPERATION AND ADJUSTED ENGINE IDLE.  ENGINE OPERATION CHECKED NORMAL.


REMARKS:
DURING CRUISE, FOOD CART S/N 3212, HAD ELECTRICAL MALFUNCTION AND EMITTED STRONG FUMES.  DISCONNECTED FOOD CART.  REPLACED FOOD CART, MFG P/N 88801-1, CHECKED GALLEY ELECTRICAL, AND OPERATION WAS NORMAL.


REMARKS:
CLT - FLT 0249 - RETURN TO FIELD DUE TO AN INOPERATIVE WEATHER RADAR.  MAINTENANCE REPLACED THE RADAR R/T.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 18 INCHES TOTAL AREA OF SURFACE CORROSION FLOOR BEAM STATION 986.5 AT RBL 5 TO LBL 45.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  CUT OUT UPPER FLANGE OF ENTIRE LENGTH OF FLOOR BEAM AND INSTALLED NEW T-CAP.  NOT MORE THAN ONE POUND ADDED WT FOR REPAIR.  REPAIRED PER EA 39521.(M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 727 TO BS 787 ABOVE S-26 R ON TRANSITION ANGLE.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  SPLICED IN NEW SECTION OF TRANSITION ANGLE.  REPAIRED PER SRM 53-60-53.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED AREA, BS 949, RBL 16 ON INTERCOSTAL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REMOVED AND REPLACED CORRODED INTERCOSTAL WITH NEW IDENTICAL PART.  REPAIREDPER SRM 51-10-2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 344 BL 0 TO LBL 10 ON FLOOR BEAM.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. CUTOFF TOP OF FLOOR BEAM AND INSTALLED NEW 'T' CAP.  REPAIRED PER TR 53-10-03.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION LB 11 BS 328 TO BS 344 ON INTERCOSTAL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPAIRED PER SERM 51-10-2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 6 FOOT CORROSION BS 867 TO BS 947.5 ON TRANSITION ANGLE.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  REPLACED TRANSITION ANGLE, REPAIRED PER SRM 51-10-2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH SQUARE TOTAL AREA, BETWEEN BS 967-987 RBL 16 ON INTERCOSTAL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-03.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 955 TO 995 LBL 50 ON Z-ANGLE.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPLACED Z-ANGLE, REPAIRED PER SRM 51-10-02.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 5 INCH TOTAL AREA OF SURFACE CORROSION STATION 947 TO 967, LBL 16 ON INTERCOSTAL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REMOVED DEFECTIVE PART AND INSTALLED NEW.  REPAIRED PER SRM 51-10-02.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 40 INCH AREA OF SURFACE CORROSION FORWARD SERVICE DOORSILL 'Z' ANGLE.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REMOVED CORRODED 'Z' ANGLE REPLACED 'Z' ANGLE.  REPAIRED PER SRM 51-10-2.  (M)


REMARKS:
MCO - FLT NR 0119 - AIRCRAFT DIVERTED DUE TO THE CENTER TANK FUEL PUMP FAILING.  MAINTENANCE REPLACED THE CENTER BOOST PUMP AND RIGHT PRESSURE SWITCH.  OPERATIONS CHECKED NORMAL.  (M)


REMARKS:
CLE - INTERIOR OVERWING EMERGENCY EXIT LIGHTS WOULD NOT TEST.  MAINTENANCE REPLACED BATTERY PACK AND CHARGER ASSEMBLY.(M)


REMARKS:
LGA - FLT 2235 - THE 'NOSE GEAR UNSAFE' LIGHT ILLUMINATED WHEN THE POWER WAS BROUGHT TO IDLE.  VISUALLY VERIFIED GEAR POSITION AND PERFORMED TOWER FLYBY.  FLIGHT CREW FOUND AIR/GRD RELAY AND LANDING GEAR LIGHTS CIRCUIT BREAKER POPPED.  RESET CIRCUIT BREAKER.  INDICATION WAS NORMAL.  LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LANDING GEAR CIRCUIT BREAKER.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
SFO - FLT NR 1426 - CREW RECEIVED AN OIL FILTER BYPASS LIGHT ON THE NR 2 ENGINE.  THE CAPTAIN PULLED THE RIGHT ENGINE BACK TO IDLE WITH NO RESULT.  FLIGHT CREW SHUTDOWN THE NR 2 ENGINE AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND THE FORWARD SCAVENGE MCD SCREEN CLOGGED.  THE SCREEN WAS CLEANED.  THE MAIN ENGINE OIL PRESSURE AND SCAVENGE FILTERS WERE REPLACED.  OPERATIONS AND LEAK CHECKED GOOD.  (M)


REMARKS:
BOS - FLT NR 0284 - ON TAKEOFF, THE MASTER CAUTION LIGHT ILLUMINATED.  THE HYDRAULIC SYSTEM 'A' PRESSURE WAS FLUCTUATING ABOVE ZERO, AND THE HYDRAULIC SYSTEM 'A' QUANTITY REACHED ZERO.  FLIGHT RETURNED TO BOS.  MAINTENANCE REPLACED THE NR 6 SPOILER ACTUATOR DUE TO LEAKAGE.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
CLT - FLT 0549 - THE CAPTAIN REPORTED PRESSURIZATION FAILURE.  THE FLIGHT RETURNED TO CLT.  MAINTENANCE PRESSURIZED THEAIRCRAFT TO 6 PSID.  NO LEAKS WERE NOTED.  THE PRESSURIZATION CONTROLLER WAS REPLACED AS A PRECAUTION.  (M)


REMARKS:
MSP - FLT 0232 - THE LEFT LANDING GEAR DOOR DID NOT LOCK UPON GEAR RETRACTION.  THE GEAR WAS CYCLED TWICE BUT THE LIGHTWOULD NOT EXTINGUISH.  MAINTENANCE INSTALLED A NEW DOOR LOCK ON THE LEFT GEAR DOOR.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
CLT - FLT 1409 - FLIGHT EXPERIENCED RADAR FAILURE DURING CLIMB-OUT.  THE FLIGHT RETURNED TO CLT.  MAINTENANCE REPLACED THE RADAR R/T.  OPERATIONS CHECKED NORMAL.  (M)


REMARKS:
BOS - THE EMERGENCY FLOOR LIGHTING FAILED.  MAINTENANCE RELAMPED SEVERAL LIGHTS AND REPLACED TWO BATTERY PACKS.  OPERATIONS TESTED GOOD.  (M)


REMARKS:
LAX - FLT 0412 - AT 23,000 FEET, THE LEFT HYDRAULIC QUANTITY LIGHT ILLUMINATED.  THE CAPTAIN DECLARED AN EQUIPMENT EMERGENCY WHEN IN RANGE OF LAX.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE DOWNLOCK ACTUATOR PRESSURE LINE ON THE RIGHT GEAR.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
DCA - FLT 0450 - THE CREW HAD DECLARED AND EMERGENCY DUE TO A LE FLAP ASYMMETRY PROBLEM.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORROSION ON STRAP AT BS 860.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  REPLACED STRAP, REPAIRED PER SRM 51-10-2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL, FOUND CORROSION 1 INCH TOTAL AREA BETWEEN BS 967-987 LBL 16 ON INTERCOSTAL.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-3.  (M)


REMARKS:
DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION.  ALL INDICATIONS WERE NORMAL.  FLIGHT RETURNED TO DCA.  MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK.  OPERATIONS CHECKED GOOD.  REF USAA950617, 95ZZZW809, 95ZZZW810.


REMARKS:
DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION.  ALL INDICATIONS WERE NORMAL.  FLIGHT RETURNED TO DCA.  MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK.  OPERATIONS CHECKED GOOD.  REF USAA950617, 95ZZZW808, 95ZZZW810.


REMARKS:
DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION.  ALL INDICATIONS WERE NORMAL.  FLIGHT RETURNED TO DCA.  MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK.  OPERATIONS CHECKED GOOD.  REF USAA950617, 95ZZZW808, 95ZZZW809.


REMARKS:
MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY.  THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT.  MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULICSYSTEM RETURN LINE FILTER.  OPERATIONS CHECKED GOOD.  REF USAA950649, 95ZZZW812, 95ZZZW813.


REMARKS:
MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY.  THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT.  MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULICSYSTEM RETURN LINE FILTER.  OPERATIONS CHECKED GOOD.  REF USAA950649, 95ZZZW811, 95ZZZW813.


REMARKS:
MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY.  THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT.  MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULICSYSTEM RETURN LINE FILTER.  OPERATIONS CHECKED GOOD.  REF USAA950649, 95ZZZW811, 95ZZZW12.


REMARKS:
DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION.  ALL INDICATIONS WERE NORMAL.  FLIGHT RETURNED TO DCA.  MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK.  OPERATIONS CHECKED GOOD.  REF 95ZZZW808, 95ZZZW809, 95ZZZW810.


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND .5 INCH CRACK AND BUCKLING AT 965 RT BULKHEAD BETWEEN LONGERON 17R AND 18R FLOOR LEVEL.  SPLICED IN NEW WEB SECTION FROM LONGERON 18R TO 17R PER SRM 53-03 FIG 19 AND USAIR EA 30491.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND GOUGED OUT OF LIMITS AT STA 208 FROM LONGERON 1L TO AND BETWEEN LONGERON 1R ANDLONGERON 2R.  BURNISHED AREA AND INSTALLED TWO DOUBLERS PER SRM 53-04 FIG 38 NR 4 EFG.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND 1.5 INCH BY .050 DEEP CHAFE AFT FACE OF BEAM OF RT WING SHELF INBED OF THE SERVICE INTERPHONE JACK IN RT MLG WW.  ROUTED OUT DAMAGED AREA AND INSTALLED A DOUBLER REPAIR PER SRM 53-01.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA OUT OF LIMITS ON BELTFRAME STA 1076 LONG 14L.  CUT OUT DAMAGED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-03 FIG 2A.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY 10 INCH DENT FWD CARGO DOOR EXTERIOR SKIN UNDER DOOR HANDLE.  INSTALLED DOUBLER REPAIR PER SRM 52-05 FIG 30.  (W)


REMARKS:
PIT - DURING Q-t/CX-5 INSPECTION, FOUND 2 , 20 INCH BY 6 INCH BY .375 INCH DEEP DENTS AND 1.5 INCH CRACK BETWEEN STA 256 TO 294 AND LONGERON 20R AND 21R APPROX STA 280.  CUT OUT DAMAGED AREA AND INSTALLED FILLER DOUBLER AND TAPERED SHIMS PER USAIR EA NR 30552.  (W)


REMARKS:
MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY.  THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT.  MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULICSYSTEM RETURN LINE FILTER.  OPERATIONS CHECKED GOOD.  REF 95ZZZW811, 95ZZZW812, 95ZZZW813.


REMARKS:
BDL - THE TAIL CONE WAS INADVERTENTLY RELEASED.  THE EVACUATION SLIDE FAILED TO DEPLOY.  MAINTENANCE REINSTALLED THE TAIL CONE AND PERFORMED AN ADJUSTMENT TEST,  NO DEFECTS NOTED.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION AT GALLEY NR 2 FLOOR SUPPORT FROM CENTER LINE TO I/B SEAT TRACK RT AT STA 200, PREVIOUS REWORK.  CPCP TASK NR C46-53303.  FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE SECTION PER SRM 53-11.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND 1 INCH BY 4 INCH AREA OF LEVEL 1 CORROSION IN FLOOR SUPPORT STA 200, RUNNNG FROM CENTER LINE LT TO O/B SEAT TRACK, AREA PREVIOUSLY REWORKED.  CPCP TASK NR C46-53303.  FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE PER SRM 53-11.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION 2 INCH BY 14 INCH AREA STA 200 TO 235, LT OF CENTER LINE IN FLOOR SUPPORT ANGLE, AREA PREVIOUSLY REWORKED.  CPCP TASK NR C46-53303.  FABRICATED AND INSTALLED NEW SECTION OF FLOOR SUPPORT ANGLE PER SRM 53-11.  (W)


REMARKS:
PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION AT STA 160 TO 218 CENTER LINE OF A/C, AREA PREVIOUSLY REWORKED.  CPCP TASK NR C46-53303.  FABRICATED AND INSTALLED NEW SECTION OF FLOOR SUPPORT ANGLE PER SRM 53-11.  (W)


REMARKS:
IAD - THE AFT TAILCONE WAS INADVERTENTLY DEPLOYED.  THE TAILCONE DID NOT FALL AWAY ENOUGH TO PULL THE ESCAPE SLIDE OUT OF THE PACK TO DEPLOY.  MAINTENANCE REPAIRED THE DAMAGED CONE TIP AND REINSTALLED THE TAILCONE.  (W)


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND MAIN ENTRY AND SERVICE DOORS OUTSIDE EMERGENCY EXIT LIGHTS WEAK.  REPLACED BATTERY PACK PER BOEING M/M.


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


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP.  REPLACED POWER SUPPLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FWD EXTERIOR EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY CHARGER PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND ALL EMERGENCY EXIT LIGHTS INOP.  REPLACED FWD FLOOR TRACK BATTERY HOUSING,  AFT FLOOR TRACK BATTERY PACK, AFT SERVICE DOOR PORTABLE LIGHT ASSEMBLY, RELAMPED FLOOR TRACK LIGHTS AND EXIT SIGNS PER BOEINGM/M.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKS AT BS 178 BULKHEAD WEB AT LBL 5.7 AND RBL 5.7, ALONG SIDE I/B ROW OF FASTENER HOLES BETWEEN WL 207 AND 218.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR POSITION LEVER PAST THE OFF POSITION TO RETRACT GEAR.  AIRCRAFT RETURNED TO MCI AND MADE AN UNEVENTFUL LANDING.  AIRCRAFT WAS MX FERRIED TO MDW WHERE THEY RIGGED THE GROUND SHIFT CABLE AND REPLACED THE LANDING GEAR ACCESSORY UNIT.


REMARKS:
DURING CLIMBOUT, CREW EXPERIENCED APU FIRE WARNING AND THE APU WAS OFF.  FIRE BOTTLE WAS ACTIVATED AND THE FIRE WARNINGLIGHT REMAINED ILLUMINATED.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND NOTED NO EVIDENCE OF FIRE OR OVERHEAT CONDITION.  REPLACED APU FIRE DETECTION LOOP M717 AND FIRE BOTTLE PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, LANDING GEAR POSITION LEVER WOULD NOT MOVE PAST OFF POSITION.  GEAR POSITION INDICATED GEAR DOWN AND LOCKED.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  MAINTENANCE FERRIED AIRCRAFT TO PHX.  REPLACED GROUND SHIFT SENSOR AND PC LOGIC CARD PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND 3 SKIN CRACK ALONG S25L AT BS 720.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FLOORBEAM STRAP CRACKED AT BS 344, JUST O/B AND ABOVE BATTERY.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
STL - DURING LANDING, SMOKE APPEARED IN COCKPIT.  FOUND AUTO GROUND SPOILER ACTUATOR, MFG P/N 1040T100-5, HAD OVERHEATED CAUSING SMOKE.  REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL.  (M)


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE TAIL INTERIOR FS 1076 LONGERON 2L HAS CRACKS ON SHIM ATTACH RIB.  FABRICATED AND INSTALLED REPAIR PLATE, ANGLE AND BRACKET FOR LONGERON 2L AT FS 1076 IAW DC9 SRM 53-03 FIG4 N/R NR 027A1/0125.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, PASSENGER DOOR UPPER DOOR JAMB AT FS 180-200 AT LONGERON 6-10 LT.  REPAIR IS NON CONFORMING.  REMOVED OLD REPAIR AND DAMAGE.  FABRICATED AND INSTALLED NEW REPAIRS IAW DC9 SRM 51-10-4 AND 53-05.  N/R NR 027A1/0120.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE PASSENGER DOOR JAMB, FS 160-168 LONGERON 7-9 REPAIRIS NOT CLASS 1.  REMOVED REPAIR, FABRICATED AND INSTALLED NEW REPAIR IAW DC9 SRM 53-05-25A 7 51-10-4.  N/R NR 027A1/0122.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FS 775-794 LONGERON 29L TO 29R DOES NOT MEET REQUIREMENTS OF CLASS A REPAIR.  REMOVED OLD REPAIR AND DAMAGE, FABRICATED AND INSTALLED NEW REPAIRS IAW DC9 SRM 53-04 FIG 12B.  N/R NR 027A1/-124.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE AFT CARGO COMPARTMENT FS 965 AT LONGERON 29R HAS CORROSION ON ATTACH ANGLE.  REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR MEMBERS FOR THE LONGERON, 1 EA SEGMENT, SPLICES AND FILLERS IAW DC9 SRM 53-02 AND 53-03.  N/R NR 027A1/0063.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE KEEL BEAM FITTING AT FS 756 WAS CRACKED IN THE LEFTWW.  REMOVED AND REPLACED THE FITTING IAW DC9 SRM 51-30-2 AND 51-30-1.  N/R NR 027N1/0668.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME BETWEEN LONGERON 28L AND 28R WAS FOUND CORRODED AT FS 522 AND 541.  FABRICATED AND INSTALLED FRAME REPAIRS IAW DC9 SRM 53-03, 51-10-2A AND 51-10-3.  N/R NR 027N1/0447 AND 0448.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE SKIN AT FS 1025 AND LONGERON 23L IS CORRODED.  FABRICATED AND INSTALLED SKIN REPAIRS IAW DC9 SRM 53-10-1, 53-01, 51-10-3 AND 51-30-2.  N/R NR 027N1/0421.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE CENTER WING KEEL AREA HAS EXTENSIVE CORROSION DAMAGE ON THE RT SIDE.  FABRICATED AND INSTALLED REPAIRS FOR THE CENTER WING KEEL PANEL AND LONGERONS 29 LT AND RT IAW DC9 SRM 51-10-3, 51-30-0, 53-31-0 AND 51-10-2A.  N/R NR 027N1/-391.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE SKIN APPROXIMATELY 27 INCHES FORWARD OF THE MLG DOOR CUT OUT HAD CORROSION.  FABRICATED AND INSTALLED SKIN REPAIRS IAW DC9 SRM 51-10-6, 51-30-1 AND 53-05.  N/R NR027N1/0391.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE FRAME AT FS 851 AND FS 965 FROM LONGERONS 28L TO 28R HAVE CORROSION.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-3, 51-10-2A AND 53-03.  N/R NR'S 027N1/0314, 0315, 0316 AND 0317.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE EXTERNAL SKIN HAS PITTING CORROSION AT FASTENER HOLES ON LOWER KEEL SKINS AT FS 658 TO FS 775.  FABRICATED AND INSTALLED SKIN REPAIRS IAW DC9 SRM 51-10-3 AND 53-03.  N/R NR 027N1/0299.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD FRAME OF THE E/E DOOR HAS CORROSION WITH BULGES.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-3, 51-10-2, 51-10-2A AND AERO CORP EO 95-104 REV IR DATED 1/19/95.  N/R NR 027N1/0298.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 29R AT THE FORWARD CARGO DOOR AREA AND THE TORQUE BOX WAS FOUND WITH CORROSION.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 51-10-3, 51-10-4, 51-10-2A, AND 53-01.  N/R NR 027N1/0222.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE SKIN AT FS 125.8 AT LONGERON 19R WAS FOUNDWITH A CREASE.  FABRICATED AND INSTALLED SKIN REPAIRS IAW DC9 SRM 51-10-3, 51-30-2, 51-10-4 AND 53-01.  N/R NR 027N1/0213.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE LOWER ANGLE OF THE FLOOR BEAM IN THE AFT CARGO COMPARTMENT AT FS 965 AT LBL 28.  FABRICATED AND INSTALLED REPAIRS IAW AERO CORP EO 95-113 REV IR DATED 2/2/95 FAA FORM 8110-3 DATED 2/9/95.  N/R NR 027N1/0117.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD CARGO BAY LONGERON 30 WAS FOUND WITH 3 IMPROPER SPLICES WITH CORROSION AT FS 813, 889 AND 945.  FABRICATED AND INSTALLED 3 NEW SPLICES IAW DC9 SRM 53-02, 52-00.  N/R NR 027A1/-0169.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE FRAME AT FS 465 BETWEEN LONGERON 29R AND LONGERON 30 ON INTERCOSTALS AND GUSSET WAS FOUND TO BE CORRODED.  FABRICATED AND INSTALLED REPAIR ANGLES AND DOUBLERS FORTHE FRAME, GUSSETS, AND INTERCOSTALS IAW DC9 SRM 51-102, 53-03-02A, 51-10-2 AND 51-30-5.  N/R NR 027A1/0120.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE FRAME UPPER CHORD AT FS 446 BETWEEN LONGERON 25R AND LONGERON 30 WAS FOUND CRACKED.  STOP DRILLED CRACK.  FABRICATED AND INSTALLED A REPAIR ANGLE IAW DC9 SRM 51-10-3, 53-03-02A, 51-10-4, AND DPS 10.225 OF PARA F.  N/R NR 207A1/0119.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE UPPER CUSP AT THE R-1 DOOR ENTRY WAS FOUND TO BE EXTENSIVELY CORRODED AT FS 200.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-05, 51-10-3, 51-30-1, 51-20-0 AND MM20-30-1.  N/R NR 027N1/0658.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD CARGO COMPARTMENT FRAMES ARE CORRODED AT FS332 THROUGH 503 BETWEEN LONGERONS 28R AND 28L.  FABRICATED AND INSTALLED REPAIR MEMBERS AND DOUBLERS IAW DC9 SRM 53-03,51-10-2A, AND 51-10-3.  N/R NR'S 027N1/0449, 0450, 0451, 0452, 0454, 0455, AND 0456.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 23 AT FS 200 WAS FOUND CRACKED.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-02, 51-10-3 AND 51-30-2.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME SEGMENT AT FS 522 AT LONGERON 28L WAS FOUND WITH CORROSION.  FABRICATED AND INSTALLED A NEW FRAME SEGMENT IAW DC9 SRM 51-10-2A, 51-10-4, AND 53-10-1.  N/R NR 027N1/0632.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP INLAKE CITY, FLORIDA, THE VERTICAL STABILIZER L/E WAS FOUND WITH 5 CRACKED STIFFENERS.  FABRICATED AND INSTALLED NEW STIFFENERS IAW DC9 SRM 55-02 AND MM 51-00.  N/R NR027N1/0598.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND UNDER THE TEFLON STRIP ON THE UPPERFLOOR FRAMES AT FS 541.  FABRICATED AND INSTALLED FRAME REPAIRS IAW DC9 SRM 53-03-2A, 51-10-3, AND 51-10-2A.  N/R NR 027N1/0658.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND UNDER THE NUTPLATES ON THE FLOOR FRAME AT FS 1019 PRESSURE DOME.  FABRICATED AND INSTALLED PRESSURE DOME FLOOR FRAME REPAIRS IAW DC9 SRM 53-05 AND 51-10-3. N/R NR 027N1/0643.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME SEGMENT AT FS 560 AT LONGERON 28L WAS FOUND CORRODED.  FABRICATED AND INSTALLED A NEW FRAME SEGMENT IAW DC9 SRM 51-10-2A, 51-10-4 AND 53-10-1.  N/R NR 027N1/0633.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A 1 INCH CRACK WAS FOUND IN THE AFT CARGO DOOR FRAME.  STOP DRILLED CRACK.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 52-03, 51-10-4, AND 51-30-5.  N/R NR 027N1/0710.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .052 IN DEPTH DENT WAS FOUND IN THE FUSELAGE (PRESSURIZED) SKIN FS 275.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04 FIG 38.  N/R NR 027N1/0281.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .027 INCH DEPTH DENT WAS FOUND AT FS 332 BETWEEN LONGERONS 23L AND 24L.  REMOVED DAMAGED AREA.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04, 51-30-2 AND 51-10-4.  N/RNR 027N1/0131.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .023 INCH DEPTH DENT WAS FOUND AT FS 945 AND LONGERON26L.  REMOVED DAMAGED SECTION.  FABRICATED AND  INSTALLED (PRESSURIZED) SKIN REPAIRS IAW DC9 SRM 53-04 AND 51-30-2.  N/R NR 027N1/0127.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A LIFE LIMITED REPAIR WAS FOUND BETWEEN LONGERON 27L AND 28R AT FUSELAGE STATION 867 TO FS 900.5.  FABRICATED AD INSTALLED FUSELAGE (PRESSURIZED) SKIN REPAIRS IAW DC9 SRM 51-10-3 AND 53-04 AND AERO CORP EO 95-111 REV IR DATED 2/1/95 FAA FORM 8110-3 DATED 2/15/95.  N/R NR 027A1/0135.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CRACKS WERE FOUND PROGRESSED BEYOND THE STOP DRILL IN THE LOWER FRAME AT FS 870 ABOVE LONGERONS 29 LT AND RT AND 28R.  FABRICATED AND INSTALLED NEW LOWER FRAME IAW DC9 SRM 51-10-3, 53-03 AND 51-10-2A.  N/R NR 027N1/0383.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LOWER RIB AT FS 813 LONGERON 27L TO LONGERON 27R WAS FOUND CORRODED.  REMOVED CORROSION, FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-03, 51-10-2A AND 51-30-3.  N/R NR 027N1/0381.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE FRAME BETWEEN LONGERONS 24R AND 26R AT FS 218.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-2A, 53-03, 53-01, 51-10-4 AND 51-10-3.  N/R NR 027A1/0145.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, AT FUSELAGE STATION 80 ON THE LEFT SIDE, THE OUTER SKINWAS FOUND WITH AN APPROX .080 INCH DEPTH DENT WITH A .75 INCH CRACK.  GAINED ACCESS TO AREA.  REMOVED DAMAGED SECTION OF SECTION OF SKIN.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04.  N/R NR 027N1/0051


REMARKS:
WHILE PREPARING FOR INSTALLATION OF THE OVERHEAD BINS 2 LONGERONS WERE FOUND CRACKED AT FS 929 LONGERONS 6L AND 6R.  REMOVED AND REPLACED 1 FITTING AT FS 929 LONGERON 6 RT AND LT IAW DC9 SRM 53-01, 51-30-4 AD 51-10-3.  N/R NR 027N1/0171.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE AFT CARGO DOOR (INTERNAL) THROUGH FORWARD HOLE ON THE OUTER SKIN THE BRACKET WAS FOUND CRACKED.  REMOVED AFT CARGO DOOR AND FITTING.  ALIGNED NEW FITTING AND INSTALLED IAWDC9 SRM 51-00 AD MM 52-00.  REINSTALLED DOOR IAW MM 52-31-0.  N/R NR 027N1/0118.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE BELLY SKIN AT FS 550 AT CENTER BOTTOM WAS FOUND WITH A 2 INCH BULGE BETWEEN RIVETS.  GAINED ACCESS TO AREA.  CORROSION WAS FOUND ON LONGERON AND SKIN.  REMOVED DAMAGED AREAS FROM SKIN AND LONGERON.  FABRICATED AND INSTALLED REPAIRS FOR SKIN AND LONGERON IAW DC9 SRM 53-02, 51-10-6, AND 53-04.  N/R NR 027N1/0041.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE NR 1 ENGINE C-1 DISK CASE WAS FOUND WITH A CRACK INTHE FLANGE ON THE AFT SIDE AT THE NOSE COWL ANTI-ICE SHUT OFF VALVE MOUNT BRACKET.  REMOVED AND REPLACED THE C-1 DISK, IAW PWA AND AERO THRUST WORK SPECS EXIT FAN STATORS 1 SET, WORK BY AERO THRUST MECH FAA REPAIR STATION NR RG2R134L.  N/RNR 027N1/0091.


REMARKS:
ONT - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND.  CYCLED LANDING GEAR AND NOSE GEAR EXTENDED.  FOUND NOSE LANDING GEAR TRANSFER CYLINDER, MFG P/N 69-14106-5, WITH INTERNAL MALFUNCTIONS. REPLACED TRANSFER CYLINDER AND NOSE LANDING GEAR OPERATION CHECKED NORMAL.  (M)


REMARKS:
STL - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO HIGH AVM AND N2 OVERSPEED.  REPLACED NR 2 ENGINE.  GROUND RUNUP AND OPERATIONS CHECKED NORMAL.  S/D  INVESTIGATION INTO THE SHUTDOWN OF ENGINE, S/N 4405, DUE TO HIGH AVM AND N2 OVERSPEED, REVEALED HIGH PRESSURE COMPRESSOR 5TH SHROUD RING, MFG P/N UL26735, HAD ANTI-FRET PADS LIBERATE FROM VANE SLOTS IMPACTING BLADES, CAUSING BLADE FRACTURES.  ENGINE WAS REPAIRED AND RETURNED TO SERVICE.  (M)


REMARKS:
FLT NR 0417 - TPA - THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF.  THE GEAR WAS RECYCLED THREE TIMES BUT GEAR STILL WOULD NOT RETRACT.  FLIGHT DIVERTED TO TPA.  MAINTENANCE REPLACED O-RING AT THE NOSE STRUT SCHRADER VALVE.  THE STRUT WAS SERVICED AND THE GEAR CYCLED.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
AFTER TAKEOFF SHUT DOWN RIGHT ENGINE, DUE TO LOUD BANG AND N1 ROLLED BACK TO 62 PERCENT.  FOUND METAL PARTICLES IN EXHAUST PIPE.  REPLACED RIGHT ENGINE.  ENGINE OPERATION CHECKED NORMAL.  S/D INVESTIGATION INTO ENGINE STALL AND METAL IN EXHAUST PIPE, REVEALED FIRST STAGE TURBINE BLADE, P/N 836201, RELEASED OUTER PORTION OF AIRFOIL DUE TO FATIGUE CRACK.  ENGINE WAS REPAIRED AND RETURNED TO SERVICE.  (M)


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND CHORD CRACKED IN AFT EDGE AT I/B FASTENER OF 18A CHORD ANGLE, LEFT MAIN WHEEL WELL,BS 727 S18A.  INSTALLED CHORD ANGLE REPAIR PER DRAWING 65-29228.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND NOSE WHEEL WELL CEILING CRACKED AT SPRING ATTACH POINT, BS 277 RBL 10.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND TWO CRACKS AT T-CHORD BS 178 BULKHEAD AFT SIDE, WL 184, ONE I/B AND ONE O/B.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, RBL 5.7 FROM WL 184 TO 201.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, LBL 5.7 FROM WL 184 TO 201.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
MAIN STABILIZER TRIM WAS INOPERATIVE, OVERRIDE USED TO OPERATE SYSTEM.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFULLANDING.  INSPECTED AND REPLACED MAIN STABILIZER TRIM RELAY PER BOEING M/M.


REMARKS:
FOUND 2 EMERGENCY FLOOR TRACK LIGHTS INOP.  RELAMPED AND RECONNECTED LIGHTS PER BOEING M/M.


REMARKS:
AFT GALLEY EMERGENCY LIGHT REMAINS ILLUMINATED WITH SWITCH IN ARMED POSITION.  REPLACED LIGHT BATTERY PACK PER BOEING M/M.


REMARKS:
OKC - FLT 1409 - THE NR 1 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED.  THE CSD WAS DISCONNECTED AND FLIGHT DIVERTED TO OKC.  MAINTENANCE REPLACED THE TEMPERATURE BULB.  OPERATIONS CHECKED GOOD.  (X)


REMARKS:
INT - DURNG 'Q-1' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORROSION ON BRACKET AT BS 792, S-23L AND S-24L.  CORROSION TASK NR:  C53-208-01.  CORROSION LEVEL:  2.  BURNISHED TOP BRACKET AND REPLACED BOTTOM BRACKET, REPAIRED PER SRM 51-10-2.  (X)


REMARKS:
INT - DURING 'Q-1' CHECK, VISUAL INSPECTION FOUND .75 INCH BY 1 INCH SEVERAL PLACES CORRODED BS 787 TO BS 847 ON FLOOR ANGLE.  CORROSION TASK NR:  C53-208-01.  CORROSION LEVEL:  2.  REPLACED ANGLE, REPAIRED PER SRM 51-10-02.  (X)


REMARKS:
INT - DURING 'Q-1' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 3 FOOT CORROSION ON ANGLE AT BS 947.5.  CORROSION TASK NR:C53-208-01.  CORROSION LEVEL:  2.  FABRICATED NEW ANGLE REF DRAWING NR 65-49616, REPAIRED PER BOEING DRAWING 65-49616.(X)


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM CRACKED IN  E/E COMPARTMENT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANAUL.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND AFT SECTION OF SHEAR BEAM STRINGER 18A CRACKED 1.25 INCHES, RIGHT WHEELWELL.  REPAIREDPER SWA ACO 640-53.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND AFT SECTION OF SHEAR BEAM STRINGER 18A CRACKED 1.5 INCHES, AT AFT BULKHEAD.  REPAIRED PER SWA ACO 640-53.


REMARKS:
FOUND FLOOR TRACK LIGHTING TORN UP AT ROW 6 AND SEVERAL LIGHTS INOP.  REPAIRED TRACK LIGHTING AND REPLACED LIGHTS PER BOEING M/M.


REMARKS:
ON TAKEOFF, EXPERIENCED BIRDSTRIKE TO NR 2 ENGINE CAUSING VIBRATION.  AIRCRAFT RETURNED TO SFO AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRDSTRIKE INSPECTION AND FOUND TWO ENGINE FAN BLADES BENT.  REPLACED BLADES AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
DURING CLIMB-OUT,  NR 1 KRUGER FLAP TRANSIT LIGHT REMAINED ILLUMINATED.  AIRCRAFT DIVERTED INTO MDW AND MADE AN UNEVENTFUL LANDING.  REPLACED NR 1 KRUGER FLAP POSITION SENSOR PER BOEING M/M.


REMARKS:
CLT - THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK.


REMARKS:
AFT SECTION OF EPL'S AND TAIL COMPARTMENT EMERGENCY LIGHTS INOP.  FOUND WIRING SHORTED BEHIND PANEL IN TAIL COMPARTMENT.  REPAIRED WIRING AND REPLACED FUSES IN BATTERY CHARGER IAW MM CH 33.  (M)


REMARKS:
AFTER TAKEOFF, FLT NR 58, ATL TO PBI, UNABLE TO RAISE NOSE LANDING GEAR.  RETURNED TO ATLANTA.  UPON INSPECTION OF NOSEWHEEL WELL, FOUND NOSE LANDING ACTUATOR FITTING SHEARED.  REMOVED AND REPLACED NLG LOCK ACTUATOR FITTING AND REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR.  PERFORMED GEAR SWING AND OPS CHECK PER MM 32-33-0 AND MM 32-33-11.  (M)


REMARKS:
CLT - THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK.  (M)


REMARKS:
STL - DURING CRUISE, EGRESS LIGHTS, FROM SEAT ROW 8 TO ROW 14, CAME ON.  CYCLED EMERGENCY LIGHT SWITCH TO OFF, TO ARMED, EXTINGUISHED LIGHTS.  FOUND OPEN FEEDER CABLE, MFG P/N 5853-1.  REPLACED FEEDER CABLE AND LIGHT OPERATION CHECKED NORMAL.  (M)


REMARKS:
STL - AFTER TAKEOFF SMOKE WAS REPORTED EXITING SIDEWALL SEAT ROWS 10 AND 11, RIGHT SIDE.  VISUALLY CHECKED AREA.  REMOVED SIDEWALL AND FOUND THREE INCH AIR CONDITIONING DUCT CONNECTOR LOOSE CAUSING CONDENSATION TO EXIT DUCT.  REINSTALLED DUCT CONNECTOR.  OPERATED AIR CONDITIONING SYSTEM AND ALL CHECKED NORMAL.  (M)


REMARKS:
MCI - DURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO OIL FILTER BYPASS LIGHT CAME ON.  REPLACED OIL FILTER AND OIL FILTER BYPASS SWITCH, MFG P/N 42D109-1A.  ENGINE OPERATION CHECKED NORMAL.


REMARKS:
STL - AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE TO LANDING GEAR UP POSITION.  USED LANDING GEAR OVERRIDE PROCEDURES TO RETRACT LANDING GEAR.  FOUND LANDING GEAR ACCESSORY UNIT, MFG P/N 65-60211-17, WITH INTERNAL MALFUNCTION.  REPLACED LANDING GEAR ACCESSORY UNIT.  LANDING GEAR OPERATION CHECKED NORMAL.  (M)


REMARKS:
DFW - DURING DESCENT SHUT DOWN NR 2 ENGINE, DUE TO HIGH OIL TEMPERATURE AND LOW OIL QUANTITY.  FOUND ENGINE HAD INTERNAL OIL LEAK.  REPLACED NR 2 ENGINE.  ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME 49,375, TOTAL CYCLES 54,671.


REMARKS:
DCA - FLT 0450 - THE CREW HAD DECLARED AN EMERGENCY DUE TO A FLAP ASYMMETRY PROBLEM.  MAINTENANCE RESET THE TRIP INDICATORS ON THE LEFT AND RIGHT FLAP TORQUE TUBE ACTUATORS.  THE FLAPS WERE CYCLED.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
LGA - FLT NR 0329 - DURING CLIMB, FLIGHT EXPERIENCED A RAPID DECOMPRESSION. AN EMERGENCY WAS DECLARED AND A DESCENT WASMADE TO 10,000 FEET.  CABIN PRESSURE DID NOT RAISE ABOVE 14,000 FEET PRE-EMPTING THE OXYGEN MASKS TO DEPLOY.  THE FLIGHT DIVERTED TO LGA AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE DUCT ASSEMBLY ON THE RIGHT PACK.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL AREAS OF CORROSION APPROXIMATELY 2 INCHES IN DIAMETER BS 794 S-22 R TO S-24 R INNER DOOR FRAME DOUBLER.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  FABRICATED NEW DOUBLER AND INSTALLED SAME.  REPAIRED PER SRM 51-10-2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 4 INCH ATTACH ANGLE CORRODED, BS 807 RBL 17.5.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  FABRICATED NEW ANGLE AND INSTALLED, REPAIRED PER DRAWING 65-46551.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 12 INCH AND .5 INCH BY 14 INCH CORROSION, BS 985.6 AT LBL 43 INCHES - RBL 30 INCHES ON FLOOR BEAM.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPLACED T-CAP ON FLOOR BEAM,REPAIRED PER TR 53-10-05.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH DIAMETER CORROSION, STATION 967 LBL 6, ON FLOOR BEAM.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REMOVED DAMAGED FLOOR BEAM CAP AND SPLICED IN LOCAL MFGD CAP AND SPLICED ANGLES AND DOUBLERS.  REPAIR PER SRM 53-00-51.  (M)


REMARKS:
LGA - FLT 0599 - THE CAPTAINS SLIDING WINDOW CRACKED.  CAPTAIN TURNED OFF THE WINDSHIELD HEAT AND RETURNED TO LGA.  MAINTENANCE REPLACED THE CAPTAINS SLIDING WINDOW.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
ATL - FLT 1194 - THE CREW RECEIVED AN EXCESSIVE FUEL FLOW INDICATION ON THE LEFT ENGINE.  A PASSING AIRCRAFT NOTICED AND EXCESSIVE CONTRAIL OUT OF THE LEFT ENGINE.  CREW SHUTDOWN THE LEFT ENGINE.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 1 ENGINE ASSY.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
DCA - WHILE INSPECTING THE TAIL AREA FOR FUEL FUMES, THE TAILCONE WAS INADVERTENTLY DEPLOYED.  THE TAIL SLIDE DID NOT DEPLOY.  THE SLIDE WAS RERIGGED WITH THE TAIL CONE LANYARD TO DETERMINE THE REASON FOR THE SLIDE NOT DEPLOYING.  MAINTENANCE RERIGGED THE SLIDE THEN RECHECKED IT FOR PROPER INSTALLATION.  (M)


REMARKS:
PHL - FLT NR 1876 - AT 4000 FEET, THE AIRCRAFT LOST OIL PRESSURE AND QUANTITY FOR THE NR 1 ENGINE.  THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED.  MAINTENANCE REPLACED THE NR 1 ENGINE.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
CLT - FLT 0741 - RETURN TO CLT DUE TO THE AIRCRAFT NOT ABLE TO BE PRESSURIZED.  MAINTENANCE PRESSURE CHECKED THE CABIN AND CHECKED THE MANUAL AND AUTO CONTROLLER.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
CLT - FLT NR 0207 - THE FLIGHT ATTENDANT REPORTED SMELLING SMOKE AND FUMES IN THE CABIN.  THE CREW ELECTED TO DIVERT TOCLT.  MAINTENANCE CHECKED ALL OVERHEAD PANEL LIGHTS, BALLASTS AND OXYGEN.  RAN ENGINE AND APU AT POWER.  MX CHECKED THEACM OILS, TAIL COMPARTMENT, GALLEY AREA, FORWARD/AFT FEEDER CABLES AND E/E COMPARTMENT AFT BAG BIN AREA.  NO FAULTS FOUND.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CORROSION AROUND NUT PLATES (TOTAL APPROXIMATELY .25 INCH BY 6INCHES), BS 958 RBL 8 INCHES.  CORROSION TASK NR C51-107-02, CORROSION LEVEL 2.  REMOVED INTERCOSTAL AND INSTALLED NEW,REPAIRED PER SRM 51-10-02.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUT PLATE HOLES, LOWER SIDE INTERCOSTAL BS 989 RBL 17. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-30-02.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUT PLATE HOLES, BS 996-BS 1006 LBL 13.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  REMOVED AND REPLACED INTERCOSTAL BS 986-BS 1006.  REPAIRED PER SRM 51-10-2 AND SRM 51-40-2.  (M)


REMARKS:
DURING C-CHECK INSPECTION, FOUND R1 DOOR, UPPER TRAILING EDGE WITH EXTERNAL SKIN BULGES OF .50 INCH DURING PRESSURIZATION.  OPENED AREA, FOUND SKIN CRACKED, STOP DRILLED AND INSTALLED REPAIR DOUBLERS, TREATED AND PRIMED PER SRM 51-10-1, SRM 51-40-3, SRM 51-10-2.  ALTERNATE REFERENCE RECEIVED UNDER REPAIR PLAN BOEING 7272-94-6285.  TIME LIMITED REPAIR 18 MONTHS OR 3,000 CYLES, WHICHEVER FIRST.


REMARKS:
DURING C-CHECK INSPECTION, FOUND R1 DOOR OUTER SKIN LOWER FORWARD CORNER WITH SKIN CRACK AND POPPED RIVET HEADS.  INSTALL REPAIR DOUBLER AND FILLER, TREATED, PRIMED.  PERFORMED HIGH FREQUENCY EDDY CURRENT, NO CRACKS DETECTED AFTER CUT-OUT. REF. SRM 52-00-3, SRM 51-30-5, SRM 51-30-8, AND SRM 51-10-2.


REMARKS:
CLT -FLT NR 1437 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
BWI - FLT 0589 - THE EMERGENCY LIGHTS WERE POPPING THE CIRCUIT BREAKER.  MAINTENANCE REPAIRED WIRES THAT WERE FOUND TO BE CHAFING IN THE CEILING OF THE AFT LAVATORY AGAINST THE WATER LINE.  (M)


REMARKS:
PIT - FLT 0519 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE INSTALLED NEW BATTERIES IN THEPOWER PACK.  (M)


REMARKS:
PIT - FLT 0281 - THE REAR PASSENGER DOOR WAS CLOSED WITH THE SAFETY STRAP OUTSIDE.  AIRCRAFT RETURNED TO PIT.  MAINTENANCE SECURED THE RIGHT REAR SERVICE DOOR SAFETY STRAP IN THE HOLDER.  NO DAMAGE WAS NOTED TO THE DOOR OR FUSELAGE.  (M)


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LONGERON WAS FOUND CRACKED AT FS 1059 RT SIDE MIDDLE OF THE APU EXHAUST DUCT CUT OUT AFT HOLE.  FABRICATED AND INSTALLED LONGERON IAW DC9 SRM 51-10-4 AND 51-01 PAGE 4.  N/R NR 027N1/0218.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE SKIN IS OIL CANNED ON THE RT SIDE AT FS 1130 JUST AFT OF THE RT ENGINE PYLON.  REMOVED DAMAGED AREA.  FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW DC9 SRM 53-04-02.  N/R NR 027N1/0399.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA I/G CORROSION AT LONGERON 28L AND FRAME 917 LEFT SIDE OFCARGO DOOR.  REMOVED DAMAGED.  FABRICATED AND INSTALLED DOUBLER AND TWO 'L' ANGLE BRACKETS IAW DC9 SRM 51-10-2A AND 53-05.  N/R NR 027N1/0391.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT FUSELAGE EXTERNAL HAS A NON STANDARD REPAIR BELOW THE CABIN OUT FLOW VALVE.  REMOVED THE OLD REPAIR.  FABRICATED AND INSTALLED NEW DOUBLER AND FILLER IAW DC9 SRM 53-04.  N/R NR 027N1/0337.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT FUSELAGE EXTERNAL HAS A NON SRM REPAIR BELOW THE EQUIPMENT RACK COOLING EXHAUST.  REMOVED OLD REPAIR.  FABRICATED A NEW DOUBLER AND FILLER AND INSTALLED IAW DC9 SRM 53-04.  N/R NR 027N1/0328.  (M)


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE EXTERNAL HAS A NON SRM REPAIR AT FS 570 RBL 18.  REMOVED OLD REPAIR.  FABRICATED NEW REPAIRS AND INSTALLED IAW DC9 SRM 53-04.  N/R NR 027N1/0323.


REMARKS:
FLT NR 485 - PHF-ATL - COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOP UPON CREW LEAVING THE AIRCRAFT IN ATL.  MAINTENANCE REPLACED BATTERY PACKS P/N EA1D131D15 AND 6012231.  OPS CHECKED OK.


REMARKS:
CLE - THE CABIN CEILING EXIT SIGN, FOR THE OVERWING EMERGENCY EXIT, WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  (M)


REMARKS:
SFO - FLT NR 0851 - THE FLAPS WERE FROZEN AT 15 DEGREES AND WOULD NOT RETRACT.  THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO SFO.  MAINTENANCE FOUND A BOLT ON THE FLAP TRANSMISSION.  OPERATIONS CHECKED NORMAL.  (M)


REMARKS:
DCA - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERIES.  (M)


REMARKS:
AT 35,000 FEET, EXPERIENCED CABIN ALTITUDE ALERT WARNING.  CREW WAS UNABLE TO CONTROL CABIN PRESSURE USING STANDBY OR MANUAL MODES.  INITIATED EMERGENCY DESCENT TO 15,000 FEET WHERE CREW REGAINED CONTROL OF PRESSURE.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT SJC.  INSPECTED AND PERFORMED PRESSURE CONTROL TEST WITH NO DEFECTS NOTED.  REPLACED MAIN OUTFLOW VALVE, O/H PRESSURE CONTROL PANEL AND PRESSURE CONTROLLER PER BOEING M/M.


REMARKS:
LGA - FLT NR 8076 - EN ROUTE BOS TO CLT, THE CABIN ALTITUDE HORN SOUNDED AND THE CABIN PRESSURIZATION WAS CLIMBING.  CAPTAIN DECIDED TO DIVERT TO LGA.  MAINTENANCE REPLACED THE CABIN PRESSURE SELECT PANEL, PRESSURE CONTROLLER AND OUTFLOW VALVE.  (M)


REMARKS:
PIT - FLT 0317 - UPON CLIMB-OUT, THE CAPTAIN REPORTED THAT HE SHUT THE AIR CONDITIONING PACK OFF AND WAS RETURNING TO PIT.  MAINTENANCE REPLACED THE LEFT COOLING PACK.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
PHF - FLT NR 1297 - AFTER TAKEOFF FROM PHF, CREW RECEIVED A CARGO DOOR LIGHT.  CAPTAIN ELECTED TO RETURN TO PHF.  MAINTENANCE ADJUSTED THE AFT CARGO DOOR WARNING SWITCH STRIKER.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND .5 INCH CRACK FORWARD VERTICAL WEB IN NLG WHEEL WELL LOWER LIGHTENING HOLE.  INSTALLED DOUBLER REPAIR PER SRM 53-02-01 FIG 8.  (M)


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND DENT 3MM DEEP AND 1 INCH IN DIAMETER FUSELAGE SKIN 6 INCHES BELOW AFT WATER SERVICE PANEL BETWEEN STRINGER 9 AND 10.  INSTALLED DOUBLER REPAIR PER SRM 53-02.  (M)


REMARKS:
CLT - THE OVERHEAD EMERGENCY LIGHTING COMES ON WITH THE SWITCH IN THE ARMED POSITION.  MAINTENANCE TROUBLESHOT THE EVACUATION LIGHTING SYSTEM.  OPERATIONS WERE FOUND TO BE NORMAL.  (M)


REMARKS:
JFK - FLT NR 803 - DURING CRUISE, SMOKE AND ELECTRICAL ODOR EMITTED FROM AFT GALLEY E-1 SERVING CART CONTROLLER, MFG P/N B006781.  TURNED OFF CONTROLLER AND OPENED CIRCUIT BREAKERS.  REPLACED THE E-1 CART CONTROLLER AND OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266.  SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4.


REMARKS:
SRQ - FLT NR 0139 - DURING A GO-AROUND PROCEDURE DUE TO THUNDERSTORMS, THE LEFT ENGINE WOULD NOT PRODUCE SELECTED THRUST.  CAPTAIN DECIDED TO DIVERT TO SRQ WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT ENGINE LP SHAFT GOVERNOR.LEAK CHECKED GOOD.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN VERTICAL STAB ATTACH ANGLE VERTICAL LEG AFT END LEFT SIDE.  INSTALLED DOUBLER REPAIR 14 INCHES IN LENGTH PER SRM 53-05 FIG 23A.  (M)


REMARKS:
PIT - DURING C-CHECK INSPECTION, FOUND 2 INCH CRACK AND STRINGER NR 68R APPROXIMATELY 4 INCHES AFT OF STATION 3870.  INSTALLED SPLICE REPAIR PER SRM 51-70-06 REPAIR NR 5 PG 206.  (M)


REMARKS:
LGA - THE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK FOR ROW 12 TO 16.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
FLT NR 556 - STL - AFTER TAKEOFF, LANDING GEAR LEVER WAS LOCKED.  USED OVERRIDE PROCEDURES TO RETRACT LANDING GEAR.  FOUND WORN BOLT FOR LANDING GEAR SAFETY SWITCH SENSOR ACTUATOR.  REPLACED BOLT AND LANDING GEAR OPERATION CHECKED NORMAL.


REMARKS:
JFK - FLT NR 740 - DURING CRUISE AFT GALLEY SERVING CART NR 4, EMITTED SMOKE AND ELECTRICAL ODOR.  TURNED OFF AND DISCONNECTED CART, MFG P/N 88801-1.  FOUND MALFUNCTIONING HEATING PLATES.  REPLACED SERVING CART AND OPERATION CHECKED NORMAL.


REMARKS:
MCI - FLT 179 - DURING CLIMB, LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AND LEFT MAIN LANDING GEAR UNSAFE RED LIGHT ILLUMINATED.  VERIFIED LANDING GEAR WAS DOWN AND DOOR REMAINED OPEN.  FOUND LEFT MAIN LANDING GEAR DOOR ACTUATOR BUSHING, MFG P/N S2210370P9-157, MISSING.  INSTALLED BUSHING AND LANDING GEAR AND LANDING GEAR DOOR OPERATION CHECKED NORMAL.


REMARKS:
MCI - DURING C-CHECK, FOUND TWO CRACKS, EACH APPROXIMATELY ONE INCH LONG, IN LEFT MLG WHEELWELL CEILING PRESSURE DECK AFT OUTBOARD CORNER, FORWARD OF 950 BULKHEAD, LBL 56 AND 58.  REPAIRED BY INSTALLING DOUBLER PER ARA 9372.  TOTAL CYCLES 42,177.


REMARKS:
MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN APPROXIMATELY .030 TO .015, STRINGER 17R TO 19R, AND STRINGER 17L TO 19L, FS 720E TO 720F.  ALSO, WORN APPROXIMATELY .040, STRINGER 19.  REPAIRED PER ARA 9354.  TOTAL CYCLES 24,723.


REMARKS:
MCI - DURING OP-15 FOUND RIGHT WING RS AFT FLAP CENTER HINGE FITTING MOUNT AREA REAR SPAR WEB, CRACKED .75 INCH IN EYEBROW AT UPPER OUTBOARD HOLE.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER SB 57-179 AND DRAWING J060272-502.


REMARKS:
MCI - DURING OP-17, FOUND A ONE INCH CRACK IN SKIN ON VERTICAL STABILIZER LEFT SIDE AT BASE, FS 1330.  STOP DRILLED CRACK PER SRM 51-10-1, AND REPAIRED PER ARA9370A.  TOTAL CYCLES 24,723.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STATION 945 TO 996.  REMOVED AND REPLACED LONGERON SECTION PER SRM51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996.  REMOVED AND REPLACED LONGERON SECTION PER SRM51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.


REMARKS:
CLT - FLT NR 0690 - THE AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF.  THE CAPTAIN DECIDED TO RETURN TO CLT.  NO EMERGENCYWAS DECLARED.  MAINTENANCE REPLACED THE AIR CONDITIONING S/O RELAY AND THE RATE CONTROL VALVE.  REFERENCE NR USAA950896.


REMARKS:
PIT - FLT 0753 - UPON GEAR RETRACTION, CREW RECEIVED AN INDICATION THAT THE RIGHT MAIN GEAR WAS NOT RETRACTED.  FLIGHT RETURNED TO PIT.  MAINTENANCE ADJUSTED THE DOWNLOCK ACTUATOR.  (M)


REMARKS:
CLT - FLT NR 0690 - THE AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF.  THE CAPTAIN DECIDED TO RETURN TO CLT.  NO EMERGENCYWAS DECLARED.  MAINTENANCE REPLACED THE AIR CONDITIONING S/O RELAY AND THE RATE CONTROL VALVE.  (M)


REMARKS:
CLT - DURING 'MQ-4' VISUAL CHECK INSPECTION, FOUND A 2 INCH BY 2 INCH CORRODED AREA LOCATED AT BS 344 BETWEEN BL 24 LT AND BL 8 RT.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  INSTALLED NEW 'T' CAP AND REPAIR ANGLES AND STRAPS AND FILTERS, REPAIRED BY SRM 53-10-03 AND SRM 51-70-13.  (M)


REMARKS:
CLT - DURING A Q-1 CHECK INSPECTION, FOUND A CRACK 14 INCHES BY 32 INCHES, BETWEEN STATION 294.5 AND 328, STRINGER 19R AND 22R.  DOUBLER INSTALLED (PREVIOUS REPAIR).  (M)


REMARKS:
CLT - DURING A Q-1 CHECK INSPECTION, FOUND A 25 INCH BY 6.5 INCH CRACK (PREVIOUS REPAIR) LOCATED BETWEEN STATION 360 AND STATION 400, S-20R AND S-21R.  DOUBLER INSTALLED (PREVIOUS REPAIR).


REMARKS:
CLT - DURING A Q-1 CHECK INSPECTION, FOUND A 1 INCH SMALL HOLE (PREVIOUS REPAIR) BETWEEN STATION 887 TO STATION 907, 4 INCHES ABOVE S-22L.  PATCH INSTALLED (PREVIOUS REPAIR).  (M)


REMARKS:
CLT - DURING 'MQ-4' VISUAL CHECK INSPECTION, FOUND NUMEROUS AREAS OF CORROSION AROUND FLOOR BOARD 17 INCHES ATTACH HOLES.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  INSTALLED NEW T-CAP, REPAIR ANGLES, STRAPS AND FILTERS.  REPAIRED BY TRM 53-10-03 AND SRM 51-70-12.  (M)


REMARKS:
CLT - DURING A Q-4 EDDY CURRENT CHECK, INSPECTION FOUND A 3.5 INCH CRACK ON STATION 520 EXTENDING 1.8 INCHES OUTBOARD AND 1.7 INCHES INBOARD OF LBL 45.5 OF FLOOR BEAM.  INSTALLED REPAIR DOUBLERS, RADIUS FILLERS AND NEW VERTICAL ANGLE PER EA 39548.  (M)


REMARKS:
CLT- DURING A Q-4 EDDY CURRENT CHECK, INSPECTION FOUND A 1.9 INCH CRACK ON STA 520 EXTENDING 1 INCH INBOARD AND .9 INCHOUTBOARD OF RBL 45.5 OF FLOOR BEAM.  INSTALLED REPAIR DOUBLER AND RADIUS FILLERS AND NEW VERTICAL ANGLE PER EA 39548.  (M)


REMARKS:
CLT - DURING A Q-4 EDDY CURRENT CHECK, INSPECTION FOUND A .9 INCH CRACK ON STATION 520 EXTENDING OUTBOARD FROM LBL 24.75 OF FLOOR BEAM.  INSTALLED REPAIR DOUBLERS, RADIUS FILLERS AND NEW VERTICAL ANGLE PER EA 34548.  (M)


REMARKS:
INT - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND 4 INCH BY 2 INCH CORRODED AREA BETWEEN STATION 947.5 AND 967 AT S-26L.  INSTALLED REPAIR SPLICES.  REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
INT - DURING 'CD-6' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BETWEEN STATION 967 AND 986.5 AT S-27L.  INSTALLED REPAIR SPLICES.  REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
ROA - DURING 'BX CHECK' VISUAL INSPECTION, FOUND 13 .125 INCH LONG STRINGER CORRODED FUSELAGE STATION 967 JUST TO THE LEFT OF WATER TANK.  REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM.  REPAIRED PER SRM 53-10-3 FIG1 FUSELAGE STRINGER REPAIR S-14-28.  (M)


REMARKS:
LAX - FLT NR 1898 - AT 131 KNOTS, A BIRD WAS INGESTED INTO THE NR 1 ENGINE CAUSING A LOSS OF POWER AND NOTICEABLE ENGINE VIBRATION.  IT WAS DECIDED TO DIVERT TO LAX.  NO EMERGENCY WAS DECLARED.  MAINTENANCE REPLACED THE NR 19 AND NR 20 FANBLADES.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
PHL - FLT 0059 - THE EMERGENCY LOW LEVEL LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE CHECKED THE OPERATION OF THEEMERGENCY LIGHTS FROM THE FLIGHT ATTENDANT AND COCKPIT POSITIONS.  OPERATIONS CHECKED NORMAL.  (M)


REMARKS:
DEN - FLT 0021 - BOTH ENGINES OVER TEMP ON TAKEOFF.  FLIGHT RETURNED TO DENVER.  MAINTENANCE INSPECTED ENGINES.  FERRIED AIRCRAFT TO PIT.  REPLACED NR 2 ENGINE ASSEMBLY, INSPECTED NR 1 ENGINE FOR AREA B EXCURSION.  FOUND THE REASON TO BE PERFORMANCE DETERIORATION.  OK FOR SERVICE.  (M)


REMARKS:
MCI - FLT NR 0675 - CAPTAIN DIVERTED TO MCI DUE TO HIGH OIL CONSUMPTION ON THE LEFT ENGINE.  THE ENGINE WAS NOT SHUT DOWN.  FLIGHT LANDED SAFELY.  MAINTENANCE FOUND A CUT SEAL ON THE LEFT ENGINE HIGH SPEED GEAR BOX RADIAL DRIVE SHAFT.  THEASSEMBLY WAS RESEALED AND THE UPPER AND LOWER OIL SEALING SLEEVES WERE REPLACED.  NO LEAKS NOTED.  (M)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORROSION AT BS 905, LBL 21.5 WL 168, BS 907, S5R AND BS 360, S4L AND S14L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 747, BS 767 S9R AND AT BS 639 S3L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 42 TO 55 WL 170.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 663 S4R, BS 500 LBL 2 WL 155, BS 344 LBL 46 WL 170 AND BS294 WL 209 RBL 55.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND KEEL BEAM LOWER O/B FLANGE CORRODED AT BS 707 TO 727, LBL 7 WL 149.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND KEEL BEAM FASTENER HOLE CORROSION AT LBL 5.5, AT BS 673.75, 677, 687.5, 692.25, 706.75 AND 708.25.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 963, BETWEEN 20 AND 21L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 842 TO 857 BETWEEN 26R AND 27L, BS 480 BETWEEN S27 AND 28R AND AT BS 306 ABOVE S25L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND T-CHORD CRACKED AT AFT CARGO BAY, BS 726 RBL 8.5 WL 203.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND GOUGE IN FWD SIDE OF BS 1156 BULKHEAD AND ON ADJOINING WEB BEHIND RT CENTER SECTION HINGE.  REPAIRED PER TRAMCO EWO 95-0560 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND COCKPIT NUMBER 1 WINDOW POST CRACKED AT UPPER AFT CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947 WL 208 RBL 10 TO 16, BS 294 LBL 15 RBL 9 WL 208 AND BS 360 RBL 14 WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE USING AUTO, MANUAL OR STANDBY MODES.  AIRCRAFT RETURNED TO ABQ AND MADE ANUNEVENTFUL LANDING.  INSPECTED AND FOUND LEFT WATER SEPARATOR BAG CANISTER LEAKING.  REINSTALLED CANISTER AND O-RINGS PER M/M.


REMARKS:
LAX - FLT 119 - DURING APPROACH WHEN LIGHTS WERE TURNED ON, SMOKE EMITTED FROM EXTERIOR LIGHT CONTROL PANEL.  TURNED OFF LIGHTS AND SMOKE DISSIPATED.  FOUND LIGHT SWITCH, MFG PN 25307-222, HAD OVERHEATED.  REPLACED SWITCH AND OPERATION CHECKED NORMAL.  CHECK C-8C - 8-6-95 - JFK.


REMARKS:
DTW - FLT 267 - DURING POWER CHANGE AT LEVEL OFF, NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED.  SHUT DOWN NR 2 ENGINE SN 3989.  REPLACED NR 2 ENGINE OIL BYPASS PRESSURE SWITCH, MFG PN A00803-2 AND OIL FILTER ELEMENT, MFG PN 7578678.  ENGINE RUN-UP OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  50,538 HOURS; 34,442 CYCLES.  CHECK C-3 - 10-7-94 - MCI.


REMARKS:
STL - FLT 693 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED NOSE LANDING GEAR GREEN, LOCKED LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR AND GREEN LOCKED LIGHT ILLUMINATED.  FOUND DEFECTIVE NOSE GEAR DOWNLOCK SWITCH, MFG PN H14-6.  REPLACED NOSE GEAR DOWNLOCK SWITCH AND LANDING GEAR LIGHTS, OPERATION CHECKED NORMAL.  CHECK C - 8-4-95 - STL.


REMARKS:
STL - FLT 582 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR AND DOOR LIGHT WAS SLOW TO EXTINGUISH.  FOUND DEFECTIVE RIGHT MAIN LANDING GEAR DOOR SWITCH, MFG H14-6.  REPLACED RIGHT MAIN LANDING GEAR DOOR SWITCH AND DOOR LIGHT, OPERATION CHECKED NORMAL.  CHECK C - 6-24-94 - STL.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STA 945 TO STA 996.  REMOVED AND REPLACED LONGERON SECTION PER SRM51-30-5, SRM 51-30-2, AND TWA STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  67,006 HOURS; 73,957 CYCLES.


REMARKS:
STL - FLT 556 - AFTER TAKEOFF, LANDING GEAR LEVER WAS LOCKED.  USED OVERRIDE PROCEDURES TO RETRACT LANDING GEAR.  FOUNDWORN BOLT FOR LANDING GEAR SAFETY SWITCH SENSOR ACTUATOR.  REPLACED BOLT AND LANDING GEAR, OPERATION CHECKED NORMAL.  CHECK C - 8-8-95 - MCI.


REMARKS:
SLC - FLT 777 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG DID NOT EXTEND.  CYCLED LANDING GEAR AND NOSE GEAR EXTENDED AND LOCKED.  LUBRICATED NLG, INSPECTED NLG AND DOORS, ALL APPEARED NORMAL.  CHECK C-1 - 11-21-94 - MCI.


REMARKS:
STL - FLT 264 - DURING APPROACH, NOSE LANDING GEAR DID NOT EXTEND UNTIL MAIN LANDING GEAR WAS DOWN AND LOCKED.  FOUND LOCK RELEASE ACTUATOR, MFG PN 65-40467-6, HAD INTERNAL MALFUNCTION.  REPLACED NLG LOCK RELEASE ACTUATOR AND NLG OPERATIONCHECKED NORMAL.  CHECK C-1 - 11-21-94 - MCI.


REMARKS:
CLE - FLT 384 - DURING DESCENT, SHUT DOWN NR 2 ENGINE, SN 2161, DUE TO LOW OIL PRESSURE LIGHT ILLUMINATION AND DECREASING OIL QUANTITY.  FOUND OIL LEAK AT NR 1 BEARING AND METAL PARTICLES IN OIL SCREEN.  CHANGED NR 2 ENGINE.  ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  48,251 HOURS; 54,637 CYCLES.  CHECK C- 7-3-95 - STL.


REMARKS:
IAH - FLT 309 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 2123, DUE TO DECREASING OIL QUANTITY.  FOUND OIL LINE B-NUT LOOSE ABOVE OIL FILTER.  TORQUED B-NUT, SERVICED ENGINE OIL.  ENGINE LEAK CHECKED AND OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  36,069 HOURS; 35,139 CYCLES.  CHECK C - 9-18-94 - STL.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 30 LOCATED AT FS 389 WAS FOUND CORRODED.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-05-04 AND DOUGLAS EO 53-02-0001.  N/R NR 027N1/0291.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD CARGO DOOR LOWER PAN WAS FOUND CORRODED.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-05, SRM 51-30-0, SRM 51-10-3, AND SRM 51-10-2.  N/R NR 027N1/0296.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LONGITUDINAL FLOOR STRUCTURE WAS FOUND CORRODED AT FS 256 TO FS 513 AT STR 28L TO STR 28R.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-11-2, SRM 51-10-3, SRM 51-30-2, AND SRM 51-10-2.  N/R NR 027N1/0292 AND 0293.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE AFT CARGO PIT LONGERON 30 CORRODED IN THE HATSECTION FROM FS 945 TO FS 950.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-04 ANDSRM 51-10-3.  N/R NR 027N1/0314.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE RT LOWER FUSELAGE SKIN HAS A 1 EACH FLUSH REPAIR AT LONGERON 25R/26R AR FS 334 THAT IS NON-CONFORMING.  ALSO, AT FS 465.  REMOVED OLD REPAIR AND DAMAGED SECTION OF SKIN.  FABRICATED AND INSTALLED NEW REPAIRS (FILLERS AND DOUBLERS) IAW DC9 SRM 51-10-3 AND SRM 53-04.  N/R NR 027A1/0066 AND 0067.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE FUSELAGE SKIN CRACKED AND CORRODED AROUND RADIO ALT. ANTENNA AT FS 340, FUSELAGE NR 30.  ALSO, FOUND CORRODED BLEND OUT BEYOND SRM LIMITS.  REMOVED DAMAGED SECTION.FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-04.  N/R NR 027N1/0287.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND AFT CARGO COMPARTMENT HAS SEVERE CORROSION BETWEEN FS 917 AND FS 897 AT LONGERON 29R.  REMOVED DAMAGED SECTIONS.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 51-10-2, SRM 51-30-2, AND SRM 51-10-2A.  N/R NR 027N1/0371.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA FOUND FUSELAGE SKIN AT FS 917 BELOW AFT CARGO DOOR REQUIRES REPAIR, CORROSION REMOVAL OUT OF LIMITS.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04.  N/R NR 027N1/0340.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A CRACK WAS FOUND IN THE CAPTAIN'S LEFT RUDDER PEDAL AFT, INBD BOLT HOLE DURING INSP ON SB 27-209, AD 82-04-02.  REMOVED AND REPLACED THE RUDDER PEDAL IAW SB 27-209 AND AD 82-04-02.  N/R NR 027A1/0153.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND RUDDER RT SIDE RIB NR 17 FWD OF EXISTING REPAIR HAS 1 EACH CRACK.  FABRICATED AND INSTALLED REPAIR MEMBERS FOR CRACKED RIB IAW DC9 SRM 55-03, FIG 12, AND SB 55-23.  N/R NR 027A1/0133.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND FS 604, LONGERON 29L END FITTING IS CORRODED AT FRAME.  ALSO, 29R FITTING.  REMOVED AND REPLACED THE END FITTING IAW DC9 SRM 53-02 AND SRM 51-10-4.  N/R NR 027A1/0106, 027A1/0110.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE FUSELAGE SKIN BELOW THE FWD CARGO DOOR AT FS 370 TO FS 426 IS CORRODED AND CRACKING.  FABRICATEDAND INSTALLED FUSELAGE SKIN REPAIRS IAW DC9 SRM 53-05, FIG 82 53-04, FIG 12B AND AERO CORP E.O. 94-097, REV IR DATED 1-6-95, FAA FORM 8110-3, DATED 1-12-95.  N/R NR 027N1/0039.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND LONGERON 30 AT FS 756 TO FS 794 CORRODED.  FABRICATED AND INSTALLED A NEW LONGERON, FRAME REPAIRS AND SPLICES IAW DC9 SRM 53-02, SRM 51-10-4, AND SRM 51-30-5.  N/R NR 027A1/0082.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, EXFOLIATED CORROSION WAS FOUND BEYOND LIMITS ON LONGERON 30 AT FS 784 THROUGH FS 958.  REMOVED AND REPLACED LONGERON 30 AND LONGERON SPLICES IAW DC9 SRM 53-02, FIG 15.  N/R NR027N1/0415.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND A NON-STANDARD REPAIR IS AT FS 313 AT UHF ANTENNA.  REMOVED ANTENNA AND OLD REPAIR.  FABRICATED AND INSTALLED NEW DOUBLER AND FILLER, THEN REINSTALLED ANTENNA IAW DC9 SRM 53-04-29, SRM 51-20-0, AND MM 21-20.  N/R NR 027N1/0353.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE RT SIDE FS 450 THROUGH FS 485 FILLER IS FALLING OUT OF PREVIOUS REPAIR.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND A CRACK IN THE FUSELAGE SKIN AFT SIDE OF PASSENGER ENTRANCE DOOR RUNNING THROUGH DOOR STOP HOLE APPROXIMATELY 2 INCHES LONG, FS 197 APPROXIMATELY 20 INCHES ABOVE WINDOW LINE.  FABRICATED AND INSTALLED FUSELAGE SKIN REPAIRS IAW DC9 SRM 53-05, FIG 26A.  N/R NR 027N1/0390.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND LEFT FS 389, LONGERON 20 HAS IMPROPER REPAIR.  REMOVED NON-STANDARD REPAIRS.  FABRICATED AND INSTALLED REPAIRS FOR LONGERON IAW DC9 SR 53-04 AND SRM 51-10-4.  N/R NR 027N1/0445.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE FWD CARGO PIT LOWER PANEL FROM FS 579 TO FS 598 AND LONGERON 27L TO LONGERON 28R HAS I.G. CORROSION.  FABRICATED AND INSTALLED FUSELAGE SKIN REPAIRS IAW DC9 SRM 53-10, FIG 2, AND AERO CORP E.O. 94-110, REV IR, DATED 12-19-94.  N/R NR 027N1/0409.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE E AND E COMPARTMENT, LONGERON 22, BETWEEN STA 160 TO STA 180, LOWER LEG.  REMOVED DAMAGED LONGERON AND REPAIRED IAW E.O. 95-159.  N/R NR 027F1-0007.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE FWD CARGO COMPARTMENT, LONGERON 29L FROM FS 332 TO FS 450.  INSTALLED NEW LONGERON, FS 332-FS 450 AND FS 332-FS 294, AND INSTALLED NEW SPLICES IAW DC9 SRM 53-02.  N/R NR 027N1-0135.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE LATERAL CABIN FLOOR SUPPORT BS 200 FROM BL ZERO TO RBL 22 AF 13.  FABRICATED PART IAW SRM 53-11-1.  ALODINE AND PRIMED PART IAW SRM 51-10.  DRILLED PART AND DEBURRED PART AND INSTALLED IAW SRM 53-11.  N/R NR 027D1-4046.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE RT AFT FS 1089 S-11 LEVEL FRAME WHICH WAS BLEEDING OUT BETWEEN ANGLE AND FRAME AT CANTED BULKHEAD TIE INTO FRAME.  DOT 1.  REMOVED ANGLES IAW SRM 51TO GAIN ACCESS TO CORROSION.  REMOVED CORROSION, FOUND FRAME WEB OUT OF LIMITS IAW SRM 51.  FABRICATD REPAIR DOUBLER, TREATED AND PRIMED METAL.  REINSTALLED ANGLES, DOUBLERS.  N/R NR 027D1-4072.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE FWD CARGO COMPT.  LONGERON NR 30L FROM FS 332 TO FS 450.  INSTALLED NEW LONGERON FS 294-FS 450 IAW DC9 SRM 53-02.  INSTALLED NEW SPLICES IAW DC9, SRM 53-02.  N/R NR 027N1-0135.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE LONGITUDINAL CABIN FLOOR SUPPORT, BS 220 AT LBL 14.  FABRICATED NEW FLOOR SUPPORT IAW DC9 SRM 51.  DRILLED HOLES AND DEBURRED IAW SRM 51.  ALODINED AND PRIMED IAW DC9 SRM 51, INSTALLED IAW DC9 SRM 51-30 AND SRM 51-30.  N/R NR 027D1-4046.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE LATERAL CABIN FLOOR SUPPORT BS 200 FROM RBL 22 TO RBL 44.  FABRICATD NEW PART, DRILLED HOLES AND DEBURRED, ALODINE AND PRIMED, AND INSTALLED NEW PART IAW SRM 51-10-2, 3, 4.  N/R NR 027D1-4046.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND A BULGE IN THE SKIN AT FS 148, LT SIDE , JUST BELOW LONGERON 18.  CUT OUT DAMAGED AREA AND FABRICATE PARTS IAW DC9 53-04.  INSTALLED REPAIR IAW SRM 53-04.  N/R NR 027F1-0027.


REMARKS:
UPON A SCHEUDLED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND AT THE FUSELAGE FRAME BS 218 AND UNDER FLOOR AT RBL 55, BOLT WAS RUSTY.  REMOVED EXISTING SPLICE, FITTING AND AIR DUCT.  ORDERED NEW FITTINGS, FABRICATED NEW CUSP SPLICE, HEAT TREATED TO 7025, DRILLED AND DEBURRED, ALODINED, PRIMED AND INSTALLED NEW FITTINGS.  CUSP SPLICE AND IAR DUCT ALL IAW 51-31-12.  N/R NR 027D1 4046.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A DENT  IN THE SKIN WAS FOUND AT FS 210, RT, BETWEEN LONGERON 18 AND LONGERON 17 AND 0.122 INCH DEEP.  THIS IS CONDITION NR 2.  CUT OUT DAMAGED AREA, FABRICATED 2 INCH FILLER PLATES, 2 INCHES BY .050 INCH, DOUBLER, 5 INCHES BY .063 INCH.  DRILLED HOLES, COUNTERSUNK AND DEBURRED, ALODINED AND PRIMED, INSTALLED AND SEALED IAW 51-20.  N/R NR 027E10027.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE E AND E COMPARTMENT, FS 180,BL 20L, UPPER FLOOR BEAM WEB AND L-ANGLE CRACKED.  REMOVED ANGLE, FABRICATED NEW ANGLE AND INTERCOSTAL REPAIRS AND INSTALLED IAW DC9 SRM CHAPTER 51-10-02 AND CHAPTER 53-05, FIGURE 100.  FS 180, BL 20L.  N/R NR 027D1-0225.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE RT AFT FUSELAGE CANTED BULKHEAD AREA, STA 1143, STR 9, EXFOLIATED BEYOND LIMITS.  REMOVED 18.025 INCHES OF EXFOLIATED LONGERON, FABRICATED REPAIR LONGERON OF 7075T6-.063.  FABRICATED REPAIR SPLICES OF 7075-T6.063 IAW SRM 53-02.  ALODINE AND PRIME PARTS IAW SRM 51-10-03, FAY SURFACE SEAL PARTS IAW SRM 51-20-0.  N/R NR 027D1-4072.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE FWD CARGO LONGERON 30 WAS CORRODED OUT 25 PERCENT OF MATERIAL THICKNESS AT FS 508.  REMOVED AND REPLACED LONGERON 30 FROM FS 503 TO FS 520 IAW DC9 SRM 51-40-4 AND SRM 51-30-05.  N/R NR 027A1/0220.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE FORWARD BAY FRAME AT FS 560 HAS CORROSION BETWEEN 26R AND 28L.  FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-03-02, SRM 51-30-1, SRM 51-30-2, AND SRM 51-30-5.  N/R NR 027A1/0057 AND 0058.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA FOUND INSIDE THE MAIN CABIN AT FS 718, LONGERON 19 FRAME(RT) FITTING IS CRACKED FWD AND AFT SIDES, ONE 1 INCH FWD AND ONE 1 INCH AFT.  FABRICATED AND INSTALLED REPAIRS IAW DC9SRM 51-10-3, SRM 51-30-01, SB53-131 AND D.A.C. DWG 5935650.  N/R NR 027A1/0201 AND 0202.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE REPAIR AT FS 125 TO FS 157 IS A NON-STANDARD REPAIR.  FABRICATED AND INSTALLED NEW SKIN FILLERS AND DOUBLERS IAW DC9 SRM 53-04, FIG 12B, AND SRM 51-20-0.  N/R NR 027A1/0234.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE MAIN CABIN DOOR BRACKET CRACKED JUST AFT OF INTERNAL DOOR HANDLE SHAFT AT OUTER SKIN ATTACHMENT.  FABRICATED AND INSTALLED A NEW BRACKET IAW DC9 SRM 51-10-3, SRM 51-10-2A, AND SRM 52-01.  N/R NR 027N1/0235


REMARKS:
UPON A SCHEDULED INSPECTION A AERO CORP IN LAKE CITY, FLORIDA, THE EXTERNAL SKIN WAS FOUND WITH NUMEROUS DENTS, FROM FS237 TO FS 541, FROM LONGERON 17R TO LONGERON 25R.  REMOVED DAMAGED SECTION OF SKIN.  FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DC9 SRM 53-04, SRM 51-30-2, AND SRM 51-20-0.  N/R NR'S 027N1/0399, 0400, 0401, 0403, 0404, 0405, 0406, 0407, 0408, AND 0409.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE MAIN CABIN COMPARTMENT AFT PRESSURE BULKHEAD ATTACH ANGLE IS CRACKED AT APPROXIMATELY 10 O'CLOCK POSITION, RT SIDE.  FABRICATED AND INSTALLED PRESSURE BULKHEAD REPAIRS IAW DC9 SRM 53-05-89.  N/R NR 927N1/0454.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 25L AT FS 218.0 WAS FOUND CORRODED.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIRS IAW DC9, SRM 53-02, FIG 2.  N/R NR 027N1/0072.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A NON-CONFORMING REPAIR WAS FOUND AT FS 541.0.  REMOVEDOLD REPAIR.  FABRICATED AND INSTALLED NEW DOUBLER AND FILLERS IAW AERO CORP E.O. 95-141, REV IR, DATED 4-25-95.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FLOOR BEAM AT FS 180.0, LBL 20.2, WAS FOUND CRACKED.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-05 AND SRM 51-10-2.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A NON-CONFORMING REPAIR WAS FOUND AT FS 832 LONGERON 23R.  REMOVED NON-CONFORMING REPAIR.  FABRICATED AND INSTALLED A NEW DOUBLER AND SHIMS IAW DC9 SRM 53-04 AND AERO CORP E.O. 95-141 REV. IR DATED 4-7-95.  N/R NR 027T1/0003.


REMARKS:
AFT SECTION OF EPL'S AND TAIL COMPARTMENT EMERGENCY LIGHTS INOP.  FOUND WIRING SHORTED BEHIND PANEL IN TAIL COMPARTMENT.  REPAIRED WIRING AND REPLACED FUSES IN BATTERY CHARGER IAW MM CH 33.


REMARKS:
ON DESCENT INTO EWR, NR 2 ENGINE FIRE HANDLE INDICATED A FIRE WARNING.  BOTH BOTTLE DISCHARGED, LIGHT REMAINED ON.  LANDED AT EWR WITHOUT INCIDENT.  FOUND NR 2 ENGINE FIRE SENSE PLUG (D1490) MISSING INSULATION IN PLUG.  SYSTEM CHECKED NORMAL AS PER MM 26-11-00.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACHANGLES LEFT AND RT AT STATION 1076.  REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223.  REF USAA950883.


REMARKS:
LAX - FLT NR 0527 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT.  THE CAPTAIN DECIDED TO RETURN TO LAX.  MAINTENANCE ADJUSTED THE 'NOSE GEAR NOT COMPRESSED' SENSORS.  GEAR RETRACTION AND INDICATION TEST GOOD.  SERVICED NOSE STRUT.  REPLACED THE RIGHT TRACK POSITIONER ACTUATOR.  GEAR RETRACTION TEST PERFORMED GOOD.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND 3 INCH CRACK AT STATION 945 SKIN CLIP AT LONGERON 45L AND 16.  REPLACED SECTIONOF SKIN CLIP PER SRM 51-10-04.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 3 INCH CRACKS IN STATION 945 SKIN CLIPS BETWEEN LONGERON 14R AND 15R AND BETWEEN 15R AND 16R.  REPLACED SECTION OF SKIN CLIPS PER SRM 51-10-04.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND .25 INCH SKIN PUNCTURE STATION 985 AT LONGERON 17 R.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND 6 INCHES BY 8 INCHES TEMPORARY REPAIR STATION 996 AT LONGERON 17R IN SKIN.  REMOVED TEMPORARY REPAIR.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 17.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND 20 INCH BY 2 INCH WEAR IN PILOTS FORWARD AND AFT INBOARD AND OUTBOARD SEAT TRACK STATION 110-140.  INSTALLED DOUBLERS PER DOUGLAS DRAWING 9957855.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND 20 INCH BY 20 INCH FIRST OFFICERS FORWARD AND AFT INBOARD AND OUTBOARD SEAT TRACK WORN STATION 110-140.  INSTALLED DOUBLER REPAIRS PER DOUGLAS DRAWING 995-7855.  (M)


REMARKS:
PIT - DURNIG Q-3/CX-2 INSPECTION, FOUND 1 INCH CRACK AT VERTICAL STABILIZER LEADING EDGE LOWER RT RIB.  INSTALLED DOUBLER REPAIR PER SRM 52-01.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH BY 2 INCH CHAFE IN BELTFRAME AT STATION 1076 LONGERON 20R.  INSTALLED SPLICE REPAIR PER SRM 53-03 FIG 26 - 3 SPLICE.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH BY 2 INCH CHAFE IN BELTFRAME STATION 1059 AT LONGERON 22R.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 26.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACHANGLES LEFT AND RT AT STATION 1076.  REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 3 INCH CRACKS IN SKIN CLIPS AT STATION 637 LONGERON 26L AND STATION 658 LONGERON 25L.  INSTALLED ANGLE DOUBLERS PER SRM 53-03 PAGE 51.   (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AND .5 BY 1 INCH CORROSION AT NUT PLATE BS 737 TO BS 797.FABRICATED NEW FLOOR TRACK AND INSTALLED, REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.(M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 986 BL ZERO TO LBL 20 INCHES ON FLOOR BEAM.  INSTALLED REPAIR DOUBLERS, REPAIRED PER TR 53-10-01A.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORRODED AREA BS 294.5 ON Z ANGLE.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 25 INCH CORROSION AT BS 857 TO BS 787 ON FLOOR SUPPORT ANGLE. INSTALLED NEW SUPPORT ANGLE SECTION INCLUDING DOUBLER AND FILLER.  ALSO, COMPLETED JOGGLE MOD AT STATION 852 SRM 53-00-53 FIG 202.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 13 INCH CORROSION BS 312 RBL 7 INCHES THROUGH RBL 20 INCHES ON FLOOR BEAM T-CAP.  REPAIRED PER SRM 737-400 53-10-51 FIG 206 PAGE 224.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 14 INCH CORRODED BS 328 RBL 28-42 ON FLOOR BEAM.  SPLICED INNEW SECTION OF T-CAP.  REPAIRED 737-300/400 TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 26 INCH BY .5 INCH CORROSION AT BS 328-344 RBL 12 INCHES ON INTERCOSTAL.  REPAIRED AND REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-02 PG 16.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 40 INCHES STATION 344 LBL 24 INCHES - RBL 24 INCHES.  REPLACED SECTION OF T-CAP.  REPAIRED PER TR 53-10-3.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE CORRODED SPOTS (.5 INCH BY 2 INCHES EACH) BS 967, RBL 19, RBL 31,RBL 43 ON FLOOR BEAM.  CUT OUT CORRODED SECTIONS ON AFT SIDE OF UPPER T-CAP, AND INSTALLED REPAIR ANGLES AND FILLERS.  REPAIRED PER SRM 53-30-51 FIG 202.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH BY 1 INCH CORRODED SPOTS BS 312 TO BS 328, RBL 12 CABIN FLOOR INTERCOSTAL.  REPLACED WITH NEW PART, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE .5 INCH BY 1 INCH CORRODED SPOTS BS 294.5 TO BS 312, RBL 12 CABINFLOOR INTERCOSTAL.  INSTALLED NEW PART, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES LBL 16 BS 967 TO BS 987 ON INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 986.5 RBL 18 TO LBL 50.  CUT OFF UPPER FLANGE AND INSTALLED NEW T-CAP.  CORROSION TASK NR C53-107-02, CORROSION LEVEL.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 947 LBL 4 TO RBL 4.  CUT OFF UPPER FLANGE INSTALLED NEW T-CAP.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH SPOTS OF CORROSION Z-ANGLE AT RIGHT AFT SERVICE DOOR SILL.  REPAIRED PER SRM 51-10-2.  CORROSION LEVEL 2, CORROSION TASK NR C53-107-02.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH SPOT OF CORROSION Z-ANGLE AT LEFT AFT ENTRY DOOR SILL. REPAIRED PER SRM 53-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND ONE .5 INCH DIAMETER SPOT OF CORROSION RBL 17 BS 947-BS 967.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORROSION, RBL 16 BS 967 TO 987 INTERCOSTAL.  REPAIREDPER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
FLT NR 31 - EWR-MDW - AFTER TAKEOFF, COULD NOT MAINTAIN CABIN PRESSURE, RT PACK INOP.  AIRCRAFT RETURNED TO EWR.  FOUNDNR 3 ENGINE 13TH STAGE MOD VALVE NOT OPENING WHEN RT PACK TURNED ON.  REMOVED AND REPLACED 13TH STAGE MOD VALVE PER MM 36-12-42.  NO HELP.  FURTHER TROUBLE SHOOTING FOUND BROKEN WIRE ON RT PACK SWITCH.  REPAIRED WIRE AND OPS CHECK OK AS PER MM 21-31-0.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH CRACK RT SIDE OF KEEL BEAM RIB.  INSTALLED ANGLE DOUBLER REPAIRS PER SRM53-03 FIG 12.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND STATION 965 BULKHEAD LOWER PORTION 1 INCH CRACK IN PANEL.  CUT OUT DAMAGED AREAAND FABRICATED NEW PANEL AND INSTALLED PER SRM 53-03 FIG 19.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFED .014 INCH DEEP 5 INCHES BY 1 INCH STATION 813 AT LONGERON 26R UNDERFILLET PANEL.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 37.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFE .014 BY .018 INCH DEEP 5 INCHES BY 1 INCH AT STATION 813 AND LONGERON 26L UNDER FILLET PANEL.  INSTALLED DOUBLERS PER SRM 53-04 FIG 37.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND .75 INCH CRACK IN WEB OF RHS FLAP AT XFS341.  INSTALLED .090 INCH FILLER AND .063 INCH 7075T6 DOUBLER PER SRM 57-01 AND USAIR EA 30788.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND DENT IN FUSELAGE SKIN 3 INCHES BY 2.5 INCHES BY .187 INCH DEEP AT STATION 996 LONG 18R.  INSTALLED .032 INCH TITANIUM DOUBLER PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 20 INCHES BY 20 INCHES STATION 180-200, FROM RT SIDE WALL SUB FLOOR BEAM.  CLEANED CORROSION AND SPLICED IN FILLER AND DOUBLER PER SRM 51-10-2.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STATION 980 LEFT LAV INBOARD SCREW HOLE IN FLOOR BEAM.  CUT OUT DAMAGED AREA AND INSTALLED FILLERS AND DOUBLER PER SRM 53-10-19.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND LEVEL 2 CORROSION AT BELTFRAME 20 INCHES BY 2 INCHES BETWEEN LONGERON 27L AND 27R AT STATION 980 (CORROSION TASK REF C51-53300).  CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-03 PG 4A FIG 2A.  (M)


REMARKS:
PIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH RIGHT LAV STATION 980 FLOOR BEAM AROUND SCREW HOLES IN FLOOR BEAM.  CUT OUT DAMAGE AND INSTALLED FILLERS AND DOUBLERS PER SRM 53-05 FIG 20D.  (M)


REMARKS:
PIT - FLT 1637 - ON TAKEOFF, THE LEFT MAIN OUTBOARD TIRE BLEW.  MOST OF THE TIRE WAS INGESTED INTO THE LEFT ENGINE.  ONAPPROACH BACK TO PIT, THE CREW RECEIVED A GEAR UNSAFE LIGHT.  THE CAPTAIN DID A MISSED APPROACH AND CYCLED THE GEAR.  WITH THE UNSAFE LIGHT STILL ON, CAPTAIN DID A FLYBY OF THE TOWER TO VERIFY THAT THE GEAR WAS DOWN.  FLIGHT LANDED WITHOUTINCIDENT.  MAINTENANCE REPLACED THE NR 2 TIRE AND WHEEL ASSEMBLY (P/N 3910063507) DUE TO A BLOWN CAP.  SPIN CHECK WAS GOOD.  (M)


REMARKS:
PIT - FLT 967 - DURING CLIMB-OUT FROM PIT, CREW RECEIVED A STALL WARNING FAULT MESSAGE.  CREW WAS ADVISED TO RETURN TO FIELD FOR REPAIRS.  NON EMERGENCY AND NO OTHER INCIDENTS.  REPLACED VARIOUS COMPONENTS WITH NO HELP.  FINAL FIX WAS REPLACEMENT OF LEFT A/C CURRENT SENSOR.  RCN 53007.  (M)


REMARKS:
CLT - FLT NR 2416 - EXTERIOR EMERGENCY LIGHTS INOP.  ISOLATED TO BATTERY PACK SUPPLYING THE AFT EXTERIOR LIGHTS.  PRECAUTIONARY PROCEDURE TAKEN, MEL'D SYSTEM.  REPLACED BATTERY PACK.  (M)


REMARKS:
CLT - DURING 'MQ-4' VISUAL CHECK, INSPECTION FOUND A 2 INCH BY 2 INCH CORRODED AREA ON FLOOR BEAM, LOCATED AT BS 312, BETWEEN BL 38LT AND BL 38RT.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  INSTALLED NEW 'T' CAP AND REPAIR ANGLES, STRAPS AND FILTERS REPAIRED BY TRM 53-10-03 AND SRM 51-70-13.  (M)


REMARKS:
UPON A SCHEUDLED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 25L FROM FS 160.0 TO FS 140.0 WAS FOUND CORRODED.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-02, FIGURE 2.  N/R NR 027N1/0093.


REMARKS:
ATL/FLL - FLT 515 - FLIGHT MADE AN AIR RETURN TO ATL DUE TO NR 1 ENGINE HIGH OIL TEMP AT 150 DEGREES.  ENGINE SHUT DOWNIN-FLIGHT AND CAPTAIN DECLARED EMERGENCY.  RAN ENGINE AT POWER, OPS CHECK GOOD AFTER CHECKING ALL WIRING AND CONNECTORS.  CHANGED OIL AND FILTER, NO ABNORMALITIES NOTED.  CLEANED GROUND STUD (906) MM 79-23, 79-33, AND WD 79-33-00.  ALSO, REMOVED AND REPLACED GROUND TERMINAL WITH NEW ONE.


REMARKS:
JAN/ATL - FLT 494 - AUTOPILOT HEADING SELECT SWITCH SHORTED OUT WITH SMOKE IN-FLIGHT.  REPLACED AUTOPILOT CONTROLLER, OPS CHECKED NORMAL PER MM 22-10.


REMARKS:
ATL/DTW  FLT 444 - ELECTRICAL COMPARTMENT DOOR CAME OPEN IN-FLIGHT, RETURNED TO GATE.  SECURED E & E DOOR, OPS CHECKED ANNUNCIATOR LIGHT, OPS CHECKED OK.


REMARKS:
ATH - FLT 880 - DURING CRUISE, SHUT DOWN NR 4 ENGINE, SN 4178, DUE TO LOW OIL QUANTITY.  FOUND OIL LEAK AT ANGLE GEARBOX OIL SCAVENGE LINE ADAPTER, MFG PN 625926.  REPLACED OIL SCAVENGE LINE ADAPTER.  ENGINE LEAK CHECKED AND OPERATION NORMAL.  ENGINE TOTAL TIME:  78,763 HOURS; 13,798 CYCLES.  CHECK C-2 - 10-19-94 - MCI.


REMARKS:
DURING TAKEOFF ROLL APPROACHING 60 KNOTS, EXPERIENCED NUMBER 2 ENGINE POWER DROP.  ABORTED TAKEOFF AND RETURNED TO GATE.  INSPECTED AND REPLACED FUEL SUPPLY LINE FROM P AND D VALVE TO RIGHT NOZZLE.  OPS AND LEAK CHECKED OK PER BOEING M/M.


REMARKS:
EXPERIENCED NUMBER 1 ENGINE OIL PRESSURE DROP AND THE CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT LANDED AT AMAWITHOUT INCIDENT.  REPLACED OIL SEAL, LEAK CHECKED AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON NUT PLATE HOLES ON TOP OF FLOOR BEAM CAP, BS 986.5 RBL 23-37 AND LBL 20-42.  INSTALLED NEW CAP ON FLOOR BEAM (ENTIRE LENGTH).  REPAIRED PER TR 53-10-05.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 40 INCHES CORRODED AREA ON 'Z' ANGLE AT LEFT AFT ENTRY DOOR FRAME STATION 950 TO STATION 999.  REPLACED 'Z' ANGLE AND FABRICATED NEW WEB UNDER ANGLE.  REPAIRED PER SRM 51-10-2.  CORROSION LEVEL 2.  CORROSION TASK NR C53-107-02.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 9 INCH CORRODED AREA ON STRINGER S-28 L STATION 315 TO STATION 324.  SPLICED IN NEW STRINGER, REPAIRED PER SRM 53-00-03, FIG 201.  CORROSION TASK NR C53-202-01.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA AT CABIN BS 986.5 - 992 LBL 36 - LBL ON INTERCOSTAL.  REPLACED INTERCOSTAL, SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
PIT - DURING RON CHECK, FOUND A 2 INCH CRACK AT AFT VENTRAL DOOR LEFT SIDE ABOVE TOP LEFT DOOR STOP.  REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 30.  (M)


REMARKS:
PIT - DURING RON CHECK MAINTENANCE, FOUND A 1.5 INCH CRACK IN THE TOP LEFT CORNER OF THE VENTRAL DOOR JAM.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 29.  (M)


REMARKS:
IND - DURING CX-6 CHECK INSPECTION, FOUND 1 INCH SQUARE AREA OF CORROSION WITH .125 INCH CRACK IN FORWARD CARGO DOOR JAM LOWER PAN.  ACCOMPLISHED DOUBLER REPAIR PER USAIR EA 30892 AND SRM 53-05 FIG NR 44.  (M)


REMARKS:
ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK IN STRINGER CORROSION FOUND UNDER STRINGER 27L AT STATION 967.  REMOVED DAMAGED STRINGER AND SPLICED NEW STRINGER PER SRM 53-10-3.  (M)


REMARKS:
PHL - FLT NR 0803 - ON CLIMB-OUT FROM PHL, PASSING THROUGH 7500, NR 1 ENGINE FAILED.  FLIGHT CREW SHUT DOWN NR 1 ENGINEAND RETURNED TO PHL.  LANDING WAS WITHOUT INCIDENT.  SINGLE ENGINE TIME WAS 10 MINUTES.  MAINTENANCE REPLACED THE LEFT ENGINE ASSEMBLY.  (M)


REMARKS:
DURING SCHEDULED C2/C4 CHECK, FOUND GOUGE UNDER FWD ENTRY DOOR AT AFT CORNER MEASURING 5 INCH BY .250 INCH BY .018 INCHDEEP.  REPAIRED PER SWA RA 1-353-1370.


REMARKS:
DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727D BELOW STRINGER 20L.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED 1/2 C-CHECK, FOUND PREVIOUS FUSELAGE SKIN REPAIR DOUBLER AT AFT ENTRY DOORWAY WITH SEVERAL DISCREPANCIES.  REPAIRED PER SWA RA 1-553-1371.


REMARKS:
DURING SCHEDULED 1/2 C CHECK,  FOUND FUSELAGE SKIN CRACKED AT LEFT SIDE, 2ND PASSENGER WINDOW FROM FRONT AT TOP FWD CORNER RIVET HEAD.  REPAIRED PER SWA RA 1-253-1372 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 C-CHECK, FOUND WEB GOUGED AND CRACKED FWD OF AFT CARGO DOOR AT BS 794.3 FROM S25R TO 24R.  REPAIRED PER SWA RA 1-553-1371.


REMARKS:
DURING SCHEDULED CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST CRACKED .156 INCH.  REPAIRED PER SWA RA 1-A53-1156.


REMARKS:
MCI - DURING CLIMB, LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AND LEFT MAIN LANDING GEAR UNSAFE RED LIGHT ILLUMINATED.  VERIFIED LANDING GEAR WAS DOWN, AND DOOR REMAINED OPEN.  FOUND LEFT MAIN LANDING GEAR DOOR ACTUATOR BUSHING, MFG P/N S2210370P9-157, MISSING.  INSTALLED BUSHING AND LANDING GEAR AND LANDING GEAR DOOR OPERATION CHECKED NORMAL.


REMARKS:
MCI - DURING C-CHECK, FOUND TWO CRACKS EACH WERE APPROXIMATELY ONE INCH LONG, IN LEFT MLG WHEELWELL CEILING PRESSURE DECK AFT OUTBOARD CORNER, FORWARD OF 590 BULKHEAD, LBL 56 AND 58.  REPAIRED BY INSTALLING DOUBLER PER ARA 9372.  TOTAL CYCLES 42,177.


REMARKS:
JFK - DURING CRUISE SMOKE AND ELECTRICAL ODOR EMITTED FROM AFT GALLEY E-1 SERVING CART CONTROLLER, MFG P/N B00678-1.  TURNED OFF CONTROLLER AND OPENED CIRCUIT BREAKERS.  REPLACED THE E-1 CART CONTROLLER AND OPERATION CHECKED NORMAL.


REMARKS:
JFK - DURING CRUISE AFT GALLEY SERVING CART NR 4, EMITTED SMOKE AND ELECTRICAL ODOR.  TURNED OFF AND DISCONNECTED CART,MFG P/N 88801-1.  FOUND MALFUNCTIONING HEATING PLATES.  REPLACED SERVING CART AND OPERATION CHECKED NORMAL.


REMARKS:
MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN APPROXIMATELY .030 TO .015, STRINGER 17R TO 19R, AND STRINGER 17L TO 19L, FS 720E TO 720F, ALSO WORN APPROXIMATELY .040, STRINGER 19L.  REPAIRED PER ARA 9354.  TOTAL CYCLES 24,723.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266.  SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4.  TOTAL CYCLES 73,957.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996.  REMOVED AND REPLACED LONGERON SECTION PER SRM51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.  TOTAL CYCLES 73,957.


REMARKS:
MCI - DURING OP-15, FOUND RIGHT WING RS AFT FLAP CENTER HINGE FITTING MOUNT AREA REAR SPAR WEB, CRACKED .75 INCH IN EYEBROW AT UPPER OUTBOARD HOLE.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER SERVICE BULLETIN 57-179 AND DRAWING J060272-502.  TOTAL CYCLES 78,686.


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND CORROSION ON LONGERON 23L FS 965 WHICH IS BEYOND THE SRM LIMITS 53-01.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED REPAIR MEMBER AND SPLICES IAW DC9-SRM 53-02 FIG 5.  (M)


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND SEVERAL CORRODED SPOTS AROUND THE AFT CARGO DOOR LOWER FRAME.  REMOVED DAMAGED SECTION.  FABRICATED AND INSTALLED A NEW SECTION AND SPLICES IAW DC-9 SRM 53-30-2.  NR 027N1-0064.


REMARKS:
STL - DURING CLIMB AFTER LANDING GEAR RETRACTION, HAD SEVERE VIBRATION FROM NOSE GEAR AREA.  CYCLED LANDING GEAR AND VIBRATION CONTINUED.  FOUND LEFT NOSE LANDING GEAR DOOR STOP CABLE, MFG P/N 3926528-1, TENSION LOW.  RIGGED CABLE TENSION AND NOSE LANDING GEAR AND DOORS CHECKED NORMAL.


REMARKS:
STL - DURING CRUISE SHUT DOWN NR 1 ENGINE, S/N 4165, DUE TO START VALVE LIGHT ILLUMINATED.  FOUND START VALVE PRESSURE SWITCH, MFG P/N 21SN41-1B, WITH INTERNAL MALFUNCTION.  REPLACED START VALVE PRESSURE SWITCH AND START VALVE, MFG P/N 726574-7.  ENGINE OPERATION AND LEAK CHECK NORMAL.


REMARKS:
ATL-TPA - FLT 25 - AFTER TAKEOFF NR 3 ENGINE STRUT OVERHEAT LIGHT ON, LIGHT GOES OFF AT IDLE, COMES BACK AFTER POWER RESTORED, ATB TO ATL.  FOUND DUCT FLANGE ON DUCT ASSY FROM NR 3 ENGINE BLEED S/O VALVE CRACKED.  REMOVED AND REPLACED DUCTASSY AS PER MM 36-00-1.  OPS AND LEAK CHECK OK ON ENG RUNUP.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND DENT IN SKIN 1.25 INCH BY 1.25 INCH BY .108 DEEP AT STATION 221 BETWEEN LONGERON 15L AND 16L.  CUT OUT DAMAGE AND INSTALLED CLASS 1 REPAIR DOUBLER PER SRM 53-04 FIG 38 SHEET NR 21 VIEW 1.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND CRACK .125 INCH LONG IN SKIN AT STATION 1437 LONGERON 2L.  STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER US AIR EA NR 30625.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH LONG CRACK STATION 1307 SKIN CLIP LONGERON 16L.  SPLICED IN NEW SECTION OF SKIN CLIP PER SRM 53-03.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND ONE .5 INCH LONG CRACK IN SKIN CLIP STATION 1307 LONGERON 16R.  SPLICED IN NEW SKIN CLIP PER SRM 53-03.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH AND 1.5 INCH CRACK IN LEFT AND RIGHT SADDLE SUPPORT FITTING FORWARD END OF KEEL STRUCTURE, STATION 940.  FABRICATED AND INSTALLED KEEL SADDLE SUPPORT FITTING PER SRM 53-05 FIG 81.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND .5 INCH DIAMETER HOLE AT STATION 1380 LONGERON 6L IN TAIL INTERIOR BULKHEAD.  REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 3.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND GOUGE .014 INCH DEEP AT STATION 1309-1322 ABOVE LONGERON 20R.  BLENDED GOUGE TO .016 INCH AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 VIEW G.  (M)


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND A 3.5 INCH CRACK IN THE RUDDER RIB NR 4 VERTICAL CHANNEL.  INSTALLED DOUBLER REPAIR PER SRM 55-02-07 FIG 3.  (M)


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND A .034 INCH DEEP BY 1.5 INCH LONG GOUGE IN MAIN ENTRANCE DOOR APERTURE FRAME JUST FORWARD OF INTERMEDIATE LEVER.  INSTALLED DOUBLER REPAIR PER SRM 53-02-16 FIG 1.  (M)


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND SKIN BUCKLED AND CRACKED JUST FORWARD OF APU EXHAUST.  INSTALLED DOUBLER REPAIR PER SRM 53-02-04 FIG 1.  (M)


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN FORWARD CARGO AFT FRAME AT DOOR HOLD OPEN ROD SUPPORT.  INSTALLED DOUBLER REPAIR PER SRM 53-02-16.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 2 CRACKS ONE .0625 INCH AND ONE .1875 INCH IN FRAME STATION 1463 LEFT SIDE DORSAL FIN ATTACH ANGLE.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 23B.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CORROSION IN MED STATION 200 BOTTOM LEFT AFT DOOR JAMB.  CUT OUT CORRODEDSECTION OF JAMB AND INSTALLED DOUBLER REPAIR PER USAIR EA 308 AND SRM 53-05 FIG 55.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A 1 INCH CRACK IN TOP KEEL BEAM 'T' ANGLE ON HORIZONTAL LEG AT STATION 985.  SPLICED IN NEW SECTION OF ANGLE AND DOUBLER PER USAIR EA 30834.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A LIGHTNING STRIKE LEAVING A .020 INCH PIT AT FUSELAGE SKIN STATION 636 BETWEEN LONGERON 9R AND 10R.  REMOVED DAMAGE AND INSTALLED FILLER AND INTERNAL DOUBLER REPAIR PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .125 INCH CRACK IN LONGERON 3L AT STATION 160.  SPLICED IN NEW SECTION OFLONGERON PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 1 INCH CRACK IN STATION 825 TO 845 LONGERON 18R CUSP WEB.  REPLACED SECTION OF CUSP WEB PER SRM 53-05 FIG 27.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SKIN CLIP STATION 1459 BETWEEN LONGERON 2R AND 3R.  MFG NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 28.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CRACK AT SKIN CLIP .375 INCH LONG AT STATION 1459 BETWEEN LONGERON 2L AND3L.  MFG NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 28.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT RIGHT INBOARD SEAT TRACK AT BOTTOM INBOARD FLOOR ATTACH ANGLE AT STATION FS-205 (PREVIOUSLY REWORKED) CORROSION TASK REF C46-53305.  REMOVED CORROSION AND SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK IN TEMPORARY REPAIR ON WING LE AT INBOARD AND OUTBOARD EDGE OF FUEL SERVICE PANEL IN SKIN.  REMOVED TEMP REPAIR AND STOP DRILLED CRACKS.  INSTALLED DOUBLER REPAIR PER SRM 57-06B. (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SUPPORT ANGLE LEFT OF CENTER UNDER RADAR SUPPORT SHELF STATION 37 BULKHEAD HORIZONTAL ANGLE.  INSTALLED DOUBLER REPAIR PER SRM 53-01.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 3 INCH BY 4 INCH AREA OF CORROSION (LEVEL 1) AT FITTING AT AFT LOWER CORNER OF AIR STAIR DOOR STATION 200 LONGERON 21L (PREVIOUSLY REWORKED).  CORROSION TASK NR REF C45-53301.  INSTALLED NEW FITTING P/N 109-7172.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CUSP MEMBRANE CRACKED IN 2 PLACES BOTH 1 INCH LONG AT STATION 1287 LEFT.MFG NEW CUSP MEMBRANE PER SRM 53-05 FIG 79.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CUSP MEMBRANE CRACKED 1 INCH LONG STATION 1250 RIGHT SIDE.  MFG CUSP MEMBRANE PER SRM 53-05 FIG 79.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .375 INCH CRACK IN FITTING AT STATION 988 INSIDE HEEL ABOVE AFT END OF DOOR HINGE.  INSTALLED DOUBLER REPAIR PER SRM 53-01.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CRACK .25 INCH LONG AT BOTH ATTACH POINTS STATION 160 LONG 4L.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK AT LONGERON ATTACH POINTS TO FRAME STATION 160 LONG 3L.ACCOMPLISHED SPLICE TYPE REPAIR PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 2 CRACKS .25 INCH LONG IN BELTFRAME AT STATION 1322 AT LONGERON 17R.  REPLACED SECTION OF FRAME AND INSTALLED DOUBLERS PER SRM 53-03 FIG 31.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK RIGHT INBOARD WEB LEADING EDGE TO HORIZONTAL STABILIZER FROM SPAR.  INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 5.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 948 LEFT SIDE WINDOW PAN.  INSTALLED DOUBLER TYPE REPAIR PER USAIR TYPICAL REPAIR 53-50-06.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 929 LEFT SIDE WINDOW PAN.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-50-06.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 888 LEFT WINDOW PAN.  INSTALLED DOUBLER REPAIR PERUSAIR TYPICAL REPAIR 53-50-06.  (M)


REMARKS:
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON BELTFRAME 1287 BETWEEN LONGERON 22L AND 23L (CORROSION TASK RED C57-53301).  ACCOMPLISHED REPAIR TO BELTFRAME PER SRM 53-03 FIG 30.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT STATION 1322 RIGHT LAV FLOOR BEAM.  CORROSION TASK NR C58-53308.  CUT OUT CORRODED AREA AND INSTALLED FILLER, ANGLE AND DOUBLERS PER USAIR TYPICAL REPAIR 53-10-19.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT STATION 1338 RIGHT LAV FLOOR BEAM CORROSION TASK NR C58-53300.  SPLICED IN NEW SECTION OF FLOOR BEAM PER USAIR TYPICAL REPAIR 53-10-14.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 4 INCH BY 2 INCH AREA OF CORROSION PREVIOUSLY REWORKED UPPER CUSP ANGLE AT APPROX STATION 180.  REMOVED DAMAGED AREA FABRICATED NEW CUSP, INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 55 AND USAIR EA 30801.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 2 INCH CRACK RIGHT SIDE OF VERTICAL FIN DRAG ANGLE AT STATION 1495.  CUT OUT DAMAGED AREAS AND INSTALLED A SPLICE REPAIR PER SRM 53-05 FIG 23A.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND CRACK .75 INCHES LONG AND CREASE .055 DEEP AT STATION 522 BETWEEN LONGERON 21R AND 22R FUSELAGE SKIN.  CUT OUT DAMAGED AREA AND INSTALLED EXTERIOR DOUBLER AND INTERIOR FINGER DOUBLER PER SRM 53-04 FIG 12B.  (M)


REMARKS:
PIT - DURING Q-1/CD-6 CHECK INSPECTION, FOUND GOUGE .015 BY 1.75 INCHES LONG AT STATION 755 LONGERON 15R.  BLENDED GOUGE, DYE CHECKED AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW E.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1282 TO 1300 LONGERON 30.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 14.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1300 TO 1338 LONGERON 29L.INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02 FIG 14.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND PUNCTURE IN APU SHROUD ENCLOSURE SKIN.  MFG AND INSTALLED REPAIR DOUBLER PER SRM 53-01 PG 2.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND TWO .75 INCH LONGERON CRACKS AT STATION 237 AND 256 LONGERON 17L.  INSTALLED SPLICE REPAIR PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT -DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN SKIN CLIP STATION 1307 LONGERON 16R.  MANUFACTURED SKIN SLIP AND INSTALLED PER SRM 51-01.  (M)


REMARKS:
PIT - DURING SCHEDULED STRUCTURAL VISIT (SIP), FOUND A 1.5 INCH CRACK IN WEB BETWEEN STATION 2220 AND 3050 AT BEND LINEABOVE CONNECTION ANGLES.  (VISUAL INSPECTION VERIFIED BY HFEC) SIP REF 53-10-19.  INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 29.  (M)


REMARKS:
ROA - DURING 'FULL C' CHECK VISUAL INSPECTION, FOUND 6 INCH BY 3 INCH DENT BETWEEN STATION 1040 AND STATION 1064 LOWER RIGHT AFT FUSELAGE.  INSTALLED DOUBLER, REPAIR DOCUMENT SRM 53-00-01 PAGE 204.  (M)


REMARKS:
DURING SCHEDULED B/C CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST CRACKED .156 INCH.  REPAIRED PER RA 1-A53-1156.


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND 2 DENTS .125 INCH DEEP IN FUSELAGE SKIN ABOVE LAV SERVICE DOOR RIGHT SIDE.  INSTALLED DOUBLER REPAIR PER SRM 53-02-02.  (M)


REMARKS:
PIT - DURING FC-6 CHECK INSPECTION, FOUND .125 INCH CRACK IN RUDDER RIB NR 5 BOTTOM ANGLE BOTH SIDES.  INSTALLED DOUBLER REPAIR PER SRM 55-02-07.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND 14 INCH BY 24 INCH AREA OF DELAMINATION AT STATION 24011 LEFT FUSELAGE SKIN.  INSTALLED TITANIUM DOUBLER REPAIR PER USAIR EA 30650.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND 14 INCH BY 24 INCH AREA OF DELAMINATION AT STATION 24011 AND 24611 RIGHT SIDE FUSELAGE SKIN.  INSTALLED TITANIUM DOUBLER REPAIR PER USAIR EA 30650.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND A DENT .085 INCH DEEP LEFT SIDE FUSELAGE STATION 5805.  INSTALLED EXTERNAL DOUBLER PER SRM 53-00-02 PG 201 AND 51-70-06 PG 201.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SKIN AT STATION 1380 RIGHT SIDE BETWEEN LONGERON 13R AND14R.  CUT OUT CRACK AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-04 FIG 18.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND GOUGE .065 BY 1 INCH LONG STATION 1309 LONGERON 29L.  NDT CHECK FOR CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH CRACK STATION 937 LEFT AT KEEL TO SADDLE SUPPORT.  FABRICATED SUPPORT CHANNEL AND INSTALLED PER SRM 53-05 FIG 81.  (M)


REMARKS:
CLT - DURING DROP-IN CHECK INSPECTION, VISUALLY FOUND A 5 INCH BY 2 INCH CORRODED AREA LOCATED AT S-25RT FROM STATION 352 TO STATION 357.  DROP IN AIRCRAFT.  CORROSION LEVEL 2.  INSTALLED REPAIR ANGLES.  (M)


REMARKS:
CLT - FOUND TWO CRACKS APPROXIMATELY 4 INCHES LONG LOWER FUSELAGE SKIN, 1 INCH LEFT AND 1 INCH RIGHT OF BL-0, STATION 727 D DIRECTLY BELOW VHF ANTENNA.  VISUALLY INSPECTED.  INSTALLED DOUBLER.  (M)


REMARKS:
FLT NR 80 - ATL - DURING FLAP RETRACTION, OUTBOARD FLAPS STAYED AT 2 DEGREES WHEN FLAPS WERE POSITIONED TO UP.  CYCLED FLAPS AND OUTBOARDS STAYED AT 2 DEGREES.  RETURNED TO ATL.  INSPECTED FLAPS, NO ABNORMALITIES FOUND.  REMOVED AND REPLACED OUTBOARD FLAP INDICATOR AND TESTED AS PER MM 27-52-13.  CHECKED OK, RESET AND SAFETIED FLAP OVERRIDE SWITCH.  (M)


REMARKS:
STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND.  CYCLED LANDING GEAR AND NOSE LANDING GEAR EXTENDED NORMAL.  JACKED AIRCRAFT AND OPERATED NOSE LANDING GEAR SEVERAL TIMES.  NOSE LANDING GEAR OPERATIONCHECKED NORMAL, NO MALFUNCTION FOUND.  (M)


REMARKS:
STL - DURING CLIMB SHUT DOWN NR 1 ENGINE, S/N 1537, DUE TO STRUT OVERHEAT.  FOUND 13TH STAGE AIR LEAK AT WING ANTI-ICE VALVE.  REPLACED GASKETS, MFG P/N 60023-1, AT 13TH STAGE VALVE.  PERFORMED HIGH POWER RUNUP LEAK CHECK AND OPERATION WASNORMAL.  (M)


REMARKS:
STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, THE GREEN DOWN AND LOCKED INDICATION DID NOT ILLUMINATE.  VISUALLY CHECKED, LANDING GEAR WAS DOWN AND LOCKED.  FOUND MASTER TEST DIM CAUTION LIGHT CARD MALFUNCTIONING, MFG P/N 69-48272-2.  REPLACED MASTER TEST DIM CAUTION CARD AND LANDING GEAR INDICATION SYSTEM CHECKED NORMAL.  (M)


REMARKS:
SHORTLY AFTER TAKEOFF, NUMBER 2 ENGINE FAILED WITH ACCOMPANYING LOUD BANG AND SEVERE VIBRATION.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 2 ENGINE ASSEMBLY.


REMARKS:
IN FLIGHT, EXPERIENCED NUMBER 4 L/E SLAT UNCOMMANDED DEPLOYMENT.  AIRCRAFT DIVERTED TO LAS AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 4 L/E SLAT ACTUATOR.


REMARKS:
STL - DURING CLIMB, SHUT DOWN NR 3 ENGINE, S/N 1502, DUE TO ALL PARAMETERS WENT HIGH.  FOUND ENGINE FUEL CONTROL SHAFT SHEARED.  REPLACED FUEL CONTROL, MFG P/N 378201-7.  GROUND RUNUP AND OPERATION CHECKED NORMAL.  (M)


REMARKS:
DEN - FLT 427 - DURING DESCENT, SHUT DOWN LEFT ENGINE DUE TO SPOOLED DOWN WITH INCREASING EGT.  FOUND METAL PARTICLES IN TAILPIPE.  CHANGED ENGINE, S/N 1205.  ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  21,594 HOURS; 10,979 CYCLES.  OP-15 - 12-3-94 - MCI.  INVESTIGATION INTO ENGINE S/N 1205 SPOOL DOWN REVEALED SEVENTH STAGE COMPRESSOR BLADE, MFG P/N 809407, FRACTURED DUE TO IMPACT CAUSING DOWNSTREAM COMPRESSOR DAMAGE.  ENGINE WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
CLT - DURING AN UNSCHEDULED MAINTENANCE CHECK INSPECTION, FOUND A DEEP CUT BY TOOLING WHEEL LOCATED AT FRAME 360, S-4 RT TO S-4 LT.  INSTALLED REPAIR DOUBLE SECTION.  (X)


REMARKS:
CLT - FLT NR 944 - DIVERTED TO CLT DUE TO 2 INCH SPREAD IN THE THROTTLE POSITION.  FOUND 8TH AND 13TH STAGE DUCTS CLAMPLEAKING.  RETORQUED THE SAME.  RAN ENGINE.  LEAK CHECKED CLAMPS.  CHECKED GOOD.  (M)


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CRACKED AT BS 344, BL 0 AT UPPER FWD CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER CORNER, BS 294.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING CLIMBOUT, NUMBER 1 ENGINE WAS SHUTDOWN DUE TO START VALVE OPEN LIGHT ILLUMINATING.  AIRCRAFT RETURNED TO BHM ANDMADE AN UNEVENTFUL LANDING.  REPLACED START VALVE AND START VALVE PRESSURE SWITCH PER BOEING MAINTENANCE MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND NR 1 STRINGER WEB CRACKED AT BS 303.9 LEFT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING CLIMBOUT, EXPERIENCED A-SYSTEM HYDRAULIC PRESSURE LOSS.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND REPLACED NUMBER 2 ENGINE REVERSER PRESSURE LINE AND HYDRAULIC CASE DRAIN FILTERS PER BOEING MAINTENANCEMANUAL.


REMARKS:
FLL/ATL - FLT 134 - AFTER STARTING APU, SMOKE/FUMES STARTED TO ENTER THE AFT END OF THE CABIN, SHUT DOWN APU.  PLACED ON MEL LOG PAGE NR 3586, ATA 49-01.


REMARKS:
DURING D-CHECK, FOUND PRESSURE BULKHEAD WEB CHAFE DAMAGE AT BS 727 BL 0 WL 185.  REPAIRED PER EWO 95-0595 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND STRINGER 3L CORRODED UNDER FASTENER BETWEEN BS 380 AND 400.  ALSO, FOUND S11R CORRODED BETWEEN BS478 AND 484.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND CORROSION BETWEEN S4 AND 6R ON AFT FACE AND O/B FLANGE O/B SURFACE OF FRAME INCLUDING STRINGER CLIP.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND FUSELAGE SKIN SCRATCHED AND DENTED AT BS 183 LBL 2 TO RBL 9, FWD OF NOSE BAY ACCESS DOOR.  ALSO, SKIN DENTED AT BS 904, ABOVE S25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND STRINGER 4R AND 4L SPLICE JOINT CRACKED AT BS 907.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND T-CHORD CRACKED BETWEEN BS 178 TO 180, WL 197 LBL 24.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND STRINGER S15L CRACKED AT BS 787.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND FUSELAGE FRAME AND SHEAR TIE CORRODED AT BS 747, RBL 6 TO 9 WL 148.  ALSO, SHEAR TIE AT BS 727A BETWEEN 21 AND 22L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 7 TO RBL 36 WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND THREE HOLES IN KEEL BEAM LOWER FLANGE AND RADIUS AT BS 727+16, RBL 7.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND FUSE FRAME CRACKED AT BS 597, BL 71 WL 202 ON BOTH RT AND LT SIDES.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING D-CHECK, FOUND CHAFING DAMAGE ON LOWER O/B FLANGE OF KEEL BEAM BS 710 TO 727, LBL 7 WL 149.  REPAIRED PER EWO 95-0596 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
THE GALLEY SLIDE SPOT LIGHT WOULD NOT COME ON.  REMOVED AND REPLACED EXIT CHUTE LIGHT BATTERY PACK LEFT AND RT DOORS.  (M)


REMARKS:
FLT NR 572 - ATL-MCI - RECEIVED AN UNSAFE NOSE GEAR INDICATION AFTER HANDLE WAS LOWERED FOR LANDING.  WHEN AIRSPEED REDUCED BELOW 160 KTS FOR APPROACH, NOSE GEAR SAFE INDICATION WAS OBTAINED.  FLIGHT OFFICER VISUALLY CONFIRMED DOWN.  CLEANED CONNECTOR ON DOWNLOCK SWITCH, JACKED AIRCRAFT, PINNED GEAR SWING NOSE GEAR SEVERAL TIMES, COULD NOT DUPLICATE.  OK TOCONTINUE SERVICE, REMOVED GEAR PINS.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AROUND SEVERAL SCREW HOLES RIGHT LAV FLOOR REAR STATION 1322.  CORROSION TASK NR C58-53300.  REMOVED CORROSION AND INSTALLED DOUBLER AND STRAP PER USAIR TYPICAL REPAIR 53-10-19.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION STATION 1338 FLOOR BEAM NR 18, 24 INCHES FROM RIGHT SIDE WALL AT SCREW HOLES.  CORROSION TASK NR C58-53300.  REPLACED ANGLE FROM RBL 12 INCHES TO OUTBOARD SIDE PER USAIR TYPICAL REPAIR 53-10-14.`


REMARKS:
PHF - FLT NR 0121 - WHEN THE GEAR WAS EXTENDED THE NOSE GEAR FAILED TO GIVE A GREEN LIGHT.  THE CAPTAIN PULLED OFF THE PATTERN AND RECYCLED THE GEAR.  AGAIN NO NOSE GEAR GREEN LIGHT.  AT THAT TIME THE CREW CHECKED THE VISUAL INDICATORS ANDDETERMINED THE GEAR WAS DOWN AND LOCKED.  THE EMERGENCY EQUIPMENT WAS CALLED OUT.  THE FLIGHT LANDED WITH NO FURTHER INCIDENT AND TAXIED TO THE GATE ON ITS OWN POWER.  MAINTENANCE CHECKED THE NOSE GEAR DOWNLOCK POSITION SWITCH AND RELAMPEDTHE NOSE GEAR DOWNLOCK INDICATOR.  OPERATIONS CHECKED NORMAL.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND .75 INCH CRACK FORWARD UPPER CORNER OF WINDOW FRAME AT STATION 886 LONG 12R.  STOP DRILLED CRACK AND REPAIRED PER USAIR TYPICAL REPAIR 53-30-06.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND .5 INCH CRACK IN LOWER FORWARD CORNER OF WINDOW DOUBLER AFT OF STATION 846 LEFT SIDE.  STOP DRILLED CRACK AND REPAIRED PER USAIR TYPICAL REPAIR 53-30-06.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND 1.25 INCH CRACK IN STRINGER OF FWD INBOARD LEADING EDGE IN RADIUS JUST FWD OF LEFT MLG ATTACH FITTING.  STOP DRILLED CRACK AND INSTALLED STAINLESS STEEL DOUBLERS PER SRM 52-05.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT STATION 237 LONGERON 29R.  REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND .375 INCH CRACK AT STATION 160 UPPER FORWARD CORNER OF FORWARD AIRSTAIR DOOR.INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-05 FIG 57A SHT 6 VIEW G.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND 1 INCH CRACK LEFT DRAG ANGLE STATION 1474 (CANTED FRAME).  STOP DRILLED CRACK AND INSTALLED SKIN AND DOUBLER REPAIR PER SRM 53-05 FIG 23B CONF 7007.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK IN STRINGER NR 68 RIGHT SIDE 4 INCHES AFT OF FRAME 3870.  INSTALLED DOUBLER REPAIR PER SRM 51-70-06 FIG 202.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED BETWEEN LEFT STUBWING UPPER AND LOWER CONNECTION ANGLES.  AREA APPROXIMATELY 10 INCHES BY 24 INCHES AT STATION 24011 TO STATION 24611.  CUT OUT DAMAGED AREA INSTALLED DOUBLER REPAIR PER USAIR EA NR 30990A.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED APPROXIMATELY 10 INCH BY 24 INCH AREA BETWEEN RIGHT STUB WING UPPER AND LOWER CONNECTION ANGLE FROM STATION 24011 TO STATION 24611.  CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER USAIR EA NR 30990A.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK BETWEEN STATION 8305 AND STATION 8805 AT STRINGER NR 2 FITTING.  INSTALLED DOUBLER ANGLE PER SRM 53-00-02.  (M)


REMARKS:
CLT - DURING AN UNSCHEDULED MAINTENANCE INSPECTION, FOUND A PUNCTURE, TEAR AND A DENT 7.3125 INCH BY 19.75 INCH BETWEENS18L AND S16L FROM FRAME BS 278 TO 297.  INSTALLED INTERIM DOUBLER.  (M)


REMARKS:
CLT - DURING A CMV-1 INSPECTION, FOUND A 2 INCH BY 3.5 INCH TEAR AND DENT AT NR 2 NACELLE STRUT RIGHT SIDE PP STATION 134.5.  INSTALLED DOUBLER, FILLERS, SKIN.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND CORROSION AT ATTACH ANGLE NR 2 RADIO RACK FLOOR PANEL.  FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-12-10.  (M)


REMARKS:
PHL - FLT NR 823 - FOUND FIRST CLASS EMERGENCY LIGHT WIRING INOPERATIVE.  MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE IN THE FIRST CLASS CLOSET.  (M)


REMARKS:
FLT NR 238 - DFW-ATL - FLIGHT ATTENDANTS ON CLIMB-OUT REPORTED SMOKE IN THE CABIN.  AIRCRAFT RETURNED TO DFW.  MAINTENANCE CHECKED SYSTEMS AND FOUND RIGHT PACK TEMPERATURE CONTROL VALVE AT FAULT, PLACED ON MEL LOG, PAGE 4928.


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LOWER AFT ANGLE AT PRESSURE BULKHEAD CORROSION APPROXIMATELY 6 INCHES BY 36 INCHES LOWER AFT FACE FROM LONGERON 25L-25R.  CORROSION TASK NR C57-53300.  SPLICED IN NEW ANGLE PER USAIR TYPICAL REPAIR 53-30-10.  (M)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK LEVEL 1 CORROSION 80 INCHES LONG, STATION 1220 TO STATION 1309.  CORROSION TASK NR C58-53302 PREVIOUS REWORKED.  REPLACED SECTION OF SEAT TRACK PER SRM 53-05 PG 8L FIG 4F.  (M)


REMARKS:
FLT NR 40 - TPA-EWR - DIVERTED TO ATL, NR 3 ENGINE LOW OIL PRESSURE FILTER BYPASS LIGHT CAME ON IN FLIGHT.  BURNED OUT TWO BULBS, ALL OTHER ENGINE INDICATIONS NORMAL.  PERFORMED PRECAUTIONARY SHUTDOWN.  FORTY MINUTES OF WINDMILL AT 30 PSI. CLEANED OIL IN CANNON PLUG OF DIFFERENTIAL PRESSURE SWITCH.  REMOVED AND REPLACED MAIN OIL FILTER, NO DEBRIS OR CONTAMINATION FOUND, OIL LIGHT OPS OK PER MM 79-00.  RAN ENGINE, OPS AND LEAK CHECK OK.  (M)


REMARKS:
JAX - FLT NR 8645 - RETURN TO JAX DUE TO THE MAIN CABIN DOOR NOT BEING CLOSED PROPERLY.  THE CAPTAIN DID NOT RECEIVE ANY LIGHTS IN THE COCKPIT PRIOR TO DEPARTURE THAT THE DOOR WAS NOT CLOSED.  MAINTENANCE INSPECTED THE DOOR.  NO DEFECTS NOTED.  (M)


REMARKS:
LGA - FLT NR 0152 - NR 1 ENGINE LOSING OIL QUANTITY ON CLIMB-OUT FROM LGA.  FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO LGA.  SET WAS APPROXIMATELY 10 MINUTES.  MAINTENANCE REPLACED LEFT ENGINE N2 GEAR BOX ASSEMBLY.  (M)


REMARKS:
IND - FLT NR 673 - DIVERTED TO IND DUE TO LOSS OF THE NR 2 VOR.  MAINTENANCE REPLACED THE NR 2 NAV RECEIVER.  VOR GROUND CHECKED GOOD.  (M)


REMARKS:
EXPERIENCED NR 1 ENGINE OIL HIGH OIL TEMP.  CREW PERFORMED ENGINE SHUT-DOWN CHECK LIST.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  INSPECTED ENGINE.  REPLACED OIL TEMP INDICATOR, OIL TEMP BULB, OIL, AND MAIN OIL FILTER.


REMARKS:
ON APPROACH, AFTER GEAR EXTENSION, LEFT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED.  RECYCLED GEAR, WITH NO HELP.  MANUALLYEXTENDED GEAR AND GREEN OK LIGHT ILLUMINATED.  LANDED AT DAL WITHOUT INCIDENT.  REPLACED LEFT MAIN GEAR UPLOCK ACTUATORAND PERFORMED RETRACTION, OK PER BOEING M/M.


REMARKS:
APU FIRE DETECTION WARNING LIGHT ILLUMINATED.  CREW EXPENDED FIRE BOTTLE.  LANDED AT HOU WITHOUT INCIDENT.  INSPECTED AREA AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION.  REPLACED FIRE BOTTLE AND CONTINUED PER MEL 26-7.  DURING RON, REPLACED APU TAILPIPE FIRE LOOP PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, NR 2 KRUGER FLAP INDICATED NO RETRACTION.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  INSPECTED AREA.  REPLACED FLAP FULL UP PROXIMITY SENSOR PER BOEING M/M.


REMARKS:
DURING CLIMBOUT AT 31,000 FEET, NOTED FIRST OFFICER'S SLIDING WINDOW CRACKED.  AIRCRAFT RETURNED TO BOI AND MADE AN UNEVENTFUL LANDING.  INSPECTED WINDOW AND CONFIRMED TO BE OUTER PANE.  REMOVED AND REPLACED WINDOW ASSEMBLY PER BOEING M.M.


REMARKS:
DURING CLIMBOUT, EXPERIENCED BIRDSTRIKE TO NR 1 ENGINE.  AIRCRAFT RETURNED TO BWI AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND PERFORMED BIRDSTRIKE INSPECTION, CONFIRMED BIRD ENTRY INTO ENGINE CORE.  ENGINE PLACED ON 10-CYCLE FLYBACK.  HOU RON BORESCOPED, NO DEFECTS NOTED.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND LEFT W/W TRANSVERSE I BEAM FLOOR SUPPORT CRACKED APPROX 2 INCHES FWD OF BS 727 BULKHEAD AT CEILING FWD OF BULKHEAD.  REPAIRED PER SWA RA 1-253-1398.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND FWD CARGO DOOR FRAME STRINGER CRACKED IN RADIUS S26R, AT BS 450 AND 470.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN LAP CRACK INDICATIONS AT THE FOLLOWING LOCATIONS:  BS 766, S10L, ATBS 776, S10L, AND AT BS 381, S14R, AT LOWER ROW OF FASTENERS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CRACK INDICATIONS UNDER BULKHEAD STRAP, RBL 5.5, WL 188 TO 202.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 947.5, RBL 10.5 TO LBL 21.0.  REPAIRED PER SWA RA 1-353-1391.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOOR FRAME CUT-OUT CHIPPED AND BENT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO FLOOR ANGLE CRACKED AT BS 747.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGERS CRACKED AT LEFT AND RIGHT ICE LIGHTS LOCATIONS.  REPAIRED PER SWA ACO 6405-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 344, RBL 7 TO LBL 7.  REPAIRED PER SWA RA 1-353-1392.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 947.5, RBL 5.  REPAIRED PER SWA RA 1-353-1390.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 344, BBL 0.  REPAIRED PER SWA RA 1-353-1393.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 328, RBL 31.5.  REPAIRED PER SWA RA 1-353-1395.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 328, RBL 41.  REPAIRED PER SWA RA 1-353-1394.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 294.5, RBL 37.5 TO RBL 41.5, LONG STRAP, AFT FLANGE.  REPAIRED PER SWA RA 1-353-1396.


REMARKS:
ROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 8 INCH BY 3 INCH CORRODED AREA ON BOTTOM AND SIDES OF STRINGER.  STRINGER 27L BENEATH FRAME AT BS 967.  REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM.  REPAIR PER SRM53-10-3 FIG 1.  (M)


REMARKS:
BNA - COMPRESSOR STALL ON LEFT ENGINE.  CAPTAIN SHUT DOWN NR 1 ENGINE.  REMOVED AND REPLACED NR 1 ENGINE PER JOB CARD.OPS AND LEAK CHECKED NORMAL.  (M)


REMARKS:
ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 6.5 INCH BY 8 INCH CORRODED SKIN, BS 747 S-27R.  REMOVED CORROSION ANDINSTALLED DOUBLER, REPAIRED PER SRM 53-10-4.  (M)


REMARKS:
ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1 INCH CORRODED AREA STRINGER 27L BETWEEN STATION 986-1016.SPLICED NEW STRINGER, REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
BUF - FLT NR 1063 - ON CLIMB-OUT FROM BUF, NR 2 ENGINE OIL PRESSURE INDICATION DROPPED TO 15 PSI.  FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO BUF WHERE LANDING WAS WITHOUT INCIDENT.  SET WAS 11 MINUTES.  MAINTENANCE REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER.  OPS CHECKED GOOD.  (M)


REMARKS:
LAX - FLT NR 0816 - THE FLOOR TRACK LIGHTING IN THE FORWARD CABIN WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPAIRED THE FLOOR TRACK LIGHTING WIRE ON THE FORWARD LEFT SECTION AND REPLACED THE BATTERY CHARGER ASSEMBLY.  REFERENCE USAA950903.


REMARKS:
PHL - FLT NR 1487 - RETURN TO FIELD DUE TO THE AFT CARGO DOOR LIGHT ILLUMINATING.  MAINTENANCE FOUND THE REAR CARGO DOOR AJAR.  VISUAL AND MECHANICAL INSPECTION CHECKS GOOD.  NO DEFECTS OR LIGHT MALFUNCTION NOTED.  (M)


REMARKS:
LAX - FLT NR 0816 - THE FLOOR TRACK LIGHTING IN THE FORWARD CABIN WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPAIRED THE FLOOR TRACK LIGHTING WIRE ON THE FORWARD LEFT SECTION AND REPLACED THE BATTERY CHARGER ASSEMBLY.  (M)


REMARKS:
PIT - FL 1749 - LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED WHEN GEAR SELECTED UP.  CYCLED GEAR AND BOTH MAIN GEAR RED LIGHTS ILLUMINATED ALONG WITH BOTH MAIN GEAR DOOR YELLOW LIGHTS.  FLIGHT RETURNED TO PIT WITH NO FURTHER INCIDENTS.  MAINTENANCE ADJUSTED THE LANDING GEAR DOOR UPLOCK SWITCHES.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 500 PLUS 4 STRINGER 16L.  INSTALLED DOUBLER, REPAIRED PER EO 5393X228.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL, FOUND .5 INCH CRACK BS 500 C PLUS 4 STRINGER 16R.  INSTALLED DOUBLER, REPAIRED PER EO 539X228.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 500 C PLUS 16, STRINGER 16R.  INSTALLED DOUBLER, REPAIRED PER EO 5393X228.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN BS 925.  INSTALLED EXT FUSELAGE SKIN REPAIR.  REPAIRED PER SRM 53-00-01 FIG 202.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CROWN SKIN CHAFED UNDER DORSAL FIN CONTACT AREA, S-1 BS 887 TO BS 867.INSTALLED EXT SKIN DOUBLER.  REPAIRED PER TR 53-30-03, SRM 53-00-01.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION AT CLIP NUT HOLES, AFT CARGO BIN AFT CENTER BULKHEAD LOWER ATTACH ANGLE.  REPLACED ATTACH ANGLE, REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-202-01, CORR5OSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION BS 947.5 TO BS 967 RBL 45 ON FLOOR BEAM T-CAP.  FABRICATED NEW T-CAP 18 INCHES LONG, REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION BS 870 S-21L.  INSTALLED FILLER AND DOUBLER,REPAIRED PER SRM 51-70-11 FIG 1.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 6 INCH CORRODED AREA AFT CARGO BS 986.50- BS 1006 DUMP SHOOT BASE.  INSTALLED NEW BASE PER DRAWING 65-45781, REPAIRED PER BOEING DRAWING 65-45781.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (M)


REMARKS:
IND - FLT NR 1157 - EN ROUTE LGA TO MCI, NR 1 NORMAL TRANSFER BUS CIRCUIT BREAKER POPPED.  CREW RESET BREAKER AND IT POPPED AGAIN.  FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE TRANSFER RELAY.  RAN ENGINES AND APU.  OPS CHECKED NORMAL.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 18 INCHES STATION 986.5 BL ZERO TO LBL 24 INCHES.  REPLACED UPPER T-CAP.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 36 INCHES STATION 344 LBL 24 INCHES TO RBL 12 INCHES.  REPLACED UPPER T-CAP OF BEAM.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES AT STATION 294.5 LBL 20 INCHES.  CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER.  REPAIRED PER SRM 53-10-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION EXCEEDING LIMITS AROUND HOLE, BS 958 RBL 7.5.  FABRICATED NEWINTERCOSTAL FROM BAC1506-437075-T6 AND INSTALLED.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 5 INCHES AT STATION 370 AT FORWARD ENTRY THRESHOLD. REPLACED Z-ANGLE.  REPAIRED PER BOEING DRAWING 65C80735.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCHES AT FORWARD SERVICE DOOR THRESHOLD.  REPLACED Z-ANGLE.  REPAIRED PER BOEING DRAWING NR 6545875.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES AT BS 947.5 TO BS 992.5 LBL 53 AFT ENTRY DOOR.  REPAIRED PER BOEING DRAWING 65-52878.  CORROSION LEVEL 2.  CORROSION LEVEL 2.  CORROSION TASK NR C53-107-02.  (M)


REMARKS:
PIT - DURING C-4 CHECK INSPECTION, FOUND A 3 INCH, 2 INCH AND A 1.1875 INCH CRACK AT STATION 1338 AT LONGERON 14L, 12L AND BETWEEN 14L AND 15L (EDDY CURRENT).  REMOVED AND REPLACED UPPER LEFT T-CAP SEGMENT PER USAIR EO NR 5389X252 PART 2.(M)


REMARKS:
PIT - FLT NR 0497 - AFTER TAKEOFF FROM PIT, FLIGHT OFFICERS AIRSPEED, ALTIMETER, AND RATE OF CLIMB INDICATORS FAILED.  FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 ADC.  OPERATIONS CHECKED OK.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, BS 296 AT WL 208 (RIGHT DOOR CUTOUT FRAME).  CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-70-11.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION BS 986 RBL 31.  CUT OUT CORROSION, INSTALLEDFILLERS AND REPAIR ANGLES, REPAIRED PER SRM 53-60-51, FIG 203.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE .375 INCH CRACKS AT NR 1 SLAT BS 299.32 ON BOTTOM SKIN.  CUT OUT SECTION OF SKIN AND INSTALLED DOUBLER, REPAIRED PER EA 39909.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 8 INCH CORRODED AREA BETWEEN BS 312 THROUGH BS 328 AT RBL 12 INCHES.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 5 INCH AND .25 INCH BY 6 INCH CORRODED AREA BETWEEN BS 328 AND BS 344 AT LBL 12 INCHES.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOT OF CORROSION RBL 24 BS 950.  REPLACED INTERCOSTAL,REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION LBL 24 BS 950.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLE RBL 17 BS 968.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION AT BS 947 LBL 47.  REPLACED MOUNT PAD, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION AT LBL 9 BS 947.  CUT OUT DAMAGE, INSTALLED FILLER AND REPAIR ANGLES, REPAIRED PER SRM 53-60-51, FIG 203.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 2 INCH AREAS OF CORROSION BS 987 LBL 32 AND LBL 45.  CUT OUT CORROSION AND INSTALLED REPAIR ANGLES AND STRAPS.  REPAIRED PER TR 53-10-01A, SRM 53-60-51 FIG 203.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL .75 INCH BY .5 INCH SPOTS OF CORROSION BS 500G STRINGER 15R TO STRINGER 25L.  REPLACED ATTACHED ANGLE, REPAIRED PER DRAWING 65-49631 AND SRM 51-10-2.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND ABOUT AN 1 INCH BY 57 INCH CORRODED AREA BS 303-360, S-17L, FORWARD ENTRY DOOR Z-ANGLE.  REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE FROM STOCK P/N 65C80735-18.  REPAIRED PER SRM 51-10-2.CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 28 INCHES BY .5 INCH CORROSION AT STATION 344 LBL 28, LLB ZERO.  FABRICATED T-CAP AND REPAIRED ANGLES.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 16 INCH CORROSION RBL 12 STATION 328 TO STATION 344.  FABRICATED INTERCOSTAL.  REPAIRED PER BOEING DRAWING 65-45234.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT -DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH CORRODED AREA AT BS 328 LBL 35 INCHES TO RBL 65 INCHES.  REMOVED DAMAGE, INSTALLED REPAIR PARTS COMPLETE REPAIR.  REPAIRED PER SRM 53-10-51 T/R 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETER AREA OF CORROSION STATION 294.5 FLOOR BEAM UPPER CHORDAT RBL 4.  INSTALLED REPAIR ANGLES PER SRM 53-10-51 FIG 206.  REPAIRED PER SRM 53-10-51, FIG 206.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 18 INCH CORRODED AREA BS 294.5 TO BS 312 AT RBL 12.  REPAIREDPER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 48 INCH AREA CORRODED AFT ENTRY DOOR Z-ANGLE BS947 THROUGH BS 997.  REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE EPR SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 60 INCH CORRODED AREA BS 280-BS 344, STRINGER 17R (FORWARD SERVICE DOOR Z-ANGLE).  REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE FROM STOCK P/N 654587545.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C52-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
FLT NR 572 - ATL-MCI - CREW NOTICED FUEL LEAKING FROM RIGHT WING FUEL TANK ACCESS PLATE.  FLIGHT RETURNED TO ATL FOR REPAIRS.  ATL MAINTENANCE RESEALED RIGHT WING UPPER TANK PLATE BL 1426.


REMARKS:
CLT - FLT NR 0578 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF.  USED OVERIDE BUTTON TO RETRACT LANDING GEAR.  FOUND PIN IN CONNECTOR CM62 BENT.  STRAIGHTENED PIN AND RECONNECTED CONNECTOR, SYSTEM TEST NORMAL PER CHAP 32 AND CHAP 27 IN MM.  (M)


REMARKS:
ROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 12 INCHES, STRINGER 27L AT BSL 967.  INSTALLED STRINGER SPLICE PER SRM 53-10-3.  REPAIRED PER SRM 53-10-3, FIG 1.  (M)


REMARKS:
CLT - DURING A PCI INSPECTION, FOUND CORROSION 10 INCHES BY 1 INCH ON STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360.  CORROSION TASK NR C53-202-02/PCI 1227, CORROSION LEVEL 2.  REPLACED END STRINGER 28R, RBL 6.  (M)


REMARKS:
IND - FLT NR 301 - EMERGENCY FLOOR LIGHTING IN FIRST CLASS WAS REPORTED AS INOP.  REPLACED EMERGENCY FLOOR LIGHTING LAMP STRIP.  (M)


REMARKS:
PIT - THE FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE.  FIXED WIRING PROBLEM AT PREVIOUS REPAIR, ROW 12.  (M)


REMARKS:
CLT - FL 1112 - DURING TAKEOFF GROUND ROLL, CREW NOTED SMELL OF BURNING RUBBER.  CREW LEFT GEAR DOWN, SMELL DID NOT DISSIPATE.  CREW DECLARED AN EMERGENCY, DUMPED CABIN AIR, AND RETURNED TO CLT.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE RAN BOTH ENGINES AND BOTH PACKS.  CABIN WAS PRESSURIZED TO APPROXIMATELY FOUR PSI.  SMELL COULD NOT BE DUPLICATED.  AIRCRAFT RELEASED FOR SERVICE.  (M)


REMARKS:
DAY - FLT 0223 - EN ROUTE IND TO BWI, AIRCRAFT EXPERIENCED AN UNCOMMANDED LEFT FULL RUDDER TRIM.  CREW DISCONNECTED THEAUTOPILOT AND YAW DAMPER WITH NO EFFECT.  FLIGHT DIVERTED TO DAY AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE RUDDER TRIM INDICATOR, CONTROL MODULE, AND ACTUATOR.  PROBLEM WAS CONFIRMED AS A BAD RUDDER TRIM SWITCH.  (M)


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FUOND IN THE FORWARD PIT CRACKS, AT FS 218, ON THE LOWER FRAME.  REMOVED DAMAGED SECTION.  FABRICATED REPAIR MEMBER AND INSTALLED IAW DC-9 SRM 51-10-3, 51-10-1 AND 51-10-2A.  (M)


REMARKS:
UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, EVIDENCE OF CORROSION WAS FOUND ON THE TCAS ANTENNA AFTSIDE.  REMOVED MOUNTING PLATE AND FINGER DOUBLERS.  FABRICATED A NEW PLATE AND FINGER DOUBLERS AND INSTALLED ALL PARTS IAW DC9 SRM 53-04 FIG 12B.  (M)


REMARKS:
IND - DURING CX-6 CHECK INSPECTION, FOUND A .125 INCH CRACK IN THE FUSELAGE SKIN AT STATION 560 LONGERON 22R.  INSTALLED CLASS 2 REPAIR PER SRM 53-04.  (M)


REMARKS:
ROA - DURING CD-3 CHECK VISUAL INSPECTION, FOUND STRINGER CORRODED AT BS 767, STRINGER 276 BS 767.  REMOVED DAMAGED STRINGER AND SPLICED NEW STRINGER PER SRM 53-10-3.  (M)


REMARKS:
CLT - DURING A Q6-CHECK INSPECTION, VISUALLY INSPECTED CARGO FLOOR BEAM.  CORROSION FOUND AT STATION 772 AT CARGO FLOORSUPPORT CHANNEL.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  INSTALLED REPAIR ANGLES.  (M)


REMARKS:
CLT - DURING A Q6-CHECK INSPECTION, VISUALLY INSPECTED A 2 INCH CORRODED AREA LOCATED AT THE FLOOR BEAM STATION 312 RBL6.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  INSTALLED T-CAP.  (M)


REMARKS:
CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A 1 INCH BY 4 INCH CORRODED AREA AFT CARGO BIN DOOR FRAME AT LOWER FORWARD CORNER.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  DOUBLER INSTALLED ON FRAME.  (M)


REMARKS:
CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES (40 INCHES) AT STATION 344 RBL 8 TO LBL 45.5, ON FLOOR BEAM.  CORROSION TASK NR C53-127-02, CORROSION LEVEL 2.  REMOVED AND REPLACED T-CAP.(M)


REMARKS:
CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES 30 INCHES AT STATION328 FROM LBL TO RBL 55, ON FLOOR BEAM.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  INSTALLED T-CAP (UPPER) PER TYPICAL REPAIR 53-10-03.  (M)


REMARKS:
CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORROSION AT FLOOR BOARD ATTACH HOLES AND AT TOP HORIZONTAL EDGE 10INCHES LOCATED ON FLOOR BEAM AT STATION 986.5 ATTACH HOLES ALONG SPAN OF BEAM AND LEADING EDGE BL 33R TO BL 44R.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  INSTALLED T-CAP.  (M)


REMARKS:
CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A SKIN DENT 3.5 INCHES BY 3.5 INCHES BY .180 INCH DEEP IN THE LAV SERVICE DOOR STATION 288 AT STRINGER 20R AND 21R.  INSTALLED SKIN.  (M)


REMARKS:
CLT - DURING A Q6-CHECK, INSPECTION FOUND BY EDDY CURRENT A 2.2 INCH CRACKED TRACK LOCATED AT STATION 520 A CENTERED RBL 45.5.  INSTALLED DOUBLERS, TRIMMED FITTINGS, TRACKS AS REQUIRED. (M)


REMARKS:
CLT - DURING A Q-6 CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.9 INCH CRACKED TRACK LOCATED AT STATION 520 EXTENDING 1.1 INCH INBOARD AND .8 INCH OUTBOARD OF RBL 24.75.  INSTALLED DOUBLERS AND TUB FITTINGS.  (M)


REMARKS:
CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A DENT 2.5 INCHES BY 5 INCHES BY .060 DEEP AT STATION 921 BETWEEN STRINGER 17R AND 18R.  INSTALLED DOUBLER.  (M)


REMARKS:
CLT - DURING A Q6-CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.8 INCH CRACK LOCATED AT STATION 520, CENTERED AT LBL 45.5.  INSTALLED TUB FITTING AND TRACK ASSY KIT 65C3468827.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1.4 INCH CRACK LOCATED AT STATION 520 EXTENDING .6 INCH OUTBOARD AND .8 INCH INBOARD OF LBL 45.5.  INSTALLED DOUBLER.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, VISUALLY INSPECTED AND FOUND A 1 INCH SKIN BULGE AND CHUNK MISSING BETWEEN STRINGER21-20 RIGHT STATION 492.4.  INSTALLED DOUBLER.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH ROUND HOLE IN SKIN (PRIOR REPAIR CLEANUP) LOCATED FS 935, STRINGER 18 RT.  INSTALLED DOUBLER.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH HOLE REPAIR LOCATED AT STATION 344, STRINGER 18L.  EXISTINGREPAIR, DOUBLER INSTALLED.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, A 16 INCH BY 10 INCH REPAIR INSTALLED LOCATED AT STATION 365, STRINGER 11L WAS VISUALLY FOUND.  EXISTING REPAIR DOUBLER INSTALLED.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 8 INCH BY 8 INCH REPAIR INSTALLED LOCATED AT STATION 430 STRINGER 10L.  PREVIOUS REPAIR DOUBLER INSTALLED.  (M)


REMARKS:
CLT - PREVIOUS 14 INCH BY 10 INCH REPAIR (EXT DOUBLER) INSTALLED LOCATED STATION 867 BETWEEN STRINGER 21R AND STRINGER 22R.  VISUALLY INSPECTED.  PREVIOUS REPAIR DOUBLER INSTALLED.  (M)


REMARKS:
CLT - VISUALLY INSPECTED EXISTING REPAIR, LARGE RIVET IN SKIN BAY LOCATED AT STATION 390 ABOVE STRINGER 11L.  INSTALLEDPROTRUDING HEAD RIVET 211TT3.  (M)


REMARKS:
PIT - FL 0576, AFTER TAKEOFF, CREW RECEIVED THE NR 1 CENTER HYDRAULIC PUMP PRESS LIGHT.  CREW NOTED LOSS OF HYDRAULIC QUANTITY FROM CENTER SYSTEM.  FLIGHT RETURNED TO PIT WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED TWO HYDRAULIC LINES (PUMP TO FILTER MODULE LINES).  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 28R AT STATION 1287.  CORROSION TASK NR C57-53300.SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 29R AT STATION 1297 CORROSION TASK NR C57-53300.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 3 INCH BY 6 INCH AREA OF CORROSION LEVEL 2 IN CUSP ANGLE AT MED FRAME LOWER ATTACH FITTING STATION 200.  CORROSION TASK NR C46-53303.  REMOVED CORRODED SECTION AND SPLICED NEW SECTION IN PER USAIR EA 31153.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 3 AREAS 2 INCHES BY 3 INCHES OF LEVEL 2 CORROSION AFT SIDE OF FRAME AT STATION1250 FROM LONGERON 28L TO 28R.  CORROSION TASK NR C57-53300.  CLEANED CORRODED SECTION AND INSTALLED DOUBLERS PER SRM 53-03 FIG 2A.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION 2 INCHES BY 35 INCHES STATION 1338, JACK PAD DOUBLER AFT CARGO AREA.  CORROSION TASK NR C57-53300.  REPLACED DOUBLER, CUT OUT DAMAGED AREA AND SPLICED IN NEW SECTION PER USAIR TYPICAL REPAIR 53-30-10.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK UPPER FORWARD CORNER OF MED JAMB.  INSTALLED INTERNAL AND EXTERNAL DOUBLER PER SRM 53-05 FIG 2B.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK LONGERON 4L AT STATION 160.  SPLICED IN NEW SECTION OF LONGERONPER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 5 CRACKS .125 INCH TO .375 INCH LONG, BELTFRAME 256 TO 408 IN LONGERON 17R.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 12 INCH CRACK IN CUSP MEMBRANE STATION 1231, LONGERON 18L.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 96.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK LEFT SIDE STATION 1463, DRAG ANGLE.  INSTALLED FILLER AND DOUBLER PER SRM 53-05 FIG 23.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH BY 20 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED AT LONGERON 28L, STATION 1211 TO 1231 CORROSION TASK NR C57-53300.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 2 INCH BY 29 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED RIGHT LAV T-CUSP ANGLE FROM STATION 1309 TO 1338 LONGERON 18R.  CORROSION TASK NR C58-53300.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-05FIG 25.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED IN BELTFRAME BETWEEN LONGERON 28R AND 28L BELTFRAME 180.  CORROSION TASK NR C45-53300.  REMOVED SECTION OF BELTFRAME AND SPLICED IN NEW SECTION PER SRM 53-03 FIG 2A.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND CORROSION 1 INCH BY 6 INCHES LEFT INBOARD SEAT TRACK MOUNT HOLES AT STATION 1205.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED FORWARD CARGO DOOR JAMB PAN ALONG BOTTOMEDGE BETWEEN PAN AND FUSELAGE SKIN CORROSION REF C51-53300.  REMOVED LOWER SECTION OF DOOR JAMB AND SPLICED IN NEW SECTION PER SRM 53-05 FIG 44.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1.8 INCH CRACK LOCATED AT STATION 520 EXTENDING 1.0 INCH INBOARD AND .8 INCH OUTBOARD OF RBL 24.75.  INSTALLED DOUBLER.  (M)


REMARKS:
CLT - DURING A Q-3 CHECK INSPECTION, VISUALLY FOUND A 1.9 INCH SKIN CRACK LOCATED AT STATION 520 EXTENDING .9 INCH OUTBOARD AND 1 INCH INBOARD OF LBL 24.75.  INSTALLED DOUBLER.  (M)


REMARKS:
CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A .9 INCH SKIN CRACK LOCATED AT STATION 520 EXTENDING 1.0 INCH OF RBL 45.5.  INSTALLED DOUBLER.  (M)


REMARKS:
CMH - FL 1101, AFTER TAKEOFF FROM FWA AND GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED.  ABNORMAL PROCEDURES COMPLIED WITH, INDICATIONS SHOWED AND UNLOCKED DOOR.  GEAR WAS SELECTED DOWN AND FLIGHT DIVERTED TO CMH.  AFTER LANDING AND ENGINE SHUTDOWN, LEFT MAIN GEAR DOOR OPENED AND RESTED ON THE GROUND.  MAINTENANCE REPLACED THE LEFT MAINGEAR DOOR ACTUATOR.  (M)


REMARKS:
CLT - FL 799 - AFTER TAKEOFF FROM CLT, CREW RECEIVED RED WARNING LIGHT ON LEFT MAIN GEAR UPON GEAR RETRACTION.  CREW EXTENDED GEAR AND THE LIGHT REMAINED ILLUMINATED.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE ADJUSTED THE POSITION OF THE LEFT UPLOCK ROLLER ASSEMBLY AND FLYING DOOR.  AIRCRAFT WAS JACKED AND A GEAR SWING PERFORMED.  (M)


REMARKS:
CLT - FL 1229, ON APPROACH, CREW RECEIVED APU FIRE WARNING LIGHT AND APU AUTO SHUTDOWN.  THE APU FIRE BOTTLE DISCHARGEDAUTOMATICALLY.  THE APPROACH CONTINUED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  NO INDICATION OF FIRE WAS FOUND.  MAINTENANCE CHECKED FOR HOT AIR LEAKS AND FOUND NONE.  ALL OTHER SYSTEMS CHECKED NORMAL.  FIRE BOTTLE REPLACED AND AIRCRAFT RELEASED FOR SERVICE.  (M)


REMARKS:
CLE - RIGHT INTERIOR OVERWING EMERGENCY LIGHTS INOP.  REPLACED BATTERY PACK, CHECKS SATISFACTORY.  (M)


REMARKS:
GSO - FLIGHT NR 1794 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT.  GROUND FLIGHT FAULT ON MULTI FUNCTION DISPLAY UNIT.  RETURNED TO GSO FOR LANDING.  FOUND PROXIMITY SENSORS ON LEFT GEAR FOR FLT GROUND OUT OF ADJUSTMENT.  ADJUSTED BOTHFLT GROUND PROXIMITY SENSOR IAW 32-63-03.  (M)


REMARKS:
GSO - FLT NR 735 - NR 1 ENGINE SHUT DOWN ON SHORT FINAL DUE TO CSD LIGHT, LOW OIL PRESSURE AND DECAYING RPM TO 38 PERCENT HP RPM.  FOUND O-RING CUT AND LEAKING FROM HP FUEL SHUTOFF VALVE AT THE PRESSURE INLET TO THE FUEL FLOW REGULATOR.  OIL LEVEL GOOD, CSD LEVEL GOOD.  GROUND RAN ENGINE, OPS CHECK GOOD.  (M)


REMARKS:
PIT - FLT NR 1025 - AFTER TAKEOFF WE RECEIVED A GND/FLT CONTROL MSG ON MFDU.  ALL INDICATIONS INDICATED AIRCRAFT WAS STILL ON GND.  RETURNED TO PIT AFTER CONSULTING WITH MAINTENANCE CONTROL.  REPLACED NR 3 RT PROXIMITY SENSOR PER MM 32-63-03.  ADJUSTED AND OPS CHECKS GOOD PER SAME.  (M)


REMARKS:
PHL - FLT NR 0117 - CLIMBING OUT FROM LGA EN ROUTE TO MCO WITH ALT ALERTING AND 'A' CHANNEL AUTOPILOT ON MEL, AIRCRAFT WOULD NOT HOLD ALTITUDE OR RESPOND TO CHANGES WITHOUT USING ALT SEL.  MAINTENANCE REPLACED THE AUTOPILOT MODE CONTROL PANEL.  BITE CHECKED AND FUNCTIONAL CHECKED GOOD.  (M)


REMARKS:
MCI - DURING OP-15, FOUND CORROSION IN HORIZONTAL LEG AT T-CAP BETWEEN STRINGERS 12 AND 13.  REMOVED CORROSION AND INSTALLED CLIPS PER SERVICE BULLETIN 57-98.  (M)


REMARKS:
JFK - DURING CLIMB, APU HAD AN AUTO SHUT DOWN.  BITE CHECK SHOWED LOW OIL PRESSURE.  REPLACED LOW OIL PRESSURE SWITCH, MFG P/N 3876024-5.  APU OPERATION THEN CHECKED NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, NR 1 ENGINE WAS SHUT DOWN DUE TO OIL QUANTITY DECREASING TO ONE GALLON.  FOUND NR 6 SCAVANGE PUMP OIL TUBE, MFG P/N RD2189-1, TO BE CRACKED.  REMOVED AND REPLACED CRACKED SCAVANGE OIL TUBE, RAN ENGINE PERFORMANCE LEAK CHECK, FOUND NORMAL.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 6 CRACKS APPROXIMATELY .125 INCH TO .25 INCH IN LONGERON 17L AT BELTFRAME 237,275, 295, 332, 370 AND 389.  SPLICED IN NEW SECTION OF LONGERON BETWEEN STATION 237 TO 408 PER SRM 53-02 FIG 2.  (M)


REMARKS:
DURING CLIMBOUT, EXPERIENCED A-SYSTEM HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED PUMP, FILTERS AND FLUSHED SYSTEM PER BOEING M/M.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAPS CRACKED AT RBL 32 AND AT LBL 12 BS 312 IN E AND E COMPARTMENT.  REPAIRED PER BOEING SRM.


REMARKS:
ATL/MDW - FLT 248 - THE CAPTAIN CALLED BACK WITH ENGINE VIBRATION.  THE AIRCRAFT RETURNED TO ATL.  MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE.  OPS CHECKED OK.


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND .50 INCH BY 1 INCH CORRODED AREA 3 PLACES ON INTERCOSTAL, BS 328 - BS344.17, RBL 11.  REPLACED INTERCOSTAL WITH NEW ONE.  REPAIRED PER SRM 53-10-51.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02. (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 28 INCH AREA CORRODED AT BS 294.5 - BS 344.17.  REPLACED Z-ANGLE.  REPAIRED PER SRM 51-10-2.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURNG 'Q-3' CHECK, VISUAL INSPECTION FOUND 4 INCH BY 2 INCH CORRODED AREA BS 312, RBL ZERO - 11, ON FLOOR BEAM.  INSTALLED NEW T-CAP SECTION.  REPAIRED PER TR 53-10-03.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURNG 'Q-3' CHECK, VISUAL INSPECTION FOUND 12 INCH BY 5.75 INCH PREVIOUSLY INSTALLED SKIN DOUBLER (NO SDA) STA 336 TO STA 348 BETWEEN STR 19R PLUS STR 20R, CRACKED.  DOUBLER INSTALLED.  REPAIRED PER SRM 53-00-01, FIGURE 202.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND .75 INCH CRACK, SEAT TRACK SUPPORT CHANNEL STA 520, LBL 24.75 AFT SIDE WL 207.5.  REPAIRED PREVIOUSLY.  REPAIRED PER EA 34112.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 11 INCH BY 12 INCH DENT, AFT CARGO DOOR.  DOUBLER INSTALLED.  REPAIRED PER SRM 52-00-01, FIGURE 202.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 2 INCH BY 42 INCH CORRODED AREA, STA 953 - STA 996, LBL 54 (LEFT AFT CABIN DOOR) ON Z-ANGLE.  REPLACED Z-ANGLE.  REPAIRED PER SRM 51-10-02.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION AT FLOORBOARD HOLES ON BEAM T-CAP, BS 328, LBL 10 TO RBL 45.  INSTALLED NEW SECTION OF T-CAP.  REPAIRED PER SRM 53-0-51.  THIS IS LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02. (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION ON INTERCOSTAL BS 957, RBL 18 TO RBL 45.  INSTALLED NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION ON INTERCOSTAL, BS 947 TO BS 967, RLB 25.  INSTALLED NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION AT FLOORBOARD ATTACH HOLES ON FLOOR BEAM.  INSTALLED UPPER T-CAP SECTION ON FLOOR BEAM.  REPAIRED PER TR 53-10-05.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION ON INTERCOSTAL, BS 947 TO BS 967, RBL 45.  INSTALLED NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  LEVEL 1 CORROSION.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 3 INCH CRACK BETWEEN BS 328 AND BS 312 AT RBL 32 INCH, ON INTERCOSTALWEB.  FABRICATED NEW WEB.  REPAIRED PER DRAWING 65-45834.  (X)


REMARKS:
INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 6 INCH CORROSION BS 328 - BS 331, AND BS 370 - BS 373, SEAT TRACK.  REPLACED SEAT TRACK.  REPAIRED PER SRM 53-00-52, FIGURE 202, REPAIR 1.  (X)


REMARKS:
ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR FUSELAGE SKIN BS 927, STR 18L - STR 19L, DAMAGED.  ONE DOUBLER INSTALLED 12 INCH BY 10.50 INCH.  REPAIRED PER SRM 53-00-01.  (X)


REMARKS:
ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, AFT CARGO DOOR.  TWO DOUBLERS INSTALLED ONE ABOVE HANDLE, 7 INCHES BY 12.50 INCHES BY 7.50 INCHES BY 21 INCHES.  ONE BELOW HANDLE, 8.25 INCHES BY 7.25 INCHES.  REPAIRED PER SRM 52-30-01.  (X)


REMARKS:
ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, FORWARD SERVICE DOOR, TOP AND LOWER HINGE, DAMAGED.  TWO DOUBLERS INSTALLED, ONE TOP HINGE, AND ONE BOTTOM HINGE, TOP 7 INCHES BY 8 INCHES, BOTTOM 5 INCHES BY 5 INCHES.  REPAIRED PER SRM 52-00-01.  (X)


REMARKS:
ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, AFT CARGO DOOR SKIN, DAMAGED.  ONE DOUBLER PREVIOSULY INSTALLED 8 INCHES BY 16 INCHES.  REPAIRED PER SRM 52-30-01.  (X)


REMARKS:
ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, FORWARD CARGO DOOR SKIN, DAMAGED.  ONE DOUBLER PREVIOSULY INSTALLED, 8 INCHES BY 11 INCHES.  REPAIRED PER SRM 52-30-01.  (X)


REMARKS:
INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 14 INCH BY 2 INCH CORROSION, BS 947.5 - BS 967, RLB 8, ON INTERCOSTAL.  REPLACED WITH NEW INTERCOSTAL.  REPAIRED PER 737-300, SRM 51-10-02, PAGE 16.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND CORROSION 1 INCH BY 55 INCHES, STA 967, RBL 27, LBL 45, ON FLOOR BEAM.  REPLACED T-CAP.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND CORROSION 1 INCH BY 3 INCH, STA 967 TO STA 986, RBL 18 INCHES, ON INTERCOSTAL.  REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 100 INCH BY 3 INCH CORROSION AROUND SCREW HOLES, BS 986.5, ON FLOOR BEAM.  REPLACED T-CAP ON TOP OF CABIN FLOOR BEAM.  REPAIRED PER TR 53-10-05.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 14 INCH BY 2 INCH CORROSION, BS 947.5 - BS 967, RLB 18, ON INTERCOSTAL.  REPLACED INTERCOSTAL.  REPAIRED PER BOEING 737-300, SRM 51-1-02, PAGE 16.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORROSION AROUND NUTPLATE HOLES (2 PLACES) INTERCOSTAL RBL 18 BETWEEN BS 967 - BS 986.5.  REPLACED INTERCOSTAL.  REPAIRED PER BOEING DRAWING 65-46812, SRM 53-60-51.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORROSION ON FLOOR PAN, SEVERAL SPOTS, STA 1038, LBL8.  FABRICATED AND INSTALLED NEW FLOOR PAN.  REPAIRED PER DRAWING 65C33419, SRM 53-60-51.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 10 INCH BY 2 INCH CORRODED AREA, RBL 53, BS 940 TO BS 993, RIGHT AFT DOOR.  REPLACED Z-ANGLE.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 2 INCH CORROSION (2 PLACES), BS 1016, FLOOR BEAM LBL 4 AND LBL 27.  REPLACED ENTIRE T-CAP PER SRM 51-10-2, BOEING DRAWING 65C32677 AND DRAWING 65C33419.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
FRA - FLT 893 - DURING TEST, FOUND LEFT AISLE FLOOR EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPAIRED WIRING AND RELAMPED SOME SOCKETS.  (X)


REMARKS:
LGA - FLT 0089 - THE AFT ENTRY DOOR EMERGENCY LIGHT WAS INOPERATIVE.  REPLACED THE LIGHT ASSEMBLY.  (X)


REMARKS:
BOS - FLT 816 - AIRCRAFT RETURNED TO THE GATE BECAUSE THE FLOOR LEVEL EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT SHUT OFF.  MAINTENANCE CYCLED THE APPROPRIATE CIRCUIT BREAKERS AND THE SYSTEM RESPONDED CORRECTLY.  (X)


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND INTERCOSTAL CRACKED AT FWD CARGO THRESHOLD AT BS 469.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FWD ENTRY DOOR AFT INNER PANEL SUPPORT ATTACH ANGLE CRACKED BETWEEN AFT NR 3 AND 4 STOP FITTINGS.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING AREAS, BETWEEN BS 363 TO 420, S21 TO 22R, BS 919,S18R, BETWEEN BS 911 TO 920, S23 TO 25R, BS 944, S23 TO 24R, BS 925, S25 TO 26R, BS 369 TO 379, S4L, BS 373, S4 TO 5L, BETWEEN BS 321 TO 334, S22 TO 24R, BS 1040, RBL 3, WL 148, BS 960, S21 TO 22R, BS 342, BETWEEN 23 TO 24R, BS 929, BETWEEN 24 TO 25L AND BS 911, S21 TO 22R.  REPAIRED ALL PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR SKIN DENTED 4 PLACES BETWEEN HINGE AND ARM CUTOUTS.  REPAIRED PER BOEINGSRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND APU DOOR SKIN DENTED BETWEEN S5 TO 6L AND RT AFT CORNER BENT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND KEEL BEAM I/B T-SPLICE CRACKED AT BS 727 RBL WL 154.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT OUTER CHORD AT BS 178 CRACKED IN RADIUS FROM WL 194.25 TO 196.5.  REPAIRED PER TRAMCO EWO 95-0659.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 940 TO 990, RBL 45 TO RBL 57, WL 208, AND AT BS 940 TO 990, RBL57 TO 45, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME I/B CHORDS CRACKED AT BS 639, LBL 66, WL 215 AND AT S16R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE PRESSURE BULKHEAD GOUGED AT FLAP DRIVE UNIT ATTACH POINT.  REPAIRED PER TRAMCOEWO 95-0658.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 597 LBL 70 WL 202, BS 727A WL 209 LBL 64, BS 663 S1 TO S2R, BS 360 BETWEEN S20 TO 21R, BS 727A WL 209 BL LBL 64, BS 663, S1 TO 2R, BS 440 S2 TO 4R, BS 1086, RBL 30.  REPAIRED PER BOEING SRM AND TRAMCO EWO 95-0648.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CHAFED AT THREE SCREW ATTACH POINTS IN LOWER CHORD AT BS 715 TO 721, LBLWL 148.  REPAIRED PER TRAMCO EWO 95-0655.


REMARKS:
DURING SCHEDULED D-CHECK, SKIN DAMAGED AT BS 1156 RBL 16, ABOVE APU DOOR AT RIGHT AFT CORNER.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FUSELAGE SKIN CRACKED AT BS 1136, LBL 26 WL 181.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FUSELAGE SKIN CRACKED AT BS 492, RBL 35 WL 157.  REPAIRED PER TRAMCO EWO 95-0639.


REMARKS:
DURING SCHEDULED D-CHECK, FUSELAGE SKIN GOUGED AT BS 939 S19L, BS 1132 LBL 26, BS 1073 BETWEEN S16 AND 17L, BS 467 RBL 5 WL 149.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 633 S6L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SKIN AND SHEAR TIE CORRODED AT BS 847 BBL 0 TO LBL 4 S27L TO 27R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND RIGHT AFT SERVICE DOOR FRAME CRACKED AT BS 494 RBL 36 S24R.  REPAIRED PER TRAMCO EWO 95-0644.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES DENTED AT BS 480 LBL 33 WL 160, LBL 40 WL 163, LBL 50 WL 173.  REPAIREDPER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 480 S24L AND 25L, BS 727 PLUS 8, S9L, BS 727 PLUS 8, S9L,  AND BS 296 S10L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663 S1 AND S3R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER MISDRILLED AT BS 727A S8L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 927 LBL 6 WL 168 BETWEEN S26 TO 27L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM, VERTICAL FLANGE CRACKED AT BS 685 WL 207 RBL 25.  REPAIRED PER TRAMCO EWO 95-0663.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER GATE BEAM CRACKED.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 344 BL 0 LBL 8, 15, 22, 30, RBL 9, 12, WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM FASTENER HOLE CORROSION AT BS 987.5 LBL 13 WL 208 RBL 7, 10, 21, 23.5  AND RBL 31 WL 208.  REPAIRED PER TRMCO EWO 95-0656.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 328 LBL 12 RBL 10, 24, 27, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 312 LBL 12 RBL 14 WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
PIT - C-1 CHECK INSPECTION, FOUND GOUGE 5 INCH LENGTH AND .047 DEEP, MAXIMUM AT THE TOP IN VERTICAL STAB RIGHT SIDE NEAR RIB NR 5, UNDER ICE SCRAPPER.  INSTALLED EXTERNAL DOUBLER REPAIR PER USAIR EA NR 31389.  (M)


REMARKS:
MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN APPROXIMATELY .035 INCH AT STRINGER 19L, STATION 720E.  REPAIRED PER ARA 9388.  (M)


REMARKS:
SFO - DURING CRUISE SERVING CART EMITTED SMOKE AND ELECTRICAL ODOR.  DISCONNECTED SERVING CART.  FOUND DEFECTIVE POWER CORD ON SERVING CART.  REPLACED SERVING CART, MFG P/N 611-710345-1.  OPERATION CHECKED NORMAL.  (M)


REMARKS:
STL - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED.  EXTENDING LANDING GEAR WAS NORMAL.  FOUND RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR, MFG P/N 65-17819-15, ROD END FRACTURED.  REPLACED UPLOCK ACTUATOR AND RIGHT MAIN LANDING GEAR UPLOCK OPERATION CHECKED NORMAL.  (M)


REMARKS:
MCI - DURING OP-17, FOUND CORROSION ON RIGHT OUTBOARD FLANGE, STRINGER 29R, FS 990.  REMOVED CORROSION PER SSRM 51-10-6AND REPLACED STRINGER 29R PER SSRM 53-10-213.  (M)


REMARKS:
JFK - DURING DESCENT, BURNING ODOR DETECTED IN CABIN NEAR R3 DOOR.  IN DEPTH VISUAL INSPECTION OF CEILING WIRING AND ELECTRICAL COMPONENTS AND AN OPERATION CHECK OF ALL CABIN LIGHTS AND MUX SYSTEM, INCLUDING OPERATION CHECK OF R-3 DOOR, WAS PERFORMED.  (M)


REMARKS:
STL - DURING CLIMB NR 3 ENGINE, S/N 3901, OIL BYPASS LIGHT CAME ON.  ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED FROM FLIGHT.  REPLACED NR 3 ENGINE BYPASS SWITCH, MFG P/N MEGA00803-2, REPLACED FILTER, DRAINED AND RESERVICED OIL.  PERFORMED HI-POWER RUNUP, REMOVED AND REPLACED FILTER.  ENGINE OPERATION AND FILTER CHECKS NORMAL.  (M)


REMARKS:
MCI - DURING C-CHECK, FOUND AFT END OF FLOOR BEAM CASTING CRACKED, FS 940.  REPAIRED PER ARA 9659.  (M)


REMARKS:
STL - DURING OP-9, FOUND CORROSION IN NR 2 GALLEY RIGHT CABIN OUTBOARD SEAT TRACK MOUNT AREA, STATION 237.  INSTALLED NEW SEAT TRACK PER SRM 53-05, FIGURE 4.  (M)


REMARKS:
MCI - DURING C-CHECK, FOUND 2 INCH CRACK IN CABIN FLOOR BEAM RADIUS AT NR 4 CHAIR TRACK, RBL 48, STATION 740.  STOP DRILLED CRACK AND INSTALLED REPAIR ANGLES PER SSRM 53-40-03.  (M)


REMARKS:
STL - DURING TAKEOFF NR 3 ENGINE, S/N 4018, SPUN DOWN.  SHUT DOWN ENGINE PER FLIGHT HANDBOOK PROCEDURES.  FOUND DEFECTIVE FUEL PUMP, MFG P/N 378201-7.  REPLACED ENGINE DRIVEN FUEL PUMP.  ENGINE OPERATION THEN CHECKED NORMAL.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION IN RIGHT WING TANK AROUND FASTENER IN STRINGER 11, BETWEEN STRINGERS 69 AND 91.0.  REMOVED CORROSION PER SRM 51-10-3, REPAIRED PER ATA 9183 AND STANDARD PRACTICES.


REMARKS:
MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN .015 INCH, STRINGER 17L.  REPAIRED PER ARA 9388.


REMARKS:
MCI - DURING OP-15, FOUND CRACK IN LOWER REAR SPAR HORIZONTAL LEG OF RIGHT WING TANK, FROM HOLE IN AFT ROW TO RADIUS.  REMOVED CRACK PER STANDARD PRACTICES AND SRM 51-10-1, REPAIRED PER ARA 9184.  (M)


REMARKS:
BGR - DURING CRUISE SHUT DOWN RIGHT ENGINE, S/N 4704, DUE TO SURGING WITH ACCOMPANYING VIBRATION.  FOUND ENGINE ELECTRONIC CONTROL COMPUTER, MFG P/N 791100-4-087, AND FUEL METERING UNIT, MFG P/N 801000-3, MALFUNCTIONING.  REPLACED ENGINE ELECTRONIC CONTROL COMPUTER AND FUEL METERING UNIT, AND ENGINE OPERATION CHECKED NORMAL.


REMARKS:
CLT - FLT NR 1187 - RETURN TO FIELD DUE TO AN INDICATION THAT THE GEAR DOOR WAS OPEN.  JACKED AIRCRAFT, CHECKED ALL LANDING GEAR INDICATION SWITCHES AND MECH.  NO DEFECTS NOTED.  CYCLED GEAR.  ALL INDICATIONS GOOD.  (M)


REMARKS:
NR 1 ENGINE OIL TEMP EXCEEDED 120 DEGREES FOR 12 MINUTES, MAXIMUM TEMP 139 DEGREES.  REPLACED FUEL HEAT VALVE.  DRAINEDAND REPLACED ENGINE OIL.  REMOVED AND REPLACED OIL SCREEN PER MM 72-00, 518C CKS OK.  NO LEAKS ON RUN-UP.


REMARKS:
STL - FLT 290 - DURING PRE-FLIGHT, ESCAPE PATH LIGHTING STRIP FROM SEAT ROW 6 TO ROW 23, REMAINED ILLUMINATED WITH LIGHT SWITCH IN THE ARMED POSITION.  REPLACED BATTERY PACK, MFG PN 5822-2.  ESCAPE PATH LIGHTING SYSTEM THEN CHECKED NORMAL. CHECK C-7-8-95 - STL.


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND PREVIOUS TEMPORARY REPAIRS TO BOTTOM SECTION OF DOOR JAMB IN FORWARD CARGO,  2EACH.  REPLACED BOTTOM SECTION OF DOOR JAMB PER SRM 53-05 FIG 44.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND 5 CRACKS .5 INCH TO 1 INCH LONG IN CANTED FRAME STATION 1463, BELOW LONGERON NR 5L AND 5R.  CUT OUT SECTION OF DAMAGED AREA AND INSTALLED NEW SECTION PER USAIR EA NR 28127A.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN END OF LONGERON 2L STATION 1401.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 5 AND USAIR EA NR 28221.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STATION 1287 LEFT INBOARD SEAT TRACK CORROSION.  REF C58-53302.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1287 TO 1300 RIGHT INBOARD SEAT TRACK.  CORROSION REF C58-53302.  SPLICED IN NEW SECTION OF SEAT TRACK FROM STATION 1260 TO 1309 PER SRM 53-05 FIG 4F.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK LEFT WING LEADING EDGE STATION XFS 45.  CUT OUT DAMAGED AREA ANDINSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 57-06B FIG 8 AND USAIR EA NR 31310.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 636 TO 731 LONGERON 28L TIE DOWNRAIL.  MANUFACTURED NEW RAIL SECTION AND SPLICED PER SRM 53-05 4E AND DAC DWG SR09530082.  (M)


REMARKS:
PIT - DURING C-4 CHECK INSPECTION, FOUND 3 INCH, 2 INCH AND A 1.1875 INCH CRACK IN STATION 1338 T-CAP AT LONGERON 14L, 12L AND BETWEEN 14L AND 15L.  REMOVED AND REPLACED UPPER LEFT TEE CAP SEGMENT PER USAIR EO 5389X252 PART 2.  (M)


REMARKS:
FRA - FL 817, IMMEDIATELY AFTER TAKEOFF FROM FRA, THE AUTO INOP LIGHT ILLUMINATED AND THE EICAS MESSAGES 'CABIN ALT AUTO 1/2' AND 'CABIN AUTO INOP' ILLUMINATED.  FLIGHT RETURNED TO FRA AND LANDED WITH NO FURTHER INCIDENT.  THE NR 1 PRESSURE CONTROL UNIT FAULTED ON BITE AND WAS REPLACED.  ALSO, AS A PRECAUTION, THE OUTFLOW VALVE ASSEMBLY WAS REPLACED.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH CRACK RIGHT FORWARD DORSAL FIN DRAG ANGLE AT APPROXIMATELY STATION 1059.  REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND .875 INCH CRACK IN WEB WING STATION XCW 58.5 RIGHT SIDE.  ROUTED OUT AREA AND REPAIRED PER USAIR EO 5790D573.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND 2 INCH CRACK IN LEFT WEB AND 2 INCH CRACK IN DOUBLER WING STATION XCW 58.5 LEFT.  REMOVED AND REPLACED DOUBLER AND WEB PLATES PER USAIR EO NR 5790D573.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND .625 INCH CRACK RIGHT SIDE WING DOUBLER STATION XCN 58.5.  ROUTED OUT CRACKED AREA AND REPAIRED PER USAIR EO NR 5790D573.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 680, LONGERON 6L.  REMOVED DAMAGED SECTION OF LONGERON AND SPLICED IN A NEW SECTION PER SRM 53-02.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND TWO .5 INCH BY .5 INCH CRACKS, FRAME STATION 1076 AT BOTH LONGERON NR 12 ATTACH FITTINGS.  REMOVED DAMAGED SECTION OF BELTFRAME AND INSTALLED FILLER AND DOUBLERS PER SRM 53-03 FIG 34 SHEET 4.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON LONGERON 28L, AT STATION 1330, CORROSION REF C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND SEVEN CRACKS RANGING FROM .25 INCH TO .5 INCH, AT BELTFRAME 1416 AT FASTENERS TO LONGERON 3L, 4L, 5L, 6L, 4R, AND 5R.  REPAIRED BELTFRAME PER SRM 53-04.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH BY 1 INCH HOLE TAIL COMPARTMENT STATION 1418, LONGERON 8R.  SPLICED INNEW SECTION OF LONGERON. (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN FORWARD UPPER WINDOW FRAME STATION 845.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-30-06.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1307 FLOOR BEAM, RIGHT SIDE.  MANUFACTURED NEW FLOOR SUPPORT, L ANGLES AND SUPPORTS.  SPLICED IN NEW SECTION PER USAIR TYPICAL REPAIR 53-10-14 AND USAIREA NR 31216.  (M)


REMARKS:
CLT - FL 2761, EN ROUTE TO MIA, LEFT ENGINE OVERHEAT LIGHT CAME ON AND EGT PEGGED AT 1250 DEGREES.  FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO CLT SET WAS 20 MINUTES.  MAINTENANCE REPLACED NR 1 ENGINE EGT SOFT CORE HARNESS AND 6 O'CLOCK THERMOCOUPLE HARNESS.  NR 1 EGT SYSTEM OPS CHECKED NORMAL.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 2 SKIN CORROSION .063 DEEP AROUND FILLET SCREW HOLE STATION 807, LONGERON 29R AREA.  CORROSION TASK NR C22-57301.  REMOVED CORROSION AND ACCOMPLISHED DOUBLER REPAIR PER SRM 53-14 FIG 53.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND CANTED FRAME 1104 AT UPPER ATTACH FASTENER CRACK .5 INCH LONGERON 4L.  SPLICEDIN NEW SECTION OF FRAME PER SRM 53-03 FIG 30.  (M)


REMARKS:
PIT - DURING RON CHECK, 1.25 INCH RUNNING FORE AND AFT AT AFT PASSENGER DOOR FLOOR SILL PLATE SUPPORT ANGLE.  INSTALLEDDOUBLER REPAIR PER USAIR EA NR 28484A AND SRM 53-05 FIG 40.  (M)


REMARKS:
PIT - DURING C-3 INSPECTION, FOUND 2 INCH CRACK LEFT FORWARD EMERGENCY EXIT WINDOW JAMB PAN FORWARD OF LATCH PIN AND A .5 INCH CRACK AFT OF LATCH PIN.  STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 32.  (M)


REMARKS:
PIT - DURING B-CHECK INSPECTION, FOUND .25 INCH BY .5 INCH BY .022 DEEP CHAF MARK, AFT PRESSURE BULKHEAD AFT SIDE LEFT BULKHEAD SKIN.  INSTALLED .063 DOUBLER AND .025 FINGER DOUBLER PER USAIR EA NR 31415.


REMARKS:
PIT - FLT NR 591 - AFTER TAKEOFF AT APPROXIMATELY 2000, NR 1 THRUST REVERSER LIGHT FLICKERED ON AND OFF. AT 3000, THE PROCEDURE LIGHT CAME ON STEADY.  CREW ELECTED TO RETURN TO FIELD.  NO EMERGENCY DECLARED.  MEL WAS ADDED AND FLIGHT DEPARTED TO SDF WITH DELAY.  ADJUSTED THE LOWER AND UPPER DOOR SWITCH AND ACTUATOR SWITCH.  (M)


REMARKS:
PIT - FLIGHT 464 - PIREP READS, CHECK BULBS IN CABIN OVERHEAD EMERGENCY EXIT LIGHTS.  REPLACED LIGHT PLATE ASSEMBLYS INFORWARD CABIN AND MID CABIN EMERGENCY EXIT SIGNS.  OPS CHECKED.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND .025 INCH CRACK ROUTED OUT TO A . 375 INCH HOLE IN AFT DOOR JAMB, FORWARD CARGO BETWEEN 2ND AND 3RD STOP.  INSTALLED DOUBLER REPAIR PER USAIR EA NR 27454 REV A.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK STATION 1437, LONGERON 12L IN FRAME WEB.  REPLACED CRACKED FRAME AND INSTALLED DOUBLER 7075 T-6 .050 PER SRM 53-01 FIG 2.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK LEFT FORWARD EMERGENCY EXIT DOOR (OVER WING EXIT).  STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03 FIG 1.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK AT STATION 1510 LONGERON 20 LEFT.  INSTALLED DOUBLER REPAIR PER SRM 51-01.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND SKIN DAMAGE 2 INCH BY .5 INCH ON DOOR FRAME AREA STATION 1211, AFT CARGO DOOR.  INSTALLED FILLER AND DOUBLER REPAIR (EXTERNAL) PER SRM 53-05 FIG 80.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND 2 INCH CRACK LONGERON 30 SPLICE DOUBLER BETWEEN STATION 484 AND 503.  REPLACED SPLICE DOUBLER PER SRM 53-02.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND PREVIOUS REPAIR CLASS 3, UPPER AFT AREA OF MED SKIN.  REMOVED PREVIOUS REPAIR AND INSTALLED CLASS 1 REPAIR PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 256 LEFT INBOARD SEAT TRACK.  CORROSION TASK NR C58-53302.  REPLACED SEAT TRACK SECTION PER SRM 53-05 FIG 4.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK AFT JAMB BETWEEN 2ND AND 3RD STOPS FOR BOTTOM (FORWARD CARGO).  INSTALLED PERMANENT REPAIR PER 53-05 FIG 4 AND USAIR EA NR 27454.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK, LEFT AFT EMERGENCY EXIT DOOR TOP PAN LEFT STOP.  SID REF 52-21-003.  REMOVED AND REPLACED EXIT DOOR.  (M)


REMARKS:
PIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 1297, LEFT INBOARD SEAT TRACK.  REPLACED SECTION OFSEAT TRACK PER SRM 53-05 FIG 4.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2.1 INCH BY 24 INCH CORRODED AREAS, FORWARD SERVICE DOOR Z-ANGLE.  CLEANED AND TREATED Z-ANGLE.  REPLACED ASSOCIATED STRAP ANGLE.  REPAIRED PER SRM 51-10-2, SRM 53-10-51, BOEING DRAWING 65-45875.  LEVEL 1 CORROSION, CORROSION TASK NR C53-107-02.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA IN 4 PLACES ON INTERCOSTAL BETWEEN BS 328 TO BS 344.17 AT LBL 10.  REPLACED INTERCOSTAL WITH NEW PART.  REPAIRED PER SRM 53-10-51.  LEVEL 1 CORROSION, CORROSIONTASK NR C53-107-02.  (M)


REMARKS:
CLT - DURING A UNSCHEDULED MAINTENANCE INSPECTION, VISUALLY FOUND A 6 INCH BY 4 INCH .5 INCH BY .150 INCH DENT WITH 9.5INCH CRACK, LOCATED LEFT WBL 86 AT THE WING LEADING EDGE.  INSTALLED INTERIM REPAIR PER EA 40063.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA, BS 947 TO 967, ON INTERCOSTAL.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 16 INCHES BY 1 INCH CORROSION BS 312 TO BS 328, ON STRINGER.  REMOVED CORROSION, FABRICATED REPAIR AND SHIMS.  REPAIRED SRM 53-00-03 FIG 201, PG 207.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH BY .15625 DENT, AFT ENTRY DOOR AFT REAR UPPER CORNER.INSTALLED DOUBLER, REPAIRED PER SRM 52-00-01, FIG 206.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH DENT CENTER OF CARGO DOOR, 3 INCHES FORWARD OF AFT EDGE.  FABRICATED REPAIR DOUBLER FROM2024-T3, .063 AND INSTALLED 6 INCH BY 7 INCH DOUBLER.  REPAIRED PER SRM 52-00-01 PAGE 203.  (M)


REMARKS:
PIT - DURING C-1 CHECK CARD NR J9-50-0949, .1250 INCH CRACK FROM RIVET STATION 639 JUST BELOW LONGERON 1.  INSTALLED CLASS 2 TEMPORARY REPAIR DOUBLER PER SRM 53-04 PAGE 55, FIG 12B.  (M)


REMARKS:
PIT - DURING C-3 CHECK CARD 9-46-80-146, FOUND .3750 INCH CRACK BOTH SIDES OF 4TH DOOR STOP HOLE FROM BOTTOM, STATION 200 LEFT.  INSTALLED DOUBLER PER EA NR 311550.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND WEB NR 3 CRUSHED 10 INCH ALONG ITS LENGTH BETWEEN RIB NR 2 AND NR 4 OF LOWER FLANGEON TAIL BOX STRUCTURE.  REPLACED WEB NR 3 AS PER SRM 57-22-03.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND WEB NR 4 CRUSHED 4 INCH BETWEEN RIB NR 2 AND NR 4 LOWER FLANGE ON TAILBOX STRUCTURE.  FABRICATED NEW WEB.  REPAIRED WEB NR IV AS PER SRM 57-22-03.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND 4 INCH BY 6 INCH TEARS THROUGH SKIN AT WEBS 3 AND 4 BETWEEN RIBS 2 AND 4 OF LOWER SKIN TAIL BOX STRUCTURE.  FABRICATED NEW SKIN.  REPLACED LOWER SKIN ON TAIL BOX STRUCTURE PER SRM 51-11-42 AND 57-01-00.(M)


REMARKS:
CLT - .5 INCH CRACK AT NR 4 FORWARD CAP RIB AT LOWER FLANGE RADIUS AND TORQUE ROD CUT OUT.  CRACK WAS VISUALLY FOUND BYCLT INSPECTION.  REPAIRED NR 4 CAP RIB.  FABRICATED NEW RIB, PER SRM 57-02-03 AND SRM 20-30-06.  (M)


REMARKS:
SFO - FL0066, AFTER TAKEOFF FROM SFO, CREW RECEIVED THE RIGHT ENGINE HYDRAULIC PUMP OVERHEAT LIGHT, RIGHT ELECTRIC PUMPOVERHEAT LIGHT, AND THE ASSOCIATED EICAS MESSAGES.  FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP.  (M)


REMARKS:
PIT - FLT 115, ENROUTE PIT-SEA, NR 1 ENGINE BEGAN TO VIBRATE.  REDUCTION IN POWER DID NOT ELIMINATE THE VIBRATION.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  ENGINE WAS NOT SHUT DOWN IN FLIGHT.  MAINTENANCE INSPECTED THEENGINE INLET AND EXHAUST SECTIONS, AND FOUND THE RUBBER SEALS ON THE ANNULUS FILLERS TO BE OUT OF POSITION.  THE STRIPSWERE REPOSITIONED.  (M)


REMARKS:
STL - FL 63, EN ROUTE PHL-SFO, RIGHT ENGINE BEGAN LOSING POWER.  CREW COULD NOT GET MORE THAN 3000 LB/HR AT FORWARD THROTTLE STOP, OR LESS THAT 1500 LB/HR AT IDLE.  FLIGHT DIVERTED TO STL AND LANDED WITH NO FURTHER INCIDENT.  ENGINE WAS NOT SHUT DOWN IN FLIGHT.  MAINTENANCE FOUND A PIN HOLE IN THE LINE FROM P1 ACCUMULATOR, AND REPLACED THE LINE.  (M)


REMARKS:
EWR - FLT NR 497 - AFTER TAKEOFF, THE CREW WAS UNABLE TO RETRACT THE NOSE GEAR.  THE CAPTAIN CYCLED THE GEAR, BUT FAILED TO GET THE GREEN LIGHT.  THE FLT RETURNED TO EWR AND LANDED WITHOUT INCIDENT.  REMOVED AND REPLACED NOSE GEAR SHRADER VALVE O-RING.  PERFORMED FULL NOSE STRUT SERVICING.  (M)


REMARKS:
MCI - FLT 987 - AFTER TAKEOFF, THE CREW COULD NOT RETRACT THE NOSE GEAR.  THE FLT RETURNED TO MCI AND LANDED WITHOUT FURTHER INCIDENT.  REMOVED AND REPLACED NOSE GEAR SHRADER VALVE O-RING.  SERVICED STRUT WITH NITROGEN.  LEAK CHECK OK.  (M)


REMARKS:
PHL - FLT NR 1926 - DURING TAKEOFF, CAPTAINS WINDSHIELD CRACKED AND THEN SHATTERED.  THE FLT RETURNED TO PHL AND LANDEDWITHOUT FURTHER INCIDENT.  REMOVED AND REPLACED CAPTAINS SIDE WINDSHIELD.  (M)


REMARKS:
CLT - FLT 880 - AFTER RETRACTING GEAR, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON.  THE CAPTAIN DECIDED TO RETURN TO CLT.  THE FLT LANDED WITHOUT FURTHER INCIDENT.  RECYCLED LEFT MAIN GEAR THROUGH 5 CYCLES ON GROUND.  GEAR INDICATION NORMAL.  AIRCRAFT OK FOR SERVICE.  (M)


REMARKS:
IND - FLT NR 987 - AT CRUISE, NR 2 ENGINE ADVANCED TO FULL THROTTLE AND WOULD NOT RESPOND TO CONTROLS.  THE CAPTAIN SHUT DOWN NR 2 ENGINE DIVERTED TO IND.  THE FLT LANDED WITHOUT FURTHER INCIDENT.  REMOVED AND REPLACED RIGHT FUEL CONTROL.RAN ENGINE.  OPS CHECK OK.  (M)


REMARKS:
ORF - MTC DISCREPANCY, EMERGENCY FLOOR LIGHTING INOP ROW 16.  REPLACED INVERTER.  (M)


REMARKS:
CAPTAIN ADVISED THAT ON TAKEOFF ROLL AND AND JUST AFTER REACHING V2, A STRONG VIBRATION WAS NOTICED.  A PRECAUTIONARY FLY-BY WAS MADE BY CLT TOWER AND THE LEFT INBOARD TIRE WAS APPARENTLY BLOWN.  NO EMERGENCY WAS DECLARED, HOWEVER, CFR WASCALLED OUT BY ATC.  THE FLIGHT RETURNED TO FIELD CLT AND LANDED WITHOUT INCIDENT.  (M)


REMARKS:
CLT - FL 2040 - EN ROUTE TO LGA, CREW NOTED PERIODIC SPIKING FROM THE NR 1 GENERATOR, WHICH CAUSED TR NR 1 CIRCUIT BREAKER TO TRIP.  CREW DISCONNECTED THE GENERATOR, AND COULD NOT GET THE APU TO START.  FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER PROBLEMS.  THE GENERATOR WAS PLACED ON MEL AND SUBSEQUENTLY REPLACED DUE TO A BURNED 'B' PHASE TERMINAL.  THE APU WAS INSPECTED AND STARTED SEVERAL TIMES WITH NO PROBLEMS NOTED.  (M)


REMARKS:
PIT - FLT NR 1567 - AIRCRAFT DISPATCHED WITH MEL 21-1A ON RIGHT PACK.  COULD NOT PRESSURIZE AFTER TAKEOFF.  RETURNED TOPIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE PRESSURIZED AIRCRAFT TO 6 PSID.  NO DEFECTS NOTED.  RELEASED AIRCRAFT FORSERVICE.  (M)


REMARKS:
MSP - FLT NR 1090 - ON CLIMB-OUT, PASSING THROUGH 10,000 FEET, NR 2 ENGINE LOP LIGHT ILLUMINATED ALONG WITH OIL QUANTITY AND OIL PRESSURE DECREASE TO ZERO.  FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO MSP WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND THE NR 4 BEARING PRESSURE LINE LOOSE, TIGHTENED SAME.  ALSO, FOUND NR 4 BEARING CHIP DETECTOR MISSING AND REPLACED CHIP DETECTOR.  SERVICED OIL AND RAN ENGINE.  OPS NORMAL.  REPLACED ENGINE DUE TO LOW OIL PRESSURE OPERATION AND RETURNED AIRCRAFT TO SERVICE.  (M)


REMARKS:
MCO - FLT NR 0417 - EN ROUTE FLL TO PIT, NR 1 ENGINE OIL TEMP CLIMBED ABOVE RED RADIAL.  PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED PER PILOTS HANDBOOK.  FLIGHT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT.  MAINTENANCE CHECKED ALL CHIP DETECTORS, NO PROBLEMS FOUND.  REPLACED OIL TEMP BULB AND RAN ENGINE AT CRUISE POWER.  OIL TEMP INDICATION CHECKED GOOD.  (M)


REMARKS:
BHM - DURING CLIMBOUT PASSING 13,000 FT, NUMBER 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED.  ALSO, ENGINE OIL TEMP BEGAN INCREASING.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING.  INSPECTED, MEL'D NUMBER 1 ENGINE START VALVE PER 80-2 AND CONTINUED.


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND 3 INCH CRACK AND A .75 INCH IN VENTRAL DOOR APERTURE TO LEFT CORNER.  ROUTED OUT CRACKED AREAS AND INSTALLED FILLER AND DOUBLERS PER DRW NR J060088 AND USAIR EA NR 31358.  (M)


REMARKS:
CLT - DURING A PCI INSPECTION, A 10 INCH BY 1 INCH CORROSION WAS FOUND AT STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360.  REPLACED END STRINGER 28R, RBL 6.  (M)


REMARKS:
AT 33,000 FL, EXPERIENCED CABIN PRESSURE DROP.  INITIATED EMERGENCY DESCENT, O2 MASKS WERE NOT DEPLOYED.  AIRCRAFT DIVERTED TO AUS AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND RIGHT A/C PACK WATER SEPARATOR FWD CLAMP BROKEN.  REPLACED CLAMP PER BOEING M/M.


REMARKS:
ATL - FLT 522 - FLT RETURNED TO ATL DUE TO HYDRAULIC LEAK.  REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY PER MM 32-40.


REMARKS:
PHL/ATL - FLT 219 - AT THE GATE IN PHL, THE FLIGHT CREW FOUND SMOKE IN THE CABIN.  FOUND APU (PN GTCP8598D) LEAKING OILCAUSING SMOKE IN THE CABIN; THE APU WAS PLACED ON MEL.


REMARKS:
ATL - FLT 505 - FUEL STREAMING OUT OF RIGHT WING TIP, NOTED ON TAKEOFF AND CLIMB-OUT.  AIRCRAFT RETURNED TO ATL.  FOUNDMANIFOLD DRAIN VALVE STUCK OPEN, REPOSITIONED VALVE.  VALVE WAS CLEANED AND OPERATION WAS CHECKED FOR FREEDOM OF MOVEMENT PER MM 28-12.


REMARKS:
ATL - FLT 919 - AIRCRAFT RETURN, ON THE CLIMB-OUT OF ATL AT 17,000 FEET, 300 KNOTS, THE FIRST OFFICER DISCOVERED FORWARD OUTER PANE WINDOW SPIDER-WEBBED.  REFERENCE, OPERATOR CONTROL NR 95ZZZX6372.


REMARKS:
ATL - FLT 919 - AIRCRAFT RETURN, ON THE CLIMB, OUT OF ATL AT 17,000 FEET, 300 KNOTS, THE FIRST OFFICER DISCOVERED FORWARD OUTER PANE WINDOW SPIDER-WEBBED.  REFERENCE, OPERATOR  CONTROL NR 95ZZZX6371.


REMARKS:
DFW/ATL - FLT 224 - ON DESCENT INTO ATL, LOST PRESSURIZATION.  OXYGEN MASKS DID NOT DROP DUE TO FLIGHT LEVEL.  INSTALLED BOTH RIGHT AND LEFT AIR CYCLE MACHINE SUPPLY DUCTS, AND RIGHT AND LEFT COALESCER BAGS.


REMARKS:
ATL/MEM - FLT 512 - CABIN PRESSURE LOST AT FL 240.  CABIN ALTITUDE INCREASED TO OVER 15,000 FEET DURING EMERGENCY DESCENT.  MASKS DEPLOYED, UNABLE TO CONTROL CABIN WITH MANUAL CONTROLLER.  INSPECTED TAIL SECTION FOR BLOWN DUCTS, CHECKED OUTFLOW VALVE, PERFORMED DECAY RATE CHECK AND STOWED ALL OXYGEN MASKS AND PERFORMED DROP CHECK PER MM 35-20.  NO DEFECTS NOTED.


REMARKS:
FLT 520 - CENTER TANK VENTED 3,000 POUNDS OF FUEL THROUGH FUEL VENT.  REPLACED LEFT WING FUEL SUPPLY PIPE ASSEMBLY.


REMARKS:
NR 1 ENGINE OIL TEMPERATURE EXCEEDED 120 DEGREES FOR 12 MINUTES, MAXIMUM TEMPERATURE, 139 DEGREES.  REPLACED FUEL HEAT VALVE.  DRAINED AND REPLACED ENGINE OIL.  REMOVED AND REPLACED OIL SCREEN PER MM 72-00, 518C.  CHECKS OK.  NO LEAKS ON RUN-UP.


REMARKS:
ATL - FLT 276 - AFTER TAKEOFF, AIRCRAFT EXPERIENCED FUEL VENTING OVERBOARD.  AIRCRAFT RETURNED TO ATL.  FOUND LT WING INDICATION READING LOW.  WING OVER-SERVICED, BACK FLUSHED FUEL, NO TRANSFER OCCURRED.


REMARKS:
EN ROUTE, NUMBER 1 TRANSFER BUSS CIRCUIT BREAKER TRIPPED.  RESET BREAKER, BUT TRIPPED AGAIN.  CABIN PRESSURE BEGAN TO CLIMB IN AUTO.  AIRCRAFT DESCENDED TO 10,000, DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING.  INSPECTED, REPLACED R3 RELAY AND PERFORMED BUSS TRANSFER CHECK.


REMARKS:
FOUND SECTION OF EMERGENCY ESCAPE PATH LIGHTING INOP.  SECURED LIGHTING AND RECONNECTED WIRING.


REMARKS:
LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION.  CYCLED GEAR, NO HELP.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACED LEFT GEAR UPLOCK SWITCH PER BOEING M/M.


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND RT BS 727 O/B CHORD FRAME AT STRINGER 18A CRACKED FROM FWD EDGE OF FLANGE TO SECONDFASTENER.  REPAIRED PER SWA ACO 651-53 REV 2.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZER STRAPS CRACKED IN E AND E COMPT BS 314 RBL 30 ON BOTTOM OF FLOORBEAM ANDAT LBL 12.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZER STRAP CRACKED AT LEFT BS 344.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND MAIN ENTRY DOOR AFT INNER PANEL SUPPORT ATTACH ANGLE CRACKED BETWEEN NUMBER 3 AND 4STOP FITTINGS.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND HORIZONTAL STAB IN SPAR SKIN CRACKED.  REPAIRED PER SWA RA 1-355-201.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND RIGHT I/B FLOORBEAM STRAP CRACKED IN E AND E COMPT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 16R CRACKED AT FASTENER HOLES AFT OF WING ICE LIGHT FRAME RIGHT SIDE.  REPAIRED PER SWA ACO 6405-53.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312 RBL 7.  REPAIRED PER SWA RA 1-253-1402.


REMARKS:
DURING CLIMBOUT EXPERIENCED BUFFETING, THEN FWD CARGO COMPT DOOR OPEN LIGHT ILLUMINATED AND PRESSURIZATION REMAINED NORMAL.  AIRCRAFT DESCENDED TO 6,000 AND RETURNED TO BOI.  INSPECTED AND LOCKED DOOR NORMALLY.


REMARKS:
CAPTAIN'S WINDSHIELD CRACKED.  AIRCRAFT DIVERTED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACED PER BOEING M/M.


REMARKS:
FLT NR 547 - PHL - AIR RETURN, AFT AIRSTAIR DOOR LIGHT ILLUMINATED.  RECYCLED AFT STAIRS, SYSTEM CHECK NORMAL.  (M)


REMARKS:
ON FLT 440 - ATL - AIR RETURN, THE RIGH PACK OVERHEATED IN FLIGHT.  THE TEMP CONTROL KNOB HAD NO EFFECT ON VALVE POSITION WHICH WAS IN FULL HOT.  ASSIGNED MEL NR DM5116, SEQ 21-01 RIGHT PACK INOP.


REMARKS:
STL - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE RED NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE.  FOUND NOSE LANDING GEAR LOCK SWITCH, MFG P/N H10-1015-3, MALFUNCTIONING.  REPLACED NOSE LANDING GEAR LOCK SWITCH AND NOSE LANDING GEAR INDICATION SYSTEM OPERATION CHECKED NORMAL.


REMARKS:
JFK - DURING CRUISE SHUT DOWN NR 4 ENGINE, S/N 4199, DUE TO DECREASING OIL QUANTITY.  FOUND OIL LEAKING IN ENGINE CORE. REPLACED NR 4 ENGINE AND ENGINE OPERATION CHECKED NORMAL.


REMARKS:
STL - AFTER TAKEOFF NOSE LANDING GEAR WOULD NOT RETRACT.  FOUND NOSE LANDING GEAR STRUT SEALS PREVENTING FULL EXTENSIONOF NOSE LANDING GEAR STRUT.  REPLACED NOSE LANDING GEAR STRUT SEALS AND NOSE LANDING GEAR OPERATION CHECKED NORMAL.


REMARKS:
JFK - DURING CRUISE A STRONG NON-ELECTRICAL BURNING ODOR WAS DETECTED IN GALLEY 'A'.  REMOVED AND REPLACED DIRTY OVEN, OPERATIONAL CHECK NORMAL.


REMARKS:
JFK - DURING CRUISE, DETECTED BURNING SMELL IN NR 1 SERVICE CENTER.  REMOVED AND REPLACED BALLAST, MFG P/N 11-2556-3.  OPERATIONAL CHECK OF BALLAST AND WIRING OK.


REMARKS:
STL - DURING CLIMB, SHUT DOWN NR 3 ENGINE, S/N 3901, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION.  FOUND FILTER BYPASS PRESSURE SWITCH, MFG P/N A00803-2, MALFUNCTIONING.  REPLACED OIL FILTER BYPASS SWITCH.  ENGINE OPERATION AND OIL BYPASS LIGHT SYSTEM CHECKED NORMAL.  (M)


REMARKS:
CDG - DURING CLIMB NR 2 ENGINE, S/N 4159, SPOOLED DOWN.  SHUTDOWN ENGINE PER STANDARD PROCEDURES.  FOUND ENGINE FUEL PUMP, MFG P/N 705301-32, MALFUNCTIONING.  REPLACED ENGINE FUEL PUMP.  ENGINE OPERATION CHECK NORMAL.


REMARKS:
ATL - DURING CRUISE, FUEL SMELL DETECTED IN CABIN.  FOUND FUEL LEAK FROM CENTER TANK IN RIGHT WHEEL WELL.


REMARKS:
OKC - DURING CLIMB NR 3 ENGINE, S/N 1910, SPOOLED DOWN.  SHUT DOWN ENGINE FUEL PUMP, MFG P/N 378201-7, MALFUNCTIONING.REPLACED ENGINE FUEL PUMP AND ENGINE PERFORMANCE CHECKED NORMAL.


REMARKS:
STL - DURING C-CHECK, FOUND TWO INCH CRACK IN NR 2 DOOR BEAM FORWARD END.  REPAIRED PER SRM 51-30 AND STANDARD PRACTICES.


REMARKS:
MCI - DURING C-CHECK, FOUND A TWO INCH CRACK BETWEEN BEADED EXTRUSION IN HORIZONTAL PRESSURE DECK WEB OF LEFT MLG WHEELWELL, AFT OUTBOARD CORNER OF WHEEL WELL CEILING, BS 948, LBL 59.  INSTALLED DOUBLER REPAIR PER SERVICE BULLETIN 727-53-0149, DRAWING 65-8960 AND TWA STANDARD PRACTICES.


REMARKS:
STL - DURING C-CHECK, FOUND A TWO INCH CRACK IN FLOOR BEAM AT CENTER AISLE AREA, STATION 239.  REPAIRED PER ARA 8749.


REMARKS:
MCI - DURING C-CHECK, FOUND A 1.5 INCH CRACK IN LEFT SIDE FRAME WEB, FS 783.85.  STOP DRILLED CRACK AND REPAIRED PER SRM 51-10-1, PAGE 6A.


REMARKS:
IND - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN GEAR DOOR WARNING LIGHT REMAINED ON.  GEAR CYCLED, LIGHT WENT OUT.  INSPECTED AND CLEANED GEAR DOOR SWITCH.  OPERATIONAL CHECK GOOD.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON SKIN DOUBLER BETWEEN STRINGER 32 AND 33, FS 529 TO FS 549.  REPAIRED PER SRM 53-31-00, FIGURE 826.


REMARKS:
MCI - DURING C-CHECK, FOUND CRACK IN STRINGER FORWARD SIDE OF STRINGER TO RIB, INSIDE FUEL TANK, LEFT WING STATION 656.56.  REPAIRED PER SRM 57-10-4, FIGURE 8 AND SERVICE BULLETIN 727-57A-159, FIGURE 4.


REMARKS:
INBOUND TO ATL, FLT NR 47, RIGHT GEAR DOOR WARNING LIGHT DID NOT COME ON WHEN GEAR WAS PUT UP OR DOWN AT FE PANEL.  REMOVED AND REPLACED DEFECTIVE CANNON PLUG ON RIGHT DOOR WARNING SWITCH, PER MM 32-62-0, OPS CHECKED OK.  (M)


REMARKS:
PIT - THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERTIVE.  MAINTENANCE REPLACED THE BATTERIES.  OPERATIONS CHECKED GOOD.(M)


REMARKS:
PIT - FLT NR 473 - CREW MOVED EMERGENCY DOOR HANDLE FOR MAIN ENTRY DOOR.  THEREFORE MAIN ENTRY DOOR WOULD NOT OPERATE AT DEPARTURE TIME.  RESET DOOR.  OPS CHECKED NORMAL.  (M)


REMARKS:
SDF - FLT NR 846 - AFTER TAKEOFF, RIGHT MAIN RED GEAR LIGHT REMAINED ILLUMINATED.  FOLLOWED ABNORMAL PROCEDURE 1-312-5 OF PHB AND RECYCLED GEAR.  AFTER RECYCLE ALL RED AND AMBER LIGHTS STAYED ON ALONG WITH GREEN LIGHTS.  THEN FOLLOWED ABNORMAL PROCEDURE 1-312-4 AF PHB AND CYCLED GEAR DOWN AND UP.  RED RIGHT GEAR STAYED ON.  FOLLOWED PROCEDURE 1-312-5 AGAIN,NO HELP.  RETURNED TO SDF, LANDING NORM.  FOUND RIGHT MLG DOOR NOT CLOSING PROPERLY.  ADJUSTED DOOR ACTUATOR.  AFT AND LANDING GEAR OPERATED NORMAL.  ALL INDICATIONS NORMAL PER M/M.  AIRCRAFT OK FOR SERVICE.  (M)


REMARKS:
CLT - FLT NR 379 - AFTER TAKEOFF, CLIMBING THROUGH FL 100, THE CREW FELT AND ENGINE VIBRATION.  THERE WAS A DROP IN EGT, DROP IN FUEL FLOW AND A DROP IN LP RPM.  THE CREW DID NOT DECLARE AN EMERGENCY AND THE FLIGHT RETURNED TO FIELD AT CLT.  THE ATC TOWER DID CALL OUT THE CFR EQUIPMENT.  THE FLIGHT LANDED WITHOUT INCIDENT.  REPLACED NR 1 ENGINE FUEL FLOW GOVERNOR PER MM 73-20-11.  LEAK AND RUN CHECK NORM.  NO VIBRATION FELT AT 96 PERCENT HP.  (M)


REMARKS:
EWR - FL 1468 - EN ROUTE DCA-BOS, WITH THE NR 1 GENERATOR ON MEL AND THE APU RUNNING, THE APU SHUT DOWN DUE TO HIGH OILTEMPERATURE.  FLIGHT DIVERTED TO EWR AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE TROUBLESHOT AND COULD NOT FIND APROBLEM WITH THE APU.  THE APU OIL AND OIL FILTER WERE CHANGED.   SUBSEQUENTLY, MAINTENANCE FOUND THAT THE APU OIL INLET COOLER WAS BLOCKED, CAUSING THE HIGH TEMPERATURES.  (M)


REMARKS:
PHL - FL 330, CLIMBING OUT OF LGA, AT FL 280, THE LEFT ENGINE SHUT DOWN AND COULD NOT BE RESTARTED.  FLIGHT DIVERTED TOPHL AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN FUEL PUMP FAILED AND REPLACED IT.  (M)


REMARKS:
STL - FLT NR 0091 - EN ROUTE FROM PIT TO SAN, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE WAS FLUCTUATING BETWEEN 35 AND 40 PSI.  FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED TO STL WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE MEL'D THE NR 2 ENGINE OIL QUANTITY INDICATION.  THE OIL QUANTITY TRANSMITTER WAS REPLACED ONTHE RON.  MAINTENANCE ALSO CLEANED THE CONNECTOR ON THE OIL PRESSURE TRANSMITTER.  RAN ENGINE AND OPS WAS NORMAL.  (M)


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND VERT STAB 5TH RIB ASSEMBLY CRACKED AT FASTENER HOLE ON LEFT SIDE.  REPAIRED PER BOEING M/M.


REMARKS:
DURING SCHEDULED CHECK, FOUND LT WING I/B UPPER AFT WING PANEL RIB CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND THE FOLLOWING STRINGER CLIPS CRACKED: S10 AND 11R AT BS 277, S8L AT BS 685, S10L AT BS 663, S5L AND S8R AT BS 616, S8L AT BS 639, S19R AT BS 500D, S22L AT BS 380, S19 TO 20L AT BS 938, S8L AT BS 616.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB AND STRINGER CRACKED AT BS 333, S8R.  REPAIRED STRINGER AND REPLACED WEB PER BOEINGSRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER FLANGE CRACKED AT BS 475, S22R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED AT BS 616 BETWEEN S7 AND 8L, BETWEEN S15 AND 14L, BS 360, WL 228.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE LEFT FRAME I/B CHORD CRACKED AT LOWER FASTENER HOLE, BS 616 WL 200.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE LEFT FRAME CRACKED AT BS 294.5 WL 208 RBL 54.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 294.5, RIGHT SIDE AT S4R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 294 S7R, BS 616 S9L, BS 787 S9L, BS 907 S9L, BS 827 S9L, BS 867 S9L, BS 847 S9L, AND BS 887 S9L.  REPAIRED ALL PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 46 TO 51, WL 170.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178 WL 200 TO 201 RBL 5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED FROM BS 360 TO 375 BETWEEN S4 AND 6L AND AT BS 962 TO 971 BETWEEN S19 TO 20L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318 BETWEEN 18 AND 19, BS 356 BETWEEN S23 TO 24R, BS 818 LBL7 RBL 12 WL 151, BS 767 BETWEEN S19 AND 20L AND AT BS 203.8 LBL 21 WL 172.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178 WL 218 RBL 10 TO 12 AND AT WL 217 LBL 11 TO 12, BS 178 WL 212 TO 213 RBL 5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5 LBL 5 TO RBL 32 WL 208 AND 207.  REPAIRED PER TRAMCO EWO 95-0727.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 328 RBL 10 WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOORWAY LOWER AFT CORNER SKIN CRACKED AT BS 328 RBL 64 WL 210.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACK IN SKIN AT AFT EDGE OF EQUIPMENT COOLING EXHAUST, BS 380 LBL 5 WL 148.  REPAIRED PER BOEING SRM.


REMARKS:
DURING CLIMBOUT, RIGHT MAIN GEAR EXTENDED TO FULL DOWN POSITION.  CREW RECYCLED GEAR TO UP POSITION AND GEAR OPERATED NORMALLY FOR REMAINDER OF FLIGHT.  AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT.  REPLACED RIGHT MAIN GEAR UPLOCKACTUATOR, INSPECTED WALKING BEAM BOLT AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
EN ROUTE, NOTED HYDRAULIC QUANTITY DROP.  DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND LEFT MAIN GEAR BRAKE LINE LEAKING.  REMOVED, REPLACED LINE AND LEAKED CHECKED PER BOEING M/M.


REMARKS:
PIT - DURING Q-3/C-6 INSPECTION, FOUND 1 INCH CRACK IN FORWARD RIGHT OVERWING EXIT DOOR PAN UPPER AFT DOOR STOP.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03.  (M)


REMARKS:
PIT - DURING Q-3/C-6 INSPECTION, FOUND LEVEL 1 CORROSION ON WEB OF AFT CARGO WALL AT STATION 1338 PREVIOUSLY REWORKED CORROSION REF NR C57-53300.  MANUFACTURED AND SPLICED IN NEW WEB SECTION AND ANGLES PER USAIR TYPICAL REPAIR 53-30-10.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 TO 2 INCH DIAMETER SPOTS OF CORROSION ON THE FLOOR BEAM AT SCREW HOLES, BS 986 LBL 45 TO RBL 45.  CUT OFF 'T' CAP AND INSTALLED NEW 'T' CAP AND REPAIR ANGLE.  REPAIRED PER EA 40072A.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 40 INCH CORROSION ON STRAP, STATION 800 TO 840.  INSTALLED NEW PART, REPAIRED PER SRM 51-10-02, DRAWING 65-47957.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 6 INCH CRACK AT HINGE LUGS, BS 328 FORWARD SERVICE DOOR LOWER GATE.  REPLACED HINGE ASSEMBLY.  REPAIRED PER SRM 51-10-2 AND MM 52-41-00.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND CORRODED SKIN PAST LIMITS OF EO 5492R274 PART IV STEPS 2 AND 3, ON NR 2 PYLON.  REPAIRED SKIN PER DRAWING 013N8774.  (M)


REMARKS:
CLT - FLT 2722 - ON APPROACH TO CLT, LEFT MAIN GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED.  DURING GO-AROUND, TOWER OBSERVED LEFT MAIN GEAR EXTEND ALONG WITH FLIGHT CREW GETTING GREEN INDICATION.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND RESTRICTOR CHECK VALVE TO DOWN SIDE OF UPLOCK PLUGGED.  REPLACED RESTRICTOR CHECK VALVE.  GEAR OPS CHECKED NORMAL.  (M)


REMARKS:
CLT - FLT 1276 - EN ROUTE MIA TO PHL, FLIGHT CREW NOTED A FAINT ODOR, POSSIBLY FUEL IN THE AFT GALLEY.  FLIGHT MADE A PRECAUTIONARY LANDING IN CLT WITHOUT INCIDENT.  MAINTENANCE INSPECTED AIRCRAFT FUEL SYSTEM.  PRESSURIZED AIRCRAFT, COULD NOT DUPLICATE.  (M)


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN DENTED AT BS 907, BETWEEN STRINGERS 22 AND 23L AND AT BS 940 AT S18 AND 19L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AT BS 713, LBL 24.5, WL 204.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND PRESSURE WEB CRACKED AT BS 178, WL 217, RBL 9.5 TO 13.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 928, RBL 14-55, WL 208.  REPAIRED PER SWA RA 1-253-423.


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 294, RBL 14 TO LBL 14, WL 208.  REPAIRED PER SWA TR 1-353-009.


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND STRINGER 27L CORRODED AT BS 1006.  REPAIRED PER BOEING SRM.


REMARKS:
UPON ARRIVAL OF FLT 586, TPA TO ATL, EMERGENCY POWER WOULD NOT TURN OFF.  MAINTENANCE REPLACED R2-7 TRANSFER BUS SENSE RELAY AND R2-7 GROUND REFUEL RELAY.  (M)


REMARKS:
PIT - DURING Q-3/C-6 INSPECTION, FOUND TWO .5 INCH CRACKS IN PAX DOOR RIVNUT BELOW BAYONET.  CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK STATION 520 FLOOR BEAM UPPER RADIUS RBL 25, WL 207.75.  DOUBLERS INSTALLED PER EA 40020, REF SB 737-53-1120.  REPAIRED PER EA 40020, REF SB 737-53-1120.  (M)


REMARKS:
INT - DURING Q-5 CHECK NDT INSPECTION, FOUND 1.25 INCH CRACK FLOOR BEAM, .75 INCH CRACK SEAT TRACK SUPPORT CHANNEL DETECTED BY VISUAL INSPECTION, STATION 520 FLOOR BEAM LBL 25, WL 207.75.  DOUBLERS INSTALLED PER EA 40020, REF SB 737-53-1120.  REPAIRED PER EA 40020, REF SB 737-53-1120.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO SKIN DENTS, AT STATION 265 TO 277 ABOVE STRINGER 11 R AND 13 R.  CUTOUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.  REPAIRED PER SRM 53-00-01.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, APPROXIMATELY 1 INCH BY 12 INCH AREA CORRODED STATION 952 BETWEEN LBL 25 AND LBL 51.  REPAIRED AND REPLACED INTERCOSTAL.  REPAIRED PER SRM DOCUMENT 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
IND - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 4 INCH BY 4 INCH CORRODED AREAS BETWEEN BS 794 AND BS 847 (AFT CARGO DOORWAY SILL).  INSTALLED NEW WEB.  REPAIRED PER SRM 51-10-02, DRAWING 65-47957.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORRODED AREA, ON INTERCOSTAL AT 25, BETWEEN BS 947 AND BS 967, WL 208.  REMOVED CORRODED INTERCOSTAL, DRILLED UP AND INSTALLED NEW INTERCOSTAL FROM STOCK P/N 65C333701.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 20 INCH CORRODED AREA, ON BEAM AT STATION 947 LBL 5 - RBL 15. INSTALLED CAP AND REPAIRED ANGLE.  REPAIRED PER EA 40080.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 59 INCHES CORRODED AREA, BS 947-1006, S-17 L (AFT ENTRY DOOR Z-ANGLE).  REMOVED CORRODED CHORD Z-ANGLE.  DRILLED UP AND INSTALLED NEW ANGLE FROM STOCK.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
FLT NR 2058 - CAPTAINS VERTICAL GYRO FAILED ON CLIMB-OUT.  FLIGHT RETURNED TO FIELD.  REPLACED NR 1 VERTICAL GYRO.  OPERATIONAL CHECK WAS NORMAL.  (M)


REMARKS:
MCI - DURING CHECK-C, FOUND .25 INCH CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER CUT-OUT.  REPAIRED PER SSRM 53-30-206.AIRCRAFT TOTAL TIME:  61,301 HOURS; 41,020 CYCLES.


REMARKS:
STL - FLT 464 - DURING CRUISE, EXPERIENCED A POSSIBLE LIGHTNING STRIKE WITH ACCOMPANYING AIR NOISE AND SMOKE IN THE CABIN.  ALL OPERATIONS AND INDICATIONS WERE NORMAL.  PERFORMED LIGHTNING STRIKE/STATIC DISCHARGE CONDITION CHECK.  CHECKED NR 1 ENGINE FOR POSSIBLE COMPRESSOR STALL, CHECKED TAIL COMPARTMENT AIR CONDITIONING SYSTEM.  ALL CHECKS WERE FOUND TO BE NORMAL.  CHECK C-1D - 5-18-95 - MCI.


REMARKS:
IND - FLT 444 - DURING CRUISE, SMOKE STARTED ENTERING CABIN.  DESCENDED TO 8,000 FEET.  FOUND APU OIL OVERSERVICED.  SERVICED APU TO PROPER LEVEL AND REPLACED BOTH COALESCER BAGS, MFG P/N 22D10.  AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL.  CHECK C-1A - 5-18-95 - MCI.


REMARKS:
PDX - FLT 173 - DURING CRUISE, 'D' GALLEY OVEN, MFG P/N 8203-11-0000, EMITTED SMOKE.  OVEN WAS TURNED OFF AND CIRCUIT BREAKER PULLED.  TROUBLESHOOTING UNDERWAY TO DETERMINE CAUSE.  OP-16 - 8-25-95 - MCI.


REMARKS:
PIT - FLT 0223 - EN ROUTE IND TO BWI, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE DROPPED TO RED LINE.  FLIGHT CREW SHUT DOWN NR 2 ENGINE AND DIVERTED TO PIT.  LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED RT ENGINE N2 ALTERNATOR AND ROTOR DUE TO INTERNAL FAILURE.  RAN ENGINE AND CHECKED CHIP DETECTORS AND OIL FILTERS.  OPS CHECKED GOOD.  (X)


REMARKS:
STL - AFTER TAKEOFF WHEN LANDING GEAR SELECTOR WAS RAISED, LANDING GEAR DID NOT RETRACT.  FOUND LANDING GEAR MAINTENANCE BYPASS HANDLE LATCH MALFUNCTION, MFG P/N H5000-2-125-218.  REPAIRED LOCK AND LANDING GEAR BYPASS HANDLE OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE.  VISUALLY CHECKED RIGHT MAIN LANDING GEAR, IT WAS DOWN AND LOCKED.  FOUND DEBRIS ON RIGHT MAIN LANDING GEAR INDICATIONSENSOR.  REMOVED DEBRIS FROM SENSOR AND LANDING GEAR INDICATION SYSTEM OPERATION CHECKED NORMAL.


REMARKS:
HNL - DURING CLIMB, SHUT DOWN NR 1 ENGINE, S/N 4165, DUE TO COMPRESSOR STALL AND RISING EGT.  FOUND METAL PARTICLES IN TAILPIPE AND TURBINE BLADE DAMAGE.  REPLACED ENGINE AND ENGINE OPERATION CHECKED NORMAL.


REMARKS:
SHV - DURING LANDING, WHEN GEAR HANDLE WAS EXTENDED, RIGHT GEAR RED AND GREEN LIGHTS DID NOT ILLUMINATE.  A FLY-BY WAS PERFORMED TO ENSURE GEAR WAS DOWN AND LOCKED.  REPLACED BROKEN WIRE, REFERENCE WIRING DIAGRAM 32-61-00.  OPERATIONAL CHECK NORMAL.


REMARKS:
HNL - AFTER TAKEOFF RIGHT WING LANDING GEAR WOULD NOT TILT FULL FORWARD.  LUBED RIGHT WING LANDING GEAR TRUCK PIVOT PIN.  JACKED AIRCRAFT AND PERFORMED OPERATIONAL CHECK OF LANDING GEAR TILT SYSTEM.  OPERATIONAL CHECK NORMAL.


REMARKS:
STL - DURING LANDING, EGRESS PATH LIGHTING AT R-2 DOOR CAME OUT OF TRACK.  REINSTALLED LIGHT STRIP, CHECKED WIRING, ANDLIGHT OPERATION CHECKED NORMAL.


REMARKS:
HNL - AFTER TAKEOFF, RIGHT WING LANDING GEAR TRUCK TILT LIGHT ILLUMINATED ON BOTH PRIMARY AND ALTERNATE.  REPLACED RIGHT WING GEAR TRUCK TILT ACTUATOR, MFG P/N 65B015397, AND CHECKED LANDING GEAR TRUCK TILT INDICATION.  LANDING GEAR INDICATION SYSTEMS CHECKED NORMAL.


REMARKS:
UPON ARRIVAL OF FLT 306, MIA-IAD, MX FOUND THE TAIL SKID AND SURROUNDING STRUCTURE DAMAGED APPARENTLY FROM GROUND CONTACT.  INSPECTED AND FERRIED AIRCRAFT TO LACI, ID 7A1 FOR STRUCTURE REPAIR.  PERFORMED NECESSARY REPAIRS TO STRUCTURE AND SKID IAW SRM 53-01, 53-04, 51-60, 51-30.


REMARKS:
EWR-ATL - FLT NR 9059 - UNABLE TO PRESSURIZE, AIR TURN BACK TO EWR.  FOUND L2 DOOR COCKED, LIGHTS OPS CHECKED GOOD, RESET DOOR, PRESSURIZED OK.  (M)


REMARKS:
PIT - DURING A Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN CUSP MEMBRANE WEB STATION 1032 OUTBOARD OF RT SEAT TRACK.  ACCOMPLISHED SPLICE REPAIR PER USAIR EA NR 315530A.  (M)


REMARKS:
CLT - FLT NR 947 - EMERGENCY EXIT LIGHTS FORWARD CABIN STAY ON WITH SWITCH IN ARMED OR OFF POSITION.  REPLACED BATTERY CHARGER.  EMERGENCY LIGHTS CHECK OK.  (M)


REMARKS:
PHL - FLT NR 1535 - CLIMBING THROUGH FL 310, CABIN ALTITUDE WAS CLIMBING AT 1000 FPM.  FLIGHT CREW WAS UNABLE TO CONTROL CABIN PRESSURE IN AUTO OR STANDBY.  RETURNED TO PHL AND LANDED WITHOUT INCIDENT.  PERFORMED PRESSURIZATION CHECK.  SYSTEM CHECKED NORMAL.  UNABLE TO DUPLICATE ANY DEFECT.  (M)


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 17L CRACKED AT END OUTBOARD OF FWD BULKHEAD OF APU COMPARTMENT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY FLOOR BEAM CORRODED AT SCREW HOLES, UPPER AND LOWER SURFACES AT AFT FLANGE AT BS 1006, LBL 15, 19 AND 23.  INSTALLED REPAIR STRAPS PER SWA RA 1-253-1411.


REMARKS:
DURING DESCENT, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  REMOVED AND REPLACED ENGINE/APU FIRE CONTROL PANEL, CLEANED AND RESECURED ENGINE FIRE LOOP CONNECTORS PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 1006, LBL 15.  REPAIRED PER SWA RA 1-253-1411.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 1016, LBL 15 AND 10.  REPAIRED PER SWA RA 1-253-1409.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND 7 CRACKS IN SEAT TRACK WEB EXTENDING FROM RIVET HEADS THAT SECURE WEB TO PRESS DECKATTACHING ANGLES BETWEEN BS 706/715 AT RBL 24.75.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME CHORD ANGLE CRACKED AT BELT FRAME AFT OF FWD ENTRY DOOR AT BS 348 FROM S14 TO17L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED BC1 CHECK, FOUND FLOOR BEAM SUPPORT STRAPS CRACKED AT BS 312, AT BL ZERO, RBL 46, AND RBL 28.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND NOSE GEAR WHEELWELL ACCESS PANEL OPENING CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
NLG RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  REPLACED LANDING GEAR CONTROL MODULE PER BOEING M/M.


REMARKS:
EXPERIENCED BIRDSTRIKE TO FIRST OFFICER'S NR 1 WINDOW.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRDSTRIKE INSPECTION.  ALSO, FOUND NR 4 WINDOW CHIPPED.  REPLACED NRS 1 AND 4 WINDOW ASSEMBLIES PER BOEING M/M.


REMARKS:
STL - FLT 176 - DURING CRUISE, EXPERIENCED SMOKE IN CABIN AND COCKPIT.  TURNED OFF RIGHT SUPPLY HIGH PRESSURE BLEED AIR, SMOKE DISSIPATED.  FOUND WATER SEPARATOR COALESCERS OIL CONTAMINATED, MFG PN 179460-8-1.  REPLACED WATER SEPARATOR COALESCERS AND AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL.


REMARKS:
DURING CLIMB, LOST CABIN PRESSURE AT 17,000 FEET, FLIGHT RETURNED.  FOUND INSULATION BLANKET UNDER LEFT OUTFLOW VALVE.REMOVED INSULATION BLANKET AND REMOVED AND REPLACED LEFT OUTFLOW VALVE, MFG P/N 103280-5-1.  ALSO, REMOVED AND REPLACEDRIGHT OUTFLOW VALVE, MFG P/N 103280-5-1, AUTOMATIC CABIN PRESSURE CONTROL, MFG P/N 102518-3-1 AND MANUAL PRESSURE CONTROLLER, MFG P/N 131046-1.  PERFORMED CABIN PRESSURE LEAK CHECK, CHECKED NORMAL.


REMARKS:
MCO - FLT NR 378 - NR 2 ENGINE OVERTEMPED ON TAKEOFF TO 944 DEGREES FOR 2 SECONDS.  FLIGHT CREW REDUCED POWER AFTER TAKEOFF TO BELOW RED LINE.  CREW COULD NOT SELECT NORMAL CLIMB N1 WITHOUT EGT EXCEEDANCE.  RETURNED TO MCO AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND VLV GEAR MOTOR FAILURE.  REPLACED VLV MOTOR AND MASTER BALLSCREW ACTUATOR.  ENGINE OPS CHECKED NORMAL. (M)


REMARKS:
CLT - DURING A CMV 1 INSPECTION, VISUALLY FOUND 6 INCH BY 5 INCH AREAS PITTED CORROSION AFT FLANGE OF FLOOR BEAM 1640.REPLACED T-CAP.  (M)


REMARKS:
JFK - DURING C-CHECK, FOUND A 3.5 INCH CRACK IN AFT PRESSURE BULKHEAD TOP LEFT GORE PANEL.  REPAIRED PER LOCKHEED SERVICE BULLETIN 93-53-258, PAGES 15 AND 16, FIGURE 4.


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1.50 INCH CORRODED AREA, BS 967, RBL 45 ON FLOOR BEAM.  INSTALLED NEW T-CAP AND REPAIR ANGLES, REPAIRED PER TR 53-10-05 C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION ACCOMPLISHED SID PSE 53.09.031A AND FOUND A 1 INCH SKIN CRACK TOP AFT DOOR STOP ADJUST HOLE.  VISUAL VERIFIED BY NDT.  CUT OUT CRACKED AREA INSTALLED FILLER AND .071 INCH AND .100 INCH DOUBLER REPAIR PER USAIR EA 31604 AND SRM 53-05 FIG 26A.  (M)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 25, WL 207.5.  INSTALLED FLOOR BEAM REPAIR, WEIGHT .8 POUNDS, AT BS 520, REPAIRED PER SB 737-53-1120 EA 40385.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STA 1060 BETWEEN LONGERON 29R AND LONGERON 30R SKIN CLIP.  CORROSION TASK NR C57-53300.  SPLICED IN SECTION OF SKIN CLIP PER SRM 53-03, FIGURE 3.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND .020 INCH CRACK IN LIGHTNING STRIKE AREA OF FUSELAGE EXTERIOR SKIN AT STA 380, LONGERON 6L AND LONGERON 7L.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 53-30-11.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND CRACK APPROXIMATELY 1 INCH LONG IN SECOND LAYER OF SKIN IN UPPER FORWARD CORNER OFM.E.D. IN FUSELAGE SKIN (X-RAY INSPECTION) SSI 53-11-015.  CUT OUT CRACK AND INSTALLED FILLER AND DOUBLERS PER SRM 53-05, FIGURE 25A.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND .50 INCH BY 9 INCH AREA OF LEVEL 1 CORROSION RESULT FROM UNIQUE EVENT, BROKEN WATER LINE.  CORROSION TASK NR C57-53300.  LONGERON 28L FROM STA 1315 - STA 1332.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14 AND USAIR EA NR 31600.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND 4.75 INCH CRACK JUST OUTBOARD OF NR 7 SLAT TRACK CUT-OUT LEADING EDGE SKIN.  INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 57-06A, FIGURE 1, AND USAIR EA NR 31672.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LT AND RT FLOOR SUPPORT RAILS, STA 218 - STA 541, FORWARD CARGO, CORROSION TASK NR C51-5330.  INSTALLED SPLICE REPAIR PER USAIR TYPICAL REPAIR 53-20-09A.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LONGERON 28L SPLICE AT STA 228.  CORROSION TASK NR C51-53300.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14.  (X)


REMARKS:
PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, STA 180 - STA 200, RT SIDE BELOW FORWARD SERVICE DOOR IN FITTINGS AND CUSP ANGLE.  CORROSION TASK NR C46-53305.  SPLICED IN NEW SECTION OF CUSP AND FITTINGS PER SRM 53-03-5, CONF. J060288-1.  (X)


REMARKS:
PIT - DURNG Q1/C6 INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA PREVIOUSLY REWORKED BELT FRAME, STA 1250, BETWEEN LONGERON 28R AND LONGERON 29R.  CORROSION TASK REF C57-53300, LEVEL 1.  REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PERSRM 53-14, FIGURE 5.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.50 INCH CRACK IN RT CUSP MEMBRANE BETWEEN STA 905 AND STA 927, RT SIDE.  MFGNEW MEMBRANE AND SPLICED PER SRM 53-05, FIGURE 97.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN LONGERON AT STA 313, LONGERON 16L.  REMOVED DAMAGED AREA ANDINSTALLED SPLICE REPAIR PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
PIT - DURING C-3 INSPECTION, FOUND LEVEL 1 CORROSION ON BELT FRAME APPROXIMATELY 12 INCHES LONG AT STA 965 FROM LONGERON 29L TO LONGERON 29R (NOT A CORROSION TASK AREA).  REMOVED CORRODED AREA AND INSTALLED ROLLER Z-FRAME SPLICE REPAIR PERSRM 53-03, FIGURE 2A.  (X)


REMARKS:
PIT - DURING C-3 CHECK INSPECTION, FOUND 2 INCH AREA OF CORROSION ON PRESSURE PANEL AT STA 110 RT, 12 INCHES RT OF AIRCRAFT CENTERLINE.  INSTALLED DOUBLER REPAIR PER SRM 53-01, FIGURE 2.  (X)


REMARKS:
PIT - DURING C-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK TOP DRAG ANGLE OF PYLON AT STA 980.  INSTALLED DOUBLER REPAIR PER SRM 53-04, FIGURE 10, AND USAIR EA NR 31737.  (X)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND A 2 INCH SKIN CRACK AT BS 727, STR 17L.  INSTALLED DOUBLER PER SRM 53-30-3.  (X)


REMARKS:
ROA - DURING 'TRANSIT CHECK' VISUAL INSPECTION, FOUND .75 INCH CRACK, RT NR 2 WINDOW CONNECTION ANGLE.  INSTALLED REPAIR PATCH, REPAIRED PER EA 31753.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 45 INCHES, STA 328, BL ZERO TO RBL 45 INCHES.  CUT OFF T-CAP FROM LBL 28 TO RBL 45, FABRICATED NEW T-CAP AND SPLICES AND INSTALLED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 294 TO STA 312, RBL 12 INCHES ON INTERCOSTAL.  REPLACED INTERCOSTAL, REPAIRED PER 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 312 TO STA 328, RBL 12 INCHES, ON INTERCOSTAL.  REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORRODED AREAS AROUND NUTPLATE HOLES, .50 INCH BY .50 INCH, FLOOR BEAM BS 947.6, LBL 24 TO RBL 6 (6 PLACES).  INSTALLED NEW T-CAP SECTION, RBL 37 INCHES TO LBL 60 INCHES, REPAIRED PER TR 53-10-05C, WEIGHT ADDED 3.6 POUNDS AT BS 947.5.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORRODED AREA ROUND NUTPLATE HOLES, .50 INCH BY .50 INCH, FLOOR BEAM BS 947.6, RBL 34 TO RBL 52, AND LBL 35 TO LBL 41.  INSTALLED T-CAP REPAIR ANGLES.  REPAIRED PER TR 53-10-05.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH, STA 927 TO STA 947, RBL 7, ON INTERCOSTAL.  REPLACED INTECOSTAL PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH, STA 957, RBL 18 - RBL 45, ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH BY .25 INCH HOLE GOUGED IN OUTBOARD J-SECTION OF STRINGER, STA1050, STR 27L.  FORMED AND INSTALLED DOUBLER FOR J-LEG OF STRINGER, REPAIRED PER SRM 53-10-3, FIGURE 1.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORROSION, STA 907  - STR 26L, ON STRINGER SPLICE.  REPLACED SPLICE, REPAIRED PER SRM 51-10-1.  REPLACED SPLICE, REPAIRED PER SRM 51-10-1.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1.5 INCH LONG CRACK IN UPPER COMPRESSION CHORD, BS 727 - RLB 24.  INSTALLED ANGLE REPAIR, REPAIRED PER EA NR 40453.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND WORN AREAS AT SCREW HOLES, BS 719 TO BS 727, RIGHT WHEELWELL ON KEEL BEAM.  INSTALLED STRAP, REPAIR PER EA 40457.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, RLB 25 LONGITUDINAL FLOOR BEAM LOWER WEB, STA 707, WL203.  INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 AND DWG 65C34537.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORRODED AREA BETWEEN BS 967 AND BS 947 AT RBL 7 INCHES ON INTERCOSTAL.  REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1.  CORROSION TASK NRC53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA, BS 984, LBL 19, ON INTERCOSTAL.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SPOT OF CORROSION ON SEAT TRACK, .75 INCH BY 6 INCHES, LBL 24, BS 943.  INSTALLED NEW TRACK SECTION.  REPAIRED PER SRM 53-10-5.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 2 INCHES BY 4 INCHES, STA 344, BL ZERO TO LBL 8 INCHES, ONFLOOR BEAM.  CUT OUT FLOOR BEAM SECTION, FABRICATED NEW T-CAP, AND REPAIRED DOUBLERS AND INSTALLED PER TR 53-10-13.  CORROSION TASK NR C53-107-01.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH BY 3 INCHES, STA 312 TO STA 328, LBL 12 INCHES, ON INTERCOSTAL.  REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-01.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION 1.50 INCHES BY 1 INCH, STA 947 TO STA 967, RBL 45 ON INTERCOSTAL.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 1 INCH, STA 986.5 TO 1006 BL ZERO ON INTERCOSTAL.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH BY .50 INCH CORRODED AREA FLOOR BEAM BS 1016, LBL 15.  REMOVED CORROSION AND INSTALLED REPAIR STRAP, REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES, STA 312 RBL 35 INCHES ON FLOOR BEAM.REPLACED T-CAP FROM LBL 6 TO RBL 36, REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 328 TO 340, LBL 12 INCHES ON INTERCOSTAL.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-10.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3.50 INCH BY 1 INCH AND 2 INCHES BY 1 INCH, BS 990 AND BS 1015 AT RBL8 INCHES ON SEAT TRACK.  REPLACED TRACK, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH SLOT IN BEAR STRAP - DOUBLER PREVIOUSLY INSTALLED, BUT NOT PER SRM BS 794 AT S23R.  REMOVED PREVIOUSLY INSTALLED DOUBLER AND INSTALLED REPAIR PER EA.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK IN OUTER SKIN AT UPPER HINGE CUT-OUT AT ENTRY DOOR.  INSTALLED EXTERIOR SKIN REPAIR.  REPAIRED PER EA 40360.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, LBL 24.5, STA 675, IN FLOOR BEAM.  CRACK CONTAINED BY FASTENER HOLE AND CUT-OUT INSTALL REPAIR CHANNEL, DOUBLERS, AND RADIUS FILLER AS REQUIRED BY EO 5791G632 AND EA 40396.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, RBL 24.5, STA 675, IN FLOOR BEAM.  CRACK CONTAINED AT AILERON QUADRANT CUT-OUT.  INSTALLED REPAIR CHANNEL AMD DOUBLERS, AND RADIUS FILLERS AS REQUIRED PER CO 5791G632 AND EA 40396.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 45, WL 207.5.  INSTALLED FLOOR BEAM REPAIR, REPAIRED PER SB 737-53-1120, EA 40385, .8 POUNDS AT BS 520. (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, LT FRAME INBOARD CHORD, FIRST FASTENER ABOVECENTER WING SKIN.  INSTALLED FILLER AND ANGLE, WEIGHT CHANGE LESS THAN 1 POUND.  REPAIRED PER EA 40391.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, RIGHT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN.  INSTALLED FILLER ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER EA 40391.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, STA 639, STUB BEAM ATTACH ANGLE, RBL 45, WL 207.  REPLACED ATTACH ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1.50 INCH CRACK, BS 727, RBL 24.5 ON ANGLE.  INSTALLED REPAIR ANGLE, REPAIRED PER EA 40453.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND DEEP GOUGE .25 INCH BY 2 INCHES IN UPPER INBOARD LEG OF S26L, BS 1044.  INSTALLED STR REPAIR, LESS THAN 1 POUND ADDED, REPAIRED PER SRM 53-10-3, FIGURE 1.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK IN UPPER RADIUS OF BEAM CAP, STA 520, FLOOR BEAM RBL 25.  INSTALLED FLOOR BEAM REPAIR, .8 POUNDS AT BS 520, REPAIRED PER SB 737-53-1120, EA 40385.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION (PREVIOUS REPAIR NOT PER SRM), FOUND UNKNOWN DAMAGED DOUBLER, 8 INCHES BY 9.50 INCHES, BS 227 TO BS 235, S19R TO S20R.  INSTALLED DOUBLER PER SRM, REPAIRED PER SRM 53-30-3.  (X)


REMARKS:
INT - DURING Q-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .25 INCH LONG SKIN CRACK ON VISUAL INSPECTION AND .625INCH LONG GUSSET CRACK LEFT C-D WINDOW POST SKIN AND GUSSET BS APPROX 219.8 BY EDDY CURRENT.  REMOVED DAMAGED AREA AND INSTALLED FILLERS AND DOUBLERS.  REPAIRED PER EA 40239.  REFERENCE USAA951217.


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION IN SUPPORT BEAM WEB AT STATION 1338 OUTBOARD END OF FLOOR BEAM UNDER AFT RIGHT LAV, PREVIOUSLY REWORKED CORROSION TASK NR C58-5330.  SPLICED IN DOUBLER FILLER AND WEB SECTION PER USAIR EA 31376A.  (M)


REMARKS:
PIT - DURING Q-3/C-6 INSPECTION, FOUND LEVEL 1 CORROSION LEFT OUTBOARD SEAT TRACK AT STATION 1174 PREVIOUSLY REWORKED CORROSION TASK NR 05853302.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG F.  (M)


REMARKS:
PIT - DURING Q-3/C-6 INSPECTION, FOUND LEVEL 1 CORROSION AROUND FLOOR BEAM NUT PLATE HOLES TOP AND BOTTOM SURFACE AT STATION 1338 AFT RT LAV PREVIOUSLY REWORKED.  CORROSION TASK REF C53-53300.  REPLACED TOP CAP OF FLOOR BEAM PER USAIR TYPICAL REPAIR 53-10-14.  (M)


REMARKS:
PIT - DURING Q-3/C-6 INSPECTION, FOUND CLASS 3 REPAIR INSTALLED PER OM-7 NR 69263 (DEFERRED MAINTENANCE).  REPLACED REPAIR AT SKIN STATION 228 TO 256 BETWEEN LONGERON 14L AND 17L PER USAIR TYPICAL REPAIR NR 53-30-12 AND SRM 53-04 FIG 4.  (M)


REMARKS:
INT - DURING Q-5 CHECK NDT INSPECTION, FOUND ONE .25 INCH CRACK, STATION 520, FLOOR BEAM UPPER RADIUS LBL 45, WL 207.75.  DOUBLER INSTALLED PER EA 40020, REF SB 737-53-1120.  REPAIRED PER EA 40020 REF SB 737-53-1120.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 520 FLOOR BEAM UPPER RADIUS RBL 45, WL 207.75.  STOP DRILLED AND INSTALLED DOUBLER REPAIR/MODIFICATION.  REPAIRED PER EA 40020.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORRODED AREA ON FLOOR BEAM AT BS 328.  REMOVED CORRODED AREA, INSTALLED REPAIR PARTS COMPLETED REPAIR.  REPAIRED PER SRM 53-10-51, FIG 205.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 36 INCH AREA CORRODED, FORWARD ENTRY DOOR Z-ANGLE.  REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSIONLEVEL 2.  (M)


REMARKS:
INT - DURING A-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH DIAMETER AREA, STATION 328 FLOOR BEAM UPPER FLANGE AT NUT PLATE HOLES.  SECTION CUT OUT AND REPLACED PER SRM 53-10-51 FIG 205.  REPAIRED PER SRM 53-10-51, FIG 205.  CORROSIONTASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 68 INCH CORRODED AREA ON FLOOR BEAM BS 344 LBL 51 TO RBL 17. INSTALLED T-CAP AND REPAIRED ANGLE.  REPAIRED PER SRM TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH DIAMETER AREA, INTERCOSTAL UPPER FLANGE STATION 328 TO344 LBL 12, WL 208.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.(M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 16 INCH CORRODED AREA ON SEAT TRACK AT BS 344 TO BS 360 LBL 25 INCHES.  REMOVED AND REINSTALLED REPAIR PART COMPLETED REPAIR.  REPAIRED PER SRM 53-00-52, FIG 202.  CORROSION TASK NRC53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH AREA, BS 328 TO BS 312, RBL 12 INCHES.  REMOVED AND REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA BS 294 TO BS 312, RBL 12 INCHES.  REMOVED AND REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 312 TO BS 328, LBL 12 INCHES.  REMOVED AND REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA RBL 14 CARGO FLOOR SUPPORT STRINGER (BEAM) AT BS 747.  CUT OUT CORRODED SECTION OF BEAM BS 733-778.  FABRICATED AND INSTALLED NEW SECTION OF BEAM (TRACK) AND SPLICES.  REPAIRED PER SRM 53-00-53 FIG 202 AND BOEING DRAWING 65-47957.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 46 INCH CORRODED AREA BS 280-326, STRINGER 17 RT (RT SERVICE DOORWAY CHORD ANGLE).  REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE WITH SAME P/N FROM STOCK.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, ON Z ANGLEBS 947-BS 1006, RBL 53.  REPLACED Z-ANGLE.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 10 INCH AREA CORRODED ON SUPPORT AT STATION 947 TO 967AT LBL 25.  REMOVED AND REPLACED CHANNEL.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH AREA CORRODED, ON SUPPORT AT 967 AT LBL 51.  REMOVED AND REPLACED SUPPORT CHANNEL.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORROSION ON SUPPORT AT STATION 947 TO 967 RBL 51.  REPLACED SUPPORT CHANNEL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND CORRODED SKIN PAST LIMITS OF EO NR 5492R274 PART IV STEPS 2 AND 3 LOCATED AT NR 2 ENGINE PYLON INBOARD.  REPAIRED SKIN PER DRAWING 012N8774 AND EA 40036.  (M0


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON BELTFRAME STATION 1322 LOWER FWD SURFACE LONGERON 30. CORROSION TASK NR C57-53300 PREVIOUSLY RE WORKED.  SPLICED IN NEW SECTION BELTFRAME PER SRM 53-03 FIG 2A.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 446 NEAR ALT STATIC PORT.  PREVIOUSLY RE WORKED FROM LAV SPILL.  CORROSION  TASK NR C51-53300.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-10-2.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION STATION 227 LONGERON 29R AT RIVET HEADS PREVIOUSLY RE WORKED CORROSION TASK NR C51-53300.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SKIN CRACK APPROXIMATELY 2 INCHES IN LENGTH IN MED UPPER FORWARD JAMB CORNER STATION 160 FUSELAGE EXTERIOR SKIN.  INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-05 FIG 25A.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION LOWER FORWARD CARGO DOOR PAN ASSY PREVIOUSLY RE WORKED.CORROSION TASK NR C51-53300.  INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 14.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION STATION 210 FORWARD END OF RIGHT SEAT TRACK.  CORROSION TASK C46-53305 PREVIOUSLY REWORKED.  SPLICED IN SEAT TRACK PER SRM 53-05 FIG 4.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 1322 FLOOR BEAM RIGHT SIDE LAV AREA.  CUT OUTDAMAGED AREAS INSTALLED FILLERS AND REPAIR ANGLES PER USAIR TYPICAL REPAIR 53-10-19.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT INBOARD SEAT TRACK LEFT STATION 1309 IN 2 POSITIONS.CORROSION TASK NR C58-53301 PREVIOUSLY RE WORKED.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND CORROSION LEVEL 1 AT STATION 1338 UNDER RIGHT LAV AROUND FLOOR SUPPORT BEAM SCREW HOLES.  PREVIOUSLY REWORKED CORROSION TASK NR C58-53309.  SPLICED IN NEW SECTION OF FLOOR SUPPORT BEAM PER USAIRTYPICAL REPAIR 53-10-14.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 1322 AROUND SCREW HOLES RIGHT OF CENTER LINE UNDER AFT LAV FLOOR SUPPORT BEAM.  CORROSION TASK NR C58-53300.  REMOVED CORROSION AND INSTALLED STRAP AND ANGLE INSTALLATION REPAIR PER USAIR TYPICAL REPAIR 53-10-19.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT LONGERON STATION 456.  CORROSION TASK NR C51-53300.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-10-2A.  (M)


REMARKS:
PIT - DURING Q-1/C-6 INSPECTION, FOUND .25 INCH CRACK RIGHT SIDE CABIN STATION 984 AND 1003 AT LONGERON 18 CUSP LINE MEMBRANE.  MANUFACTURED CUSP MEMBRANE AND INSTALLED PER SRM 53-05 FIG 97.  (M)


REMARKS:
PIT - DURING Q-1/C-6 INSPECTION, FOUND 1 INCH CRACK IN FRAME TO FUSELAGE CLIP AFT SIDE OF BS 1437 AT LONGERON 1.  SPLICED IN NEW CLIP PER SRM 53-03 FIG 6.  (M)


REMARKS:
PIT - DURING Q-1/C-6 INSPECTION, FOUND 1.09375 INCH CRACK AT STATION 821 AND LONGERON 17R IN EXTERIOR SKIN.  CUTOUT DAMAGED AREA AND INSTALLED FILLER AND 6.5 INCH BY 8.5 INCH INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW H.  (M)


REMARKS:
PIT - DURING Q-1/C-6 INSPECTION, FOUND .5 INCH CRACK AT CANTED FRAME 1485 AT LONGERON 7L.  STOPPED DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-14-4 FIG 3.  (M)


REMARKS:
ROA - DURING 'BX' CHECK VISUAL INSPECTION, FOUND 18.5 INCHES BY 2 INCHES CORROSION (STRINGER IS CORRODED), BS 967 STRINGER 27 LEFT.  REMOVED DAMAGE AND INSTALLED STRINGER SPLICE.  REPAIRED PER SRM 53-10-3, FIG 1.  (M)


REMARKS:
PIT - DURING C-2 CHECK INSPECTION, FOUND .5 INCH CRACK IN LONGERON 6R AT STATION 617 SID INSPECTION REF PSE 53.09.009 AND 010 LFEC INSPECTION.  INSTALLED LONGERON SPLICE AND DOUBLERS PER SRM 53-10-17.  (M)


REMARKS:
PIT - DURING C-2 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 756 AT LONGERON 4L.  SID INSPECTION REF PSE 53.09.009 AND .010 LFEC INSPECTION.  INSTALLED LONGERON SPLICE AND DOUBLERS PER USAIR SRM 53-10-17.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .25 INCH LONG SKIN CRACK ON VISUAL INSPECTION AND .625INCH LONG GUSSET CRACK LEFT C-D WINDOW POST SKIN AND GUSSET BS APPROX 219.8 BY EDDY CURRENT.  REMOVED DAMAGED AREA AND INSTALLED FILLERS AND DOUBLERS.  REPAIRED PER EEA 40239.  (M)


REMARKS:
INT - DRUING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETER .020 DEEP CORROSION INTERCOSTAL BETWEEN STATION 328 AND STA 344 LBL 8.5.  REPLACED WITH INDENTICAL PART NR 65-45834-259.  LEVEL 1 CORROSION, CORROSION TASK NR C53-107-02.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AROUND NUT PLATE HOLES ON INTERCOSTAL BETWEEN STATION 967.5 TO STATION 947 AT LBL 42.  LEVEL 1 CORROSION.  REPLACED WITH NEW INTERCOSTAL FROM STOCK.  REPAIRED PER SRM 51-10-2 AND BAC DRAWING 65-46812-170.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORROSION 8 PLACES, STATION 328 TO 344 AND STATION 344 TO 360 RBL 12.  REPLACED INTERCOSTALS.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.(M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 45 INCHES STATION 312, LBL 16 TO RBL 36.  REPLACED UPPER T-CAP.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 10 INCH AREA OF FUSELAGE SKIN CHAFFED, FORWARD END OF DORSALFIN CONTACT AREA.  INSTALLED EXT FUSELAGE SKIN DOUBLER.  REPAIRED PER SRM 53-00-01, FIG 202.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND DENT 3.5 INCHES BY 4.75 INCHES, STATION 344 AT STRINGER 19R.  INSTALLEDDOUBLER.  REPAIRED PER SRM 53-00-01.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOOR INTERCOSTAL BS 328 TO 312 RBL 12.  LEVEL 1 CORROSION.  INSTALLED NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 50 INCH CORROSION AREA AT NUT PLATE HOLES, BS 328 FLOOR BEAM CAP LBL 34 TO RBL 65.  INSTALLED NEW T-CAP SECTION.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 28 INCH CORROSION AT STATION 967 LBL 28 INCHES TO LBL 50 INCHES.  REPLACED T-CAP OF FLOOR BEAM.  REPAIRED PER SRM 53-00-51.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 5 INCHES OF CORROSION BS 335, RBBL 51.  REPLACED SEAT TRACK.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 6 INCHES OF CORROSION BS 348-360.  REPLACED SEAT TRACK.  REPAIRED PER SRM 53-00-52.  (M)


REMARKS:
INT - DURING Q-CHECK VISUAL INSPECTION, FOUND 1 INCH BY 48 INCH CORROSION STATION 986 RBL 4 INCHES TO LBL 52 INCHES.  REPLACED UPPER T-CAP.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORROSION LBL 18 INCHES STATION 967 TO STATION 986.  REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-4.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION STATION 1006 TO STATION 1016 LBL 16 INCHES.REPLACED WITH LIKE PART.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 8 INCH SCREW HOLES TO CLOSE TO EDGE, STATION 907 RBL 24 TO LBL 45.  INSTALLED NEW T-CAP SECTION.  REPAIRED PER TR 53-10-05 AND SRM 53-60-51.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STATION 1016 LBL 6 INCHES TO RBL 6 INCHES.INSTALLED REPAIR DOUBLER.  REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
PHL - FLT 2184 - DURING RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON.  THE CAPTAIN CYCLED THE GEAR, BUT THE LIGHTDID NOT GO OUT.  THE CAPTAIN DECIDED TO RETURN TO PHL.  REMOVED AND REPLACED THE LEAKING SCHRADER VALVE.  (M)


REMARKS:
PIT - FLT NR 1133 - EN ROUTE PIT TO IAH, LEFT FORWARD AND RIGHT AFT FUEL BOOST PUMP CIRCUIT BREAKERS TRIPPED AND WOULD NOT RESET.  FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND FUEL SCAVENGE SOLENOID VALVE INOP.  RELEASED WITH FUEL SCAVENGE SYSTEM ON MEL 28-17 FOR SOLENOID VALVE REPLACEMENT.  (M0


REMARKS:
IND - FLIGHT NR 0133 - RIGHT ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND B-SYSTEM HYDRAULIC QUANTITY DROPPED TOONE QUARTER.  FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND SERVICED HYDRAULICS.  OPS/LEAK CHECKED GOOD.  (M)


REMARKS:
PIT - FLIGHT NR 0009 - AIRCRAFT DISPATCHED WITH MEL 26-2A FOR NR 2 ENGINE B-LOOP.  ON CLIMB-OUT FROM PIT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED.  FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO PIT.  LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED THE P8-1 FIRE CONTROL PANEL AND PERFORMED ENGINE RUN UP.  OPS CHECKED GOOD.  (M)


REMARKS:
STL - FLT 202 - A CHECK OF THE EGRESS LIGHTS REVEALED ROW 15 TO ROW 19 INOPERATIVE.  REMOVED AND REPLACED FEEDER LINE FLEX CABLE, MFG PN 5853-1.  OPERATIONAL CHECK OF THE EGRESS LIGHT SYSTEM WAS NORMAL.  CHECK C-2D - 10-17-95 - MCI.


REMARKS:
SFO - UPON TEST, THE L4 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE.  MAINTENANCE REPLACED THE LIGHT ASSEMBLY.  (X)


REMARKS:
CABIN O2 MASKS DEPLOYED DURING CLIMBOUT.  AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING.  REPACKED MASKS, REPLACED O2 GENERATORS, AND PRESSURIZATION CHECKED AIRCRAFT PER BOEING M/M.


REMARKS:
DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM STRAP CRACKED JUST O/B AND ABOVE BATTERY.  REPAIRED PER BOEING SRM.


REMARKS:
DURING DESCENT, NUMBER 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT DAL.  INSPECTED, NO CONTAMINATION NOTED.  REPLACED BYPASS SWITCH, LEAK CHECKED AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
EN ROUTE FROM TUS TO SAN, FIRST OFFICER'S WINDSHIELD BEGAN ARCING, THEN CRACKED.  AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED WINDOW ASSEMBLY AND HEAT CONTROLLER PER BOEING M/M.


REMARKS:
NOTED A-SYSTEM FLUID LOSS EN ROUTE.  AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING.  INSPECTED TAIL AREA AND PERFORMED LEAK CHECK.  REPLACED ELEVATOR FEEL ACTUATOR PER PER BOEING M/M.  TEST FLOWN WITH NO DEFECTS NOTED.


REMARKS:
FLT 72 - AT 1.5 EPR, TAKEOFF ROLL AUTO PRESSURE GREEN LIGHT ILLUMINATED.  APPROXIMATELY SEVERAL SECONDS LATER, BOTH PACKS TRIPPED OFF, TEMPS AND PRESSURE NORMAL.  DID NOT RETARD THROTTLES UNTIL ABORT WAS INITATED.  RAN AIRCRAFT AT HIGH POWER, SYSTEM CHECKS NORMAL IAW MM 21-11-00, PAGES 501-503.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2.50 INCH DIAMETER SPOT OF CORROSION, BS 957, LBL 50, ON INTERCOSTAL. REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1.50 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, RBL 16, BS 967 TO BS 987, ON INTERCOSTAL.  REMOVED AND REPLACED WITH NEW PART. CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 6 INCH CRACK FORWARD SERVICE DOOR LOWER GATE.  REPLACED HINGE ASSEMBLY.  REPAIRED PER EA 40346.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND STA 520 FLOOR BEAM NEEDS TO BE MODIFIED AT BL ZERO PER SB 737-53-1120DUE TO CRACKS AT LBL 45, RLB 25, RBL 45 AND LBL 25.  MODIFIED CHANNEL PLUS LINK INSTALLED PER REF EA 40383 SB 737-53-1120.  NOTE:  NO REPAIR MADE.  MODIFIED CHANNEL PLUS LINK INSTALLED ONLY.  REPAIRED PER SB 737-53-1120, EA 40383.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH DIAMETER SPOT OF CORROSION AND 3.50 INCH BY 18 INCH AREA OF CORROSION, BS 936 AND BS 957 ON DOOR Z-ANGLE.  REMOVED CORRODED Z-ANGLE AND INSTALLED NEW Z-ANGLE FROM STOCK, PN 65-45855-101.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL .50 INCH BY 1 INCH CORRODED AREAS, BS 727F TO BS 787, RBL 14,CARGO FLOOR TRACK.  CUT OUT CORRODED TRACK (BEAM) FROM BS 727E PLUS 14 TO BS 807. FABRICATED AND INSTALLED NEW BEAM SECTION AND SPLICES.  REPAIRED PER SRM 53-00-53, FIGURES 202 AND 203, TR 53-10-06.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (X)


REMARKS:
ON FLT NR 248 - ATL- AIRCRAFT RETURN, AFTER DEPARTURE THE LEFT FUEL HEAT CAME ON AND STAYED ON, DID NOT EXCEED OIL TEMPLIMITS.  REMOVE AND REPLACE FUEL HEAT VALVE ON LEFT ENGINE PER MM 73-11-2, OPS CHECK NORMAL.  (M)


REMARKS:
ON FLT 530 - ATL - AIRCRAFT EXPERIENCED A VIBRATION ON THE LEFT SIDE OF THE AIRCRAFT BY THE COCKPIT.  AIRCRAFT RETURNED.  CHECKED AROUND THE NOSE GEAR AREA AND FOUND THE EXTERNAL POWER DOOR PANEL LEFT OPEN AND CLOSED DOOR.


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND THREE 1 TO 2 INCH CRACKS, BL 0 BS 500G TO BS 520, ON INTERCOSTAL.  REMOVED, FABRICATED AND INSTALLED NEW UPPER CHORD ANGLE.  REPAIRED PER DRAWING 65C34688.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCH FORWARD ENTRY DOOR TRANSITION ANGLE.  INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 6 INCH BY 1 INCH S-27 L, BS 1004 TO BS 1010 ON STRINGER.SPLICED IN NEW STRINGER SECTION WEIGHT CHANGE LESS THAN 1 LB.  REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-208-01,CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 5 INCH BY 1 INCH S-25 L BS 968 ON STRINGER.  INSTALLED DOUBLER WEIGHT CHANGE LESS THAN 1 LB.  REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 12 INCH BY 1 INCH AT S-26 R, BS 974 TO BS 986 ON STRINGER.  SPLICED NEW STRINGER SECTION IN, REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AROUND NUTPLATE HOLES .25 INCH BY .25 INCH, BS 967 LBL 4,RBL 5, RBL 18 RBL 26, RBL 47, ON FLOOR BEAM.  INSTALLED TEE SECTION ANGLES AND STRAPS.  REPAIRED PER TR 53-10-05 C.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH GOUGE IN STRINGER OUTBOARD 'J' SECTION, STATION 1044 STRINGER 27L.  INSTALLED REPAIR DOUBLER UNDER 'J' LEG OF STRINGER, AFTER SMOOTHING GOUGE.  REPAIRED PER SRM 53-10-3 FIG 1.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT AFT END OF HINGE, FRONT CABIN SERVICE DOOR LOWER GATE HINGE.  REPLACED HINGE, REPAIR PER EA 40350.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STRINGER 16 L, BETWEEN STATION 500B AND STATION 520, ON STRINGER.  INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK S-16R, BETWEEN STATION 500B AND 520, ON STRINGER.  INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK RIGHT WING TO BODY SUPPORT ANGLE BS 540-522.  REPLACED ANGLE, LESS THAN 1 LB WEIGHT CHANGE, REPAIR PER EA 25375 AND SRM 51-40-3.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, BL 0 LONGITUDINAL FLOOR BEAM SUPPORT FITTING FORWARD RADIUS, STATION 727, WL 202.5.  INSTALLED REINFORCING ANGLES, RADIUS FILLERS, SHIMS AND SEALED.  REPAIRED PER EO 5394G176. (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH GOUGE IN OUTER SKIN OF AFT CARGO DOOR TOP AFT CORNER OF DOOR (6 INCH BY 6 INCH DOUBLER).  INSTALLED EXT SKIN DOUBLER, REPAIRED PER SRM 52-00-3.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BL 0 STATION 708 AND BS 710.  INSTALLED WEB REPAIR, REPAIRED PER DWG 65C34537.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM WEB (LOWER) STATION 707, WL 203.  INSTALLED WEB REPAIR (WT .3 LBS), REPAIRED PER SRM 51-40-2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 3 INCH CORRODED AREA BS 986.5 RBL 24.  REPLACED SEAT TRACK,WT CHANGE LESS THAN 1 LB.  REPAIRED PER SRM 51-10-1 AND SRM 53-10-5.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2. (M)


REMARKS:
SFO - DURING INSPECTION, FOUND BOTH L4 AND R4 DOOR EXIT IDENTIFIERS INOPERATIVE.  REPLACED BOTH EXIT IDENTIFIERS.  (M)


REMARKS:
BDL - FLT NR 2351 - FLIGHT WAS UNABLE TO PRESSURIZE AFTER TAKEOFF.  RETURNED TO BDL AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPAIRED L1 DOOR SEAL AND TIGHTENED BOLT IN UPPER CAM ASSEMBLY.  PRESSURIZATION AND DOOR SEAL CHECKED NORMAL.  (M)


REMARKS:
PHL - FLT NR 2169 - EN ROUTE LGA TO FLL, PRESSURIZATION FAILED.  FLIGHT DESCENDED TO 10,000 FEET AND DIVERTED TO PHL.  LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED THE PRESSURIZATION CONTROLLER.  BITE AND OPS CHECKED NORMAL.  (M)


REMARKS:
IND - FLT NR 2116 - ON CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE.  FLIGHT CREW REPORTED LEAK AROUND L1 DOOR.  RETURNED TO IND AND LANDED WITHOUT INCIDENT.  MAINTENANCE INSPECTED L1 DOOR AND SEAL.  LUBED ROLLERS.  OK FOR SERVICE.  (M)


REMARKS:
CLT - FLT NR 0127 - DURING CLIMB-OUT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED.  CREW FOLLOWED HANDBOOK PROCEDURES INCLUDING ENGINE SHUTDOWN.  FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE CORE OVERHEAT/FIRE DETECTOR ELEMENT AND REPLACED LEFT AND RIGHT ENGINE FIRE BOTTLES.  (M)


REMARKS:
DURING SCHEDULED MAINTENANCE, FOUND TOP OF FLOOR BEAM CHORD CORRODED AT BS 947, WL 208, RBL 55 TO LBL 55.  REPAIRED PERBOEING SRM.


REMARKS:
AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 2 ENGINE.  AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 2 ENGINE PER PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, UNABLE TO RAISE GEAR HANDLE.  OVERRIDE TRIGGER WAS USED TO RAISE GEAR, CYCLED GEAR NORMALLY.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  REPLACED RELAY R276, CHECKED AIR SAFETY SENSOR, AND OPS CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1121, BETWEEN S12 AND 13L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 875 TO 883, BETWEEN S1 AND 2L, BETWEEN S1 AND 2R, AT BS 258,S21L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1019, BS 340 BETWEEN S17 AND 18L, BS 256 BETWEEN S22 TO 23R AND AT BS 310, S21R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178 BBL 0 WL 185.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD CRACKED 2 PLACES AT BS 178, LBL 5 TO 12 AT WL 201 TO 205, LBL 5.7.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986 WL 208 RBL 5, 24, 32 AND 43.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178 LBL 5 WL 184.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND O/B CHORD CRACKED AT BS 1156 RBL 23 S4R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AND SHEAR TIE AT S15 CRACKED AT BS 360 AND BS 907 S4R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787, S1L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492 RBL 37 WL 161.  REPAIRED PER TRAMCO EWO 95-0789.


REMARKS:
STL - FLT 86 - PRIOR TO LANDING, LT MLG GREEN LIGHT WAS INOPERATIVE RESULTING IN A FLY-BY.  REPLACED LENS, MFG PN 10648LD 2-359.  CHECK C-10A - 11-24-95.


REMARKS:
STL - FLT 116 - DURING TAKEOFF, AN ELECTRICAL SMELL WAS DETECTED IN THE COCKPIT.  TROUBLESHOOTING REVEALED THE AURAL WARNING BOX WAS FAULTY.  REMOVED AND REPLACED AURAL WARNING BOX, MFG PN H05A0035-A.  OPERATIONAL CHECK NORMAL.  CHECK C-1D- FEBRUARY 2, 1995 - MCI.


REMARKS:
DURING OP-15, FOUND CORROSION ON GALLEY FLOOR, RT INBOARD SEAT TRACK, UNDER NR 2 GALLEY, STA 234 AND STA 210.  REPLACEDSEAT TRACK SECTION PER SRM 53-05.  AIRCRAFT TOTAL TIME:  64,684 HOURS, 61,704, CYCLES.


REMARKS:
STL - DURING OP-15, FOUND A 1.50 INCH CRACK IN FLOOR BEAM STA 200.  REPAIRED PER ARA 8794.  AIRCRAFT TOTAL TIME:  64,684 HOURS, 61,704 CYCLES.


REMARKS:
STL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 10R, STA 465.  REPAIRED PER SRM 53-11-2, FIGURE 2.  AIRCRAFT TOTAL TIME:  64,684 HOURS, 61,704 CYCLES.


REMARKS:
STL - DURING CHECK C, FOUND A 2.50 INCH CRACK AT LEFT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, FS 1292.  REPAIRED PER SRM 53-05, FIGURE 23.  AIRCRAFT TOTAL TIME:  40,618 HOURS, 36,293 CYCLES.


REMARKS:
STL - DURING CHECK C, FOUND A .3750 INCH CRACK IN RIGHT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, STA 1292.  REPAIRED BY INSTALLLING DOUBLER PER SRM 53-05, FIGURE 23.  AIRCRAFT TOTAL TIME:  40,618 HOURS, 36,293 CYCLES.


REMARKS:
STL - FLT 126 - AFTER TAKEOFF, NR 2 CSD LOW PRESSURE LIGHT CAME ON.  NR 2 CSD DISCONNECTED.  REMOVED AND REPLACED CSD, MFG PN 696233B, OPERATIONAL AND LEAK CHECK OKAY.  ENGINE TOTAL TIME:  34,358 HOURS, 32,155 CYCLES.  CHECK C-12 - 1-11-95- STL.


REMARKS:
STL - FLT 363 - FOLLOWING AN ENGINE CHANGE, DURING TAKEOFF, FLIGHT ATTENDANTS REPORTED A BURNING SMELL AT MID-CABIN.  REMOVED AND REPLACED RIGHT AND LEFT WATER SEPARATORS.  OPERATIONAL CHECK NORMAL.  CHECK C - 12-19-94 - STL.


REMARKS:
STL - FLT 192 - DURING CLIMB, NR 1 ENGINE FUEL HEAT VALVE INTRANSIT LIGHT STAYED ON WITH SWITCH IN THE OFF POSITION.  SHUT DOWN NR 1 ENGINE AND RETURNED FROM FLIGHT.  REMOVED AND REPLACED NR 1 ENGINE FUEL HEAT VALVE, MFG PN 700341-15A.  OPERATIONAL CHECK NORMAL.  OP-17 - 1-8-95 - MCI.


REMARKS:
MCI - DURING CHECK C, FOUND CRACK IN BEARSTRAP, FORWARD GALLEY DOOR CUTOUT AT LOWER AFT CORNER.  REPAIRED PER SSRM 53-30-206, PAGES 201-213, FIGURE 202.  AIRCRAFT TOTAL TIME:  63,044 HOURS, 42,507 CYCLES.


REMARKS:
STL - FLT 159 -  AFTER TAKEOFF, THE RT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE IN THE UP POSITION.  FOUND RT GEAR TARGET ASSEMBLY LOOSE.  SECURED TARGET ASSEMBLY WITH BELT, MFG PN NAS6203-2H.  PERFORMED MM SENSOR CHECK, OPERATIONAL CHECK NORMAL.  CHECK C-2D - 10-17-95 - MCI.


REMARKS:
MCI - DURING CHECK C, FOUND .3750 INCH DENT ON TOP SIDE OF AFT CARGO FORMER RING, FS 1030.  REPAIRED PER SSRM 53-60-202, PAGE 201.  AIRCRAFT TOTAL TIME:  63,044 HOURS, 42,507 CYCLES.


REMARKS:
DURING CHECK C, FOUND CORROSION AT BOTTOM EDGE OF AFT LAV SERVICE COMPARTMENT SKIN, LT SIDE OF FUSELAGE.  INSTALLED DOUBLER REPAIR PER SRM 53-30-3, FIGURE 3-5-3A.  AIRCRAFT TOTAL TIME:  66,911 HOURS, 45,166 CYCLES.


REMARKS:
JFK - DURING CHECK C, FOUND CORROSION IN AFT LAV SERVICE COMPARTMENT PRODUCTION EDGE AFT EDGE, AND DISTRESSED RIVET HEAD LT SIDE OF FUSELAGE.  REMOVED CORROSION AND DAMAGED SKIN AND INSTALLED DOUBLER REPAIRS PER SRM 53-30-03, FIGURE 3-5-3A.  AIRCRAFT TOTAL TIME:  66,911 HOURS, 45,166 CYCLES.


REMARKS:
LAX - FLT 810 - DURING A TEST OF THE EGRESS LIGHTING SYSTEM, THE AFT COACH SECTION DID NOT ILLUMINATE.  REMOVED AND REPLACED ONE EACH FLEX CABLE, MFG PN 5854-1 AND CHECK C-4D - 11-25-95 - LAX.


REMARKS:
JFK - DURING CHECK C, FOUND CRACK IN LOWER EDGE RADIUS, LW RIB STA 738.5, STR 6 AND STR 8, AFT OF ACCESS HOLE.  REPAIRED PER SRM 57-10-05.  AIRCRAFT TOTAL TIME:  66,911 HOURS, 45,166 CYCLES.


REMARKS:
JFK - DURING CHECK C, FOUND CRACK IN RIB AT WS 686.5, LT SIDE.  REPAIRED BY STOP-DRILLING CRACK AND INSTALLED REPAIRED DOUBLER PER SRM 57-10-05, FIGURE 1.  AIRCRAFT TOTAL TIME, 66,911 HOURS, 45,166 CYCLES.


REMARKS:
JFK - DURING CHECK C, FOUND CRACK EXTENDING BEYOND BOLT HOLE ON STR 13R, STA 601.5.  STOP DRILLED AND REPAIRED PER SB 727-57A-159.  AIRCRAFT TOTAL TIME:  66,911 HOURS, 45,166 CYCLES.


REMARKS:
CLT - DURING CMV-2 CHECK INSPECTION, FOUND LIGHTNING STRIKE ON SKIN AT FS 1310 BETWEEN S27L AND S28L.  INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-00-01, FIGURE 203 AND USAIR EA 40270.  (X)


REMARKS:
JFK - FLT 730 - IN CRUISE, L-1 WINDSHIELD OUTER PANE CRACKED RESULTING IN AN UNSCHEDULED LANDING AT ABQ.  REPLACED L-2 WINDSHIELD, MFG PN 5912290505.  CHECK C-1 - 6-27-95.


REMARKS:
STL - FLT 136 - DURING THE COURSE OF AN INSPECTION, IT WAS DISCOVERED THE EGRESS LIGHTING WAS INOPERATIVE.  REPAIRED WIRING HARNESS TO THE EGRESS LIGHTING, OPERATION NORMAL.  CHECK C-2D - 6-29-95 - MCI.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND T-STRIP CRACKED ABOVE FWD UPPER AIRSTAIR DOORWAY STOP IN SEVERAL PLACES.  REPAIRED T-STRIP PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LOWER AFT DOOR STOP.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND WHEEL WELL LOWER FIXED PANEL BELOW KEEL BEAM CRACKED 1 INCH ON RIGHT SIDE ACROSS FROM PREVIOUS REPAIR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT PREVIOUS REPAIR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 772 LBL 12.25 RBL 3, RBL 7.5, RBL 8.25 AND RBL 13.25.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 RBL 4.  REPAIRED PERSWA RA 1-253-1420.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 LBL 10.  REPAIRED PER SWA RA 1-253-1419.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 1006 AFT FLANGE, LBL 15 TO28.  REPAIRED PER SWA RA 1-253-1417.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORROSION AROUND FASTENER HOLE AND MIGRATING UNDER WEB AT BS 1016, FWD FLANGE LBL 0 TO 39.  REPAIRED PER SWA RA 1-253-1415.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND CABIN SEAT TRACK CRACKED AT SCREW HOLE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FWD GALLEY FLOORBEAM CORROSION UPPER TEE CAP FASTENER BS 294 LBL 11.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FWD ENTRY DOOR WEB TO FRAME ATTACH BRACKET CRACKED AT BS 294 S11L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN LAP CORRODED AT BS 910 S27L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO DOOR WEB DAMAGED AT CUTOUT LOWER AFT SIDE.  REPAIRED PER BOEING SRM.


REMARKS:
FLT NR 9 - EWR-MCO - DIVERTED TO ATL AFTER OIL FILTER BYPASS LIGHT FOR NR 2 ENGINE ILLUMINATED IN FLIGHT, OPERATED AT REDUCED POWER.  ALL OTHER INDICATIONS NORMAL.  REPLACED MOS BYPASS SWITCH, OIL PRESS RELIEF VALVE PER MM 79-33-0.  ON HIGH POWER ENG RUN, VIBRATION OCCURRED, FOLLOWED BY FAILURE.  REMOVED AND REPLACED NR 2 ENGINE PER MM 72-00.  OPS CHECK OK. REASON FOR FAILURE OF ENG AWAITING TEAR DOWN REPORT.  (M)


REMARKS:
ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 30 INCH BY 2 INCH CORROSION AT STRINGER 27 LEFT BS 947 TO 977.  REMOVED DAMAGE AND INSTALLED STRINGER SPLICE.  (M)


REMARKS:
PIT - DURING APU MODIFICATION TRACK, FOUND CORROSION ON FLOOR BEAM, BETWEEN STATION 4850 AND 5305 AND BL 0.  CUT OUT CORRODED SECTION OF BEAM AND SPLICED IN NEW 'T' EXTENSION PER SRM 51-70-06.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES IN SEVERAL AREAS, BS 302 TO BS 362 LEFT SIDE, Z-ANGLE.  REMOVED CORRODED Z-ANGLE, REPLACED AND COMPLETED INSTALLATION.  REPAIRED PER SRM 51-10-2, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES, RBL 11 BS 312 TO BS 328, ON INTERCOSTAL.  REPAIRED PER SRM 51-10-2, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 312 TO BS 328, ON INTERCOSTAL.  REPAIRED PER SRM 51-10-2, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1.5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 328 LBL 13 TO RIGHT END OF FLOOR BEAM.  REPLACED T-CAP.  REPAIRED PER TR 53-10-03 SRM 51-70-12 SRM 51-70-11, CORROSION TASK NRC53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 25 INCH BY .5 INCH CORRODED AREA LBL 22 BS 344-369, ON SEAT TRACKS.  FABRICATED SEAT TRACKS AND INSTALLED.  REPAIRED PER SRM 53-00-52, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 947 LBL 4 AND RBL 4, ON FLOOR BEAM.  INSTALLED T-CAP, REPAIR ANGLES AND STRAPS, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 74 INCHES BY .5 INCHES CORRODED AREA BS 344 LBL 55 - RBL 21, ON FLOOR BEAM.  FABRICATED T-CAP AND REPAIR ANGLE AND INSTALLED.  REPAIRED PER TR 53-10-3, CORROSION TASK NR C53-107-02, CORROSIONLEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 30 PERCENT CORRODED 'Z' ANGLE FORWARD GALLEY ENTRANCE, STATION 277 AND STATION 344.  REMOVED AND REPLACED NR ME-32 REQUIRED.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 328 TO BS 344, ON INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 37 INCH CORRODED AREA BS 955 TO BS 992 AT LEFT AFT ENTRY DOOR, Z-ANGLE.  REMOVED CORRODED Z-ANGLE AND INSTALLED NEW Z-ANGLE.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED AREA BS 312, BL 0 (CABIN FLOOR BEAM UPPER FLANGE).  CUTOUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER.  REPAIRED PER SRM 53-10-51 AND FIG 206,CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 987 LBL 45 TO RBL 45 ON FLOOR BEAM.  SPLICED IN T-CAP.  REPAIRED PER EA 40379, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)


REMARKS:
ROA - DURING 'CX-2' CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED STRINGER CAUSED BY LAVATORY SPILL, STRINGER 27L AT BS 947.  REMOVED CORRODED STRINGER SECTION AND SPLICED IN NEW SECTION.  REPAIRED PER SRM 53-10-3 FIG 1.  (M)


REMARKS:
INT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 360-540 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN.  REPLACED UPPER ROW OF RIVETS AT STRINGER 14.  REPAIRED PER EA 3177A.  (M)


REMARKS:
INT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN.  REPLACED UPPER ROW OF RIVETS AT STRINGER 14.  REPAIRED PER EA 3177A.  (M)


REMARKS:
INT - DURING 'TRANSIT CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 RHS, ON FUSELAGE SKIN.  REPLACED UPPER ROW OF RIVETS AT STRINGER 14.  REPAIRED PER EA 3177A.  (M)


REMARKS:
INT - DURING 'DROP IN-AV' VISUAL/ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES AND LOCATIONS, FROM BS 727-908LEFT WINDOW BELT PANEL BS 727-908 LEFT SIDE.  REPLACED UPPER ROW OF FASTENERS BS 727-908 S-14 L.  REPAIRED PER EA 31780.  (M)


REMARKS:
ROA - DURING 'TRANSIT CHECK' EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK RIGHT NR 2 WINDOW POST.  STOP DRILLED AND PRIMED.  REPAIRED PER TYPICAL REPAIR 53-10-01 REV A PAGE 3.  (M)


REMARKS:
ROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK FORWARD ENTRY DOOR UPPER HINGE CUTOUT, STATION 303.37 STRINGER 10-L, IN FUSELAGE SKIN.  REMOVED DAMAGE AND INSTALLED DOUBLER.  REPAIRED PER SRM 53-30-3, FIG 21 DETAIL 1.  (M)


REMARKS:
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 45 INCHES OF STRINGER 27L CORRODED, STRINGER 27L BETWEEN STATION 948 TO 993.  REMOVED CORROSION AND INSTALLED STRINGER SPLICE.  (M)


REMARKS:
ROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 6 INCHES OF STRINGER CORRODED STRINGER 27R AT STATION 965.  REMOVED CORROSION AND INSTALLED STRINGER SPLICE.  (M)


REMARKS:
MSP - FLT NR 1090 - AIRCRAFT WOULD NOT PRESSURE AFTER TAKEOFF.  FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND L1 DOOR NOT CLOSED PROPERLY.  RECLOSED DOOR, PRESSURIZATION CHECKED NORMAL.  (M)


REMARKS:
PIT - DURING Q-5/C-1 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON BELT FRAME, STA 1309, BETWEEN LONGERON 28R AND LONGERON 28L.  CORROSION TASK NR C57-53300.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-03, FIGURE 2A.  (X)


REMARKS:
PIT - DURING C-6 INSPECTION, FOUND 2 CRACKS APPROXIMATELY 2.25 INCHES IN LENGTH IN SHEAR CLIP AND PREVIOUS REPAIR DOUBLER AT FRAME STA 1019, LONGERON 14L.  REMOVED DAMAGED AREA AND INSTALLED FILLER, REPAIR ANGLES, AND NEW SHEAR CLIP PER USAIR E.A. NR 31774. (X)


REMARKS:
PIT - DURING Q-1/C-3 INSPECTION, FOUND A 3 INCH CRACK, VERTICAL STABILIZER FRONT SPAR AFT OF CANTED FRAME 1388.  REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLES PER SRM 55-02-26.  (X)


REMARKS:
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND 1 INCH CRACK AT RIVET HOLE IN LONGERON 2R AT STA 1418, OUTBOARD LEG.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 5.  (X)


REMARKS:
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND 2 INCH BY 5 INCH LEVEL 1 CORROSION PREVIOUSLY REWORKED AFT SIDE OF FRAME WEB, STA 1338, BETWEEN LONGERONS 28R AND 28L.  REMOVED CORRODED AREA OF WEB AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-16.  (X)


REMARKS:
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND 4 INCH CRACK IN FRAME MLG JAMB KEEL AREA, STA 937, CENTER SECTION.  MANUFACTURED DOUBLER AND ANGLE REPAIR PER SRM 53-05.  (X)


REMARKS:
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND TOOLING MARKS (GOUGES), 6 INCH BY 4 INCH AREA BETWEEN LONGERON 27L AT BOTTOM LT SIDE OF AFT PRESSURE BULKHEAD.  INSTALLED DOUBLER TYPE REPAIR PER SRM 53-03, FIGURE 20.  (X)


REMARKS:
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND LOWER FORWARD CARGO DOOR PAN CORRODED/CRACKED IN 2 PLACES APPROXIMATELY .50 INCH IN LENGTH EACH.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-05, FIGURE 44.  (X)


REMARKS:
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND .75 INCH VERTICAL CRACK AFT SIDE OF STA 1388, CANTED FRAME, IN ANGLE ON LEFT FRONT SPAR OF VERTICAL STABILIZER.  INSTALLED ANGLE REPAIR PER SRM 55-02, FIGURE 26.  (X)


REMARKS:
PIT - WHILE ACCOMPLISHING X-RAY INSPECTION OF PYLON AREA IN BOS, MAINTENANCE DISCOVERED A .25 INCH CRACK IN SKIN AT STA965, LONGERON 14L.  AIRCRAFT WAS MAINTENANCE FERRIED TO PIT FOR REPAIR.  INTERIM EXTERNAL DOUBLER REPAIR INSTALLED PER USAIR EA NR 31838.  AIRCRAFT RELEASED TO SERVICE.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION .50 INCH BY 66 INCHES AT Z-ANGLE AT FORWARD SERVICE DOOR AREA STA 294 TO STA 360.  REPLACED Z-ANGLE.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2. (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH BY .50 INCH HOLE AT WEB OF FLOOR BEAM, STA 1016 PLUS 6 INCHES, RBL 6.  INSTALLED DOUBLER.  REPAIRED PER SRM 51-40-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION AT SEAT TRACKS 1 INCH BY 1 INCH, RBL 8, RBL 24, AND RBL 36 AT STA 986 - STA 1016.  REPLACED THREE SEAT TRACKS.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 1 INCH ROUND AREA AT NUTPLATE CORRODED, FLOOR WEB 10 INCHES AFT OF FLOOR BEAM, BS 1016, BL ZERO.  CUT OUT CORROSION, INSTALLED DOUBLER.  REPAIRED PER SRM 51-40-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON INTERCOSTAL CLIP NUT HOLES, STA 957.  MANUFACTURED NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1.50 INCH BY 1 INCH CORROSION AT FRAME BS 992.  MANUFACTURED FRAME REPAIR, HEAT TREATED, AND INSTALLED.  REPAIRED PER SRM 51-40-3, SPM 20-30-06.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL RBL 12, STA 294 - STA 312.  INTERCOSTAL REPLACED. REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL RBL 11, STA 316.  INSTALLED NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C52-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON TOP FLANGE OF INTERCOSTAL, RBL 11, STA 328 TO STA 344.  INSTALLED NEW PART ON AIRCRAFT.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON INTERCOSTAL, LBL 10, STA 296.  INSTALLED NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-1, RESTORED TO ORIGINAL.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND CORROSION .50 INCH BY 1 INCH FORWARD SERVICE DOOR SILL PLATE SUPPORT ANGLE.  REPLACED ANGLE, REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 3 INCH BY 8 FEET CORROSION FS 328, RBL 10 INCHES, RBL 58 INCHES, TEE CAP.  INSTALLED LOCAL MANUFACTURED TEE CAP AND SPLICED ANGLES.  REPAIRED PER T.R. 53-10-13, EA 40349.  CORROSION LEVEL 1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH BY 48 INCH CORRODED CABIN FLOOR BEAM, BS 328 AT RBL 10 INCHES - RBL 58 INCHES.  REMOVED CORRODED SECTION OF T-CAP AND SPLICED IN NEW SECTION.  REPAIRED PER TR 53-10-13.  CORRISION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH FLOOR SUPPORT ANGLE CORRODED AT CLIP NUT HOLES, STA947 - STA 986, BL ZERO, WL 208.1.  INSTALLED NEW PRE-FAB ANGLE.  WEIGHT CHANGE LESS THAN 1 POUND.  REPAIRED SRM 51-10-1, PAGE 5.  CORROSION LEVEL 1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES, STA 986 - STA 1016, RBL 24 AND RBL 26, WL 208.1 SEAT TRACK.  REPLACED SEAT TRACKS, REPAIRED PER SRM 51-10-01.  CORROSION LEVEL 1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORRODED Z-ANGLE AT LEFT REAR CABIN ENTRY DOOR, STA947 - STA 986, LBL 50, WL 208.1.  INSTALL NEW PREFABRICATED Z-ANGLE.  WEIGHT CHANGE LESS THAN 1 POUND.  REPAIRED PER SRM 510-10-1, PAGE 5, ITEM 4.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 36 INCH AREA OF SURFACE CORROSION, 1 INCH CIRCLE OF EXFOLIATION AT RIGHT REAR CABIN DOOR Z-ANGLE, STA 947 - STA 1006, RBL 50, WL 208.1.  REPLACED Z-ANGLE.  REPAIRED PER SM 51-10-01.  CORROSION LEVEL 1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 4.5 INCH BY 6.5 INCH CORROSION, BS 550A PLUS 10 INCHES, STRINGER 28 RIGHT, FUSELAGE SKIN.  INSTALLED DOUBLER, REPAIRED PER EA 40449.  CORROSION LEVEL 1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CLIP-NUT HOLES CORRODED ENTIRE LENGTH OF FLOOR BEAM STA 986.5, RBL 70- LBL 70 FLOOR BEAM WL 208.1.  REPLACED T-CAP OF BEAM.  REPAIRED PER TR 53-10-05 C.  CORROSION LEVEL 1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 36 INCH BY 22 INCH DOUBLER PREVIOUSLY INSTALLED EXTERNAL SKIN OF AFT CARGO DOOR FUSELAGE SKIN.  DOUBLER INSTALLED, REPAIRED PER 737-200, SRM 52-00-3, FIGURE 5.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 9 INCH BY 5.50 INCH DOUBLER PREVIOUSLY INSTALLED FUSELAGE SKIN, BS 847, S22R.  REPAIR IS PER SRM, DOUBLER INSTALLED, REPAIRED PER SRM 737-200, SRM 53-30-3, FIGURE 1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK EDDY CURRENT, FOUND CRACKED FRAME .5 INCH LONG AT STA 727, S18R.  REPLACED FRAME SECTION, EO 5394G068.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT LBL 25 INTERCOSTAL 1 INCH FORWARD OF BS 520, FLOOR BEAM WL 206 (UPPER CHORD).  REPLACED INTERCOSTAL PER SRM 51-10-2.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND SIX, .25 INCH CRACKS, BL ZERO, LONGITUDINAL FLOOR BEAM WEB BETWEEN STA 707 - STA 713, WL 203.  INSTALLED REPAIR DOUBLER, REPAIRED PER BOEING DRAWING NR 65C34537.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1 INCH BY 1 INCH DENT STA 907, S17L, SKIN.  INSTALLED 1.50 INCH BY 1.50 INCH FILLER 2024-T3 .080, AND 7 INCH BY 8 INCH DOUBLER 2024-T3 .090.  REPAIRED PER SRM 53-30-3, FIGURE 28.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND SEVERAL CRACKS IN HOLES BETWEEN S20L AND S21L, ONE, .50 INCH CRACK ATATTACH HOLE FOR TRANSITION ANGLE FRAME, BS 460, LEFT SIDE.  CUT OUT CRACK AT TRANSITION AREA OF FRAME AND BETWEEN S20L AND S21L.  MANUFACTURED, HEAT TREATED, AND INSTALLED REPAIR AND FILLER.  REPAIRED PER SRM 20-30-06, SRM 53-10-4.  (X)


REMARKS:
IINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY .1850 INCH, BS 727, S18A, LEFT SIDE.  INSTALLED SPLICE STRAPS, REPAIRED PER EA 40542.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .3750 INCH CRACK S4R TIE CLIP STA 707.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK STA 767 AT STRINGER 10 RIGHT, TIE CLIP.  REPLACEDTIE CLIP PER EO 5393G227.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG STA 747 AT STRINGER 6 RIGHT, TIE CLIP.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG AT TIE CLIP, STA 727, STRINGER 5 RIGHT.  REPLACEDTIE CLIP, REPAIRED PER EO 5393G227.  (X)


REMARKS:
INT - DURNG 'Q-2' CHECK EDDY CURRENT INSPECTION, FOUND 2 CRACKS IN AFT OPEN FASTENER HOLE BS 727, OUTBOARD CHORD, BS 727, STRINGER 18L, IN OUTBOARD CHORD.  INSTALLED LEFT 727 OUTBOARD CHORD, REPAIRED PER EO 5394G068 AND 262-21-93828.  (X)


REMARKS:
INIT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH DENTED AREA PRESSURE BULKHEAD, STA 727, BULKHEAD RBL 40.  REPAIRED OVERSIZED FASTENER HOLES AND INSTALLED REPAIR PER EO. WEIGHT CHANGE LESS THAN 1 POUND.  REPAIRED PER EO 5394G068 AND BOEING DRAWING 65C33722.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG AT WEB, STRINGER 18A RIGHT, STA 727.  INSTALLED DOUBLER, REPAIRED PER EA 40452.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 1 INCH CORROSION ON FLOOR BEAM BS 344, LBBL 15.  INSTALLED NEW T-CAP REPAIRED PER TR 53-10-13.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 15 INCH CRACK IN HINGE AT LOWER GATE, LOWER GATE HINGE OF FORWARD GALLEY DOOR.  INSTALLED IMPROVED PART, REPAIRED PER EA 40349.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG IN STRINGER 18A LEFT, STA 727.  INSTALLED DOUBLERS, REPAIRED PER EA 40452.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .3750 INCH CRACK S27L (KEEL BEAM) TO BS 727 BULKHEAD ATTACH ANGLE 1 INCH AFT OF BULKHEAD PLUS 5 INCHES ABOVE LOWER SKIN T-SPLICE.  INSTALLED PREFABRICATED T-SPLICE, REPAIRED PER BOEING DRAWING 69-41460.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK STA 727 BULKHEAD STIFFENER FITTING LBL 25, WL 202.5.  REPLACED FITTING.  REPAIRED PER SRM 5-10-1.  (X)


REMARKS:
INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1.25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM AT AILERON QUADRANT STA676.  WL 206.5.  INSTALLED DOUBLER, REPAIRED PER EA 40395, EO 5791G632.  (X)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND A .25 INCH CRACK COMING FROM RIVET AT STA 101, LEFT AFT OF STRAKE IN SKIN.  REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR PER USAIR TYPICAL REPAIR 53-30-11.  (X)


REMARKS:
GSO - FLT 667 - EN ROUTE PIT-RDU, CREW RECEIVED 'HORIZON' ALERT.  FLIGHT DIVERTED TO GSO DUE TO WEATHER AND LANDED WITHNO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 1 VERTICAL GYRO.  (X)


REMARKS:
PIT - FLT 987 - AFTER TAKEOFF FROM PIT, CREW EXPERIENCED LOSS OF RADIO COMMUNCIATIONS.  SHORTLY THEREAFTER, ONE RADIO BEGAN TO WORK.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE CAPTAIN'S AUDIO SELECTOR PANEL AND MICROPHONE.  (X)


REMARKS:
CLT - FLT 521 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF.  STOPPED AT 8,000 FEET ABOVE AGL, THEN RETURNED TO CLT.  ON DESCENT AT 2,000 FEET, AIRCRAFT STARTED TO PRESSURIZE.  MAINTENANCE REPLACED OUTFLOW VALVE DUE TO STICKING.  OPS CHECKED OK.  (X)


REMARKS:
MCI - FLT 469 - DURING CRUISE, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED.  REMOVED AND REPLACED NR 3 STRUT DUCT SEAL, MFG PN 10-61065-2.  OPERATIONAL CHECK NORMAL.  CHECK C-1 - 4-28-95 - MCI.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK, RBL 22, STA 200 - STA 232.  INSTALLED NEW SECTION OF TRACK PER SRM 51-01 AND SPLICED PER SRM 53-05, FIGURE 4I.  AIRCRAFT TOTAL TIME:  25,931 HOURS; 13,041 CYCLES.


REMARKS:
DURING OP-16, FOUND CORROSION ON FORWARD END OF NR 3 FLOOR TRACK.  INSTALLED NEW SECTION OF TRACK PER SRM 51-01, AND SPLICED PER SRM 53-05, FIGURE 4F.  AIRCRAFT TOTAL TIME:  25,931 HOURS; 13,041 CYCLES.


REMARKS:
STL - FLT 141 - DURING LANDING AND TAXI, THE EGRESS LIGHTS FLICKERED ON AND OFF.  FOUND BATTERY PACK, MFG PN 5822-2, WEAK.  REPLACED BATTERY PACK AND EGRESS LIGHT, OPERATION CHECKED NORMAL.  CHECK C - 8-27-95 - STL.


REMARKS:
STL - FLT 99 - DURING APPROACH, SMOKE EMITTED INTO AFT CABIN AND COCKPIT.  FOUND LEFT AND RIGHT COALESCER ELEMENTS, MFGPN 179460-8-1, CONTAMINATED.  REPLACED LEFT AND RIGHT COALESCER ELEMENTS AND AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL.  CHECK C-2D - 10-17-95 - MCI.


REMARKS:
STL - FLT 568 - AFTER TAKEOFF, NR 1 ENGINE FIREWARNING LIGHT ILLUMINATED.  REMOVED AND REPLACED CRACKED 8TH STAGE DUCT. OPERATIONAL LEAK CHECK ACCOMPLISHED, NO LEAKS FOUND.  OP-15 - 8-21-95 - STL.


REMARKS:
STL - FLT 298 - DURING CRUISE, HAD AN ELECTRICAL FLASH AND ODOR EMITTED FROM CIRCUIT BREAKER PANEL.  FOUND CIRCUIT BREAKER FOR FLIGHT DECK TEMPERATURE CONTROL WITH INTERNAL MALFUNCTION.  REPLACED TEMPERATURE CONTROL CIRCUIT BREAKER, MFG PNBAC18R2A.  FLIGHT DECK TEMPERATURE CONTROL CHECKED NORMAL. CHECK C - 6-19-95 - STL.


REMARKS:
STL - FLT 394 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DOOR OPEN LIGHT REMAINED ON.  VISUAL CHECKSHOWED LANDING GEAR DOORS TO BE CLOSED.  FOUND PIN PUSHED BACK IN RIGHT GEAR DOOR SWITCH CONNECTOR.  SECURED PIN IN RIGHT GEAR DOOR SWITCH CONNECTOR.  LANDING GEAR DOOR OPERATION AND INDICATION CHECKED NORMAL.  CHECK C - 8-11-95 - STL.


REMARKS:
STL - FLT 541 - AFTER TAKEOFF, LANDING GEAR RETRACTION LEFT MLG UNSAFE LIGHT REMAINED ON.  CYCLED LANDING GEAR AND LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED.  FOUND LEFT MLG DOOR LATCH HOOK NOT LATCHING INTO POSITION.  RIGGED DOOR LATCH ROLLER ASSY.  LANDING GEAR AND DOOR OPERATION AND INDICATION CHECKED NORMAL.  CHECK C - 8-11-95 - STL.


REMARKS:
ATL/RDU - FLT 292 - ON LANDING ROLL-OUT, CREW REPORTED BOTH MAIN TIRES ON RT SIDE BLOWN.  AIRCRAFT NOT ABLE TO CLEAR RUNWAY.  MAINTENANCE FOUND THE RT MAIN GEAR TORQUE LINKS HAD FAILED ALLOWING WHEELS/AXLES TO ROTATE HORIZONTALLY.  AIRCRAFT FERRIED TO MIA FOR FURTHER EVALUATION.  REPLACED RT MLG ANTI-SKID TRANSDUCER HARNESS PER DC9 MM 32-43-2.  REMOVED RT MAIN GEAR PISTON ASSY.  INSPECTED RT MLG STRUT INTERNAL SURFACES, NO DEFECTS NOTED.  INSTALLED RT MLG PISTON ASSY PER DC9MM 32-11.


REMARKS:
PHL/PHL - FLT 545, CREW ADVANCED THROTTLES ON TAKEOFF AND GOT A TAKEOFF WARNING HORN AT APPROXIMATELY 15 KNOTS.  CYCLEDFLAPS AFTER CLEANING THE TAKEOFF WARNING SWITCH.  NO DEFECTS NOTED.


REMARKS:
IAD/RDU - FLT 295-1 - PILOT REPORTED LEFT HYDRAULIC PUMP FAILURE.  DIVERTED FLIGHT TO ATL FROM RDU.  REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP.  OPS CHECK NORMAL.  PER MM 29-10.


REMARKS:
FLT 543 - AIR RETURN, NOSE GEAR UNSAFE LIGHT ON WHEN GEAR WAS RETRACTED.  LOWERED GEAR AND GOT 3 EACH GREEN LIGHTS AND LANDED.  REMOVED AND REPLACED DOWN LINE CHECK VALVE, PERFORMED SEVERAL GEAR SWINGS AND UPLATCH CHECKS.  OPS CHECK NORMALPER MM 32-10.


REMARKS:
AT 37,000, EXPERIENCED NUMBER 2 ENGINE OIL PRESSURE DROP,  THEN ENGINE STOPPAGE.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT DIVERTED TO TUS AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 2 ENGINE PER BOEING M/M.


REMARKS:
AFTER GEAR RETRACTION, UPON GEAR HANDLE BEING POSITIONED TO OFF, INBOARD GEAR ANTI-SKID LIGHT ILLUMINATED.  LIGHT EXTINGUISHES WITH HANDLE IN UP OR DOWN POSITIONS.  AIRCRAFT DIVERTED TO BNA AND MADE AN UNEVENTFUL LANDING.  AT HOU, REPLACEDRT INBOARD ANTI-SKID VALVE PER BOEING M/M.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND STRINGER SPLICE AT S27L CORRODED AT BS 947.5 AND 967.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND WEB FWD FLANGE TO FRAME CRACKED AT S7L AT BS 294.  REPAIRED PER BOEING SRM.


REMARKS:
FLT 18 - UPON GEAR EXTENSION, NOSE GEAR GREEN LIGHT ILLUMINATED.  RED NOSE GEAR LIGHT ALSO REMAINED ILLUMINATED.  FOLLOWED AIRCRAFT MANUAL PROCEDURES AND RECEIVED VISUAL FROM TOWER.  BOTH INDICATED DOWN AND LOCKED.  REMOVED AND REPLACED NOSE LOCK SWITCH IAW 32-61-71.  OPERATIONAL CHECK NORMAL.  (X)


REMARKS:
JFK - DURING CRUISE, NR 1 ENGINE LOST OIL.  ENGINE FUEL PUMP SEAL, TW 25052 MFG 378201-7, WAS WORN.  REPLACED MFG A03128CHGA.  LEAK CHECK OF FUEL PUMP GARLOCK SEAL WAS NORMAL.


REMARKS:
STL - DURING LANDING, CREW RECEIVED AN UNSAFE GEAR INDICATION.  REPLACED RIGHT MAIN LANDING GEAR DOOR ACTUATOR.  TW P/N10395 MFG 7-3141-4.  PERFORMED GEAR SWING ALL THREE OPERATIONS CHECK NORMAL.


REMARKS:
FLT NR 167 - SFO - DURING LANDING, NR 2 ENGINE THROTTLE STUCK MID POSITION.  ENGINE SHUT DOWN.  APPARENT CAUSE OF TROUBLE, PORTABLE WATER SUPPLY LINE FROZE AND RUPTURED.  REPAIRED WATER LINE IN CEILING OF AFT CARGO PIT.


REMARKS:
FLT NR 471 - STL - DURING CLIMB, MAIN LANDING GEAR HANDLE WOULD NOT TRAVEL BEYOND ONE-THIRD OF TRAVEL.  SPOILERS WOULD NOT ARM FOR LANDING.  FOUND WIRE BUNDLE BLOCKING GEAR CONTROL LEVER.  REPOSITIONED TO CLEAR AND SECURED WIRE BUNDLE.  GEAR SWING OPERATIONS NORMAL.


REMARKS:
PHX - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT.  FOUND NOSE STRUT FLAT.  REPLACED SCHRADER VALVE O-RING, MFG P/N MS28778-7, AND SERVICED STRUT WITH OIL AND AIR.  EXTENDED NOSE STRUT TO FULL EXTENSION AND BACK DOWN WITH NO FINDING.  NOSE LANDING GEAR CHECKS NORMAL.


REMARKS:
JFK - FLT NR 881 - DURING TAKEOFF, EXPERIENCED LOSS OF HYDRAULIC FLUID.  RETURNED FOR LANDING.  REMOVED AND REPLACED RIGHT AUX AND RIGHT ENGINE DRIVEN PUMPS AND FILTERS.  TW 92190 MFG 428177 S/N 407390 AND TW 800877 MFG 314195 S/N 388244 RESPECTIVELY.  PRESSURIZE AND LEAK CHECK.  NO LEAKS.


REMARKS:
TPA - DURING LANDING, UNABLE TO LOWER NOSE GEAR.  CYCLED LANDING GEAR.  NOSE STRUT SEALS REPLACED, REPACKED NOSE STRUT. CYCLED GEAR AND OPERATIONS ARE NORMAL.


REMARKS:
STL - FLT NR 202 - DURING CRUISE, THERE WAS AN ELECTRICAL SMELL COMING FROM THE RECIRCULATING FAN, P/N 605457-7 TWPN 12801.  CIRCUIT BREAKER PULLED AND PLACARDED.  DECEMBER 24, 1995, MSP REPLACED RECIRCULATION FAN.  OPERATIONS CHECK NORMAL.


REMARKS:
STL - DURING CRUISE, SHUTDOWN NR 2 ENGINE, S/N 1526, DUE TO DECREASING OIL PRESSURE AND OIL QUANTITY.  FOUND OIL CAP MISSING, REPLACED OIL CAP, INSPECTED OIL SCREEN, SERVICED OIL, RAN AND LEAK CHECKED ENGINE.  OPERATIONS CHECKED NORMAL.  (M)


REMARKS:
OKC - FLT NR 265 - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON.  CHECKED AND LUBRICATED LANDINGGEAR VALVE.  OPERATIONAL CHECK NORMAL.


REMARKS:
MCO - FLT NR 265 - DURING DESCENT, SMOKE WAS DETECTED IN AFT LAVATORIES.  LAVATORY CIRCUIT BREAKERS WERE PULLED, SMOKE IMMEDIATELY CEASED AND DISSIPATED.  THE LAVATORY WATER HEATERS WERE FOUND WITH NO WATER IN THEM.  HEATERS WERE PURGED AND OPERATIONIONALLY CHECKED.  OPERATIONAL CHECK NORMAL.


REMARKS:
FLT NR 741 - SEA - DURING DESCENT, THE LEADING EDGE FLAP/SLAT LOCKOUT LIGHT ILLUMINATED.  RESET BOTH ASYMMETRICAL BRAKES, FLAP/SLAT OPERATION CHECKED NORMAL.


REMARKS:
STL - FLT 124 - DURING LAYOVER, MAINTENANCE FOUND RIGHT AFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE.  REMOVED AND REPLACED LIGHT BULB.  OPERATIONAL CHECK NORMAL.


REMARKS:
JFK - FLT NR 227 - AFTER TAKEOFF, THE NOSE LANDING GEAR UNSAFE LIGHT CAME ON.  RETURNED TO JFK.  NOSE STRUT FLAT.  CHANGED SHRADER VALVE, TWA 32-5315 MFG MS28778-7.  SERVICED NOSE STRUT WITH HYDRAULIC FLUID AND DRY NITROGEN.  LEAK CHECK OK.


REMARKS:
FLT NR 312 - SMF - AFTER TAKEOFF, SMOKE EMITTED INTO CABIN.  FLIGHT RETURNED.  FOUND RIGHT ENGINE HAD INGESTED A BIRD.REPLACED RIGHT ENGINE, S/N 3256.  ENGINE OPERATION AND AIR CONDITIONING SYSTEMS OPERATION CHECKED NORMAL.


REMARKS:
STL - FLT NR 2 - DURING CRUISE, NR 2 ENGINE CSD FAILED.  NR 2 CSD WOULD NOT DISCONNECT.  SHUT DOWN NR 2 ENGINE.  REMOVED AND REPLACED NR 2 ENGINE CSD, MFG P/N 705117E, AND REPAIRED CSD SOLENOID GROUND WIRE.  OPERATIONAL CHECK NORMAL.


REMARKS:
FCO - DURING CRUISE, SHUT DOWN NR 2 ENGINE, S/N 4181, DUE TO DECREASING OIL QUANTITY.  FOUND OIL LEAKING FROM INTEGRATED DRIVE GENERATOR DRIVE CAVITY DRAIN.  CAPPED DRAIN LINE.  ENGINE LEAK CHECK WAS NORMAL.


REMARKS:
FLT NR 444 - ATL- AIR RETURN - ON TAKEOFF BOTH NAV SYSTEMS WERE INOP.  NAV TRANSFER CIRCUIT BREAKER WOULD NOT RESET.  REMOVED AND REPLACED NAV SWITCHING UNIT.  OPS CHECK WITH T/C-30 IAW 34-10.  (M)


REMARKS:
FLT 496 - ATL - AIR RETURN - THE CREW REPORTED FUEL VENTING FROM THE RIGHT WING.  MAINTENANCE FOUND 2 SCREWS ON NR 3 PROBE WOULD NOT TIGHTEN.  REPLACED 2 NUT PLATES AND 2 SCREWS.  LEAK CHECKED OK PER MM 28-15.  (M)


REMARKS:
FLT NR 515 - ATL - WHEN THE AIRCRAFT WAS PASSING THROUGH 17,000 FEET WHEN IT LOST CABIN PRESSURE AND WAS UNABLE TO CONTROL MANUALLY.  AIR RETURN.  FOUND LEFT AND RIGHT PACK DUCTS BLOWN OFF AT WATER SEPARATORS, REINSTALLED LEFT AND RIGHT DUCTS AND REPLACED LEFT COALESTER BAG.  PRESSURIZED AIRCRAFT OPS CHECKED GOOD.  (M)


REMARKS:
FLT NR 580 - ATL - AIRCRAFT RETURNED, WAS UNABLE TO PRESSURIZE AFTER TAKEOFF.  NO DOOR LIGHTS ON AIRCRAFT.  AIRCRAFT RETURNED TO GATE FOUND E/E DOOR OPEN.  FOUND DOOR LIGHT SWITCH INOP.  DEFERRED DOOR SWITCH FOR REPAIR, CLOSED DOOR DISPATCHED AIRCRAFT.  CONTROL NR DM05712, SEQ 33-17.  (M)


REMARKS:
FLT NR 278 - ATL-CMH - THE AIRCRAFT EXPERIENCED A TAIL COMPARTMENT HIGH TEMP INDICATION, THE FLIGHT DIVERTED TO CHA.  FOUND SEVERAL LOOSE CLAMPS ON LEFT PACK AND FLOW CONTROL VALVE TIGHTENED SAME.  RAN TO 1.9 EPR, NO LEAKS NOTED.  (M)


REMARKS:
FLT NR 231 - ATL - AIRCRAFT RETURNED AFTER TAKEOFF AND GEAR RETRACTION LEFT GEAR DOOR OPEN LIGHT CAME ON IN FLIGHT.  REMOVED AND REPLACED LEFT LANDING GEAR DOOR SWITCH IAW MM 32-10, OPS CHECK GOOD.  (M)


REMARKS:
FLT NR 229 - ATL-DFW - UPON GEAR EXTENSION LEFT MAIN GEAR DOOR UNSAFE LIGHT AND GREEN DOWNLOCK LIGHTS WERE INTERMITTENT.  FOUND CANNON PLUG ON LEFT DOWN LOCK SWITCH LOOSE.  SECURED CANNON PLUG AND SAFTIED IAW VALUJET MAINTENANCE MANUAL.  (M)


REMARKS:
BOS - FLT 1204 - EN ROUTE PHL-PWM, THE OUTER PANE OF THE CAPTAIN'S WINDSHIELD BEGAN TO ARC AND CRACK.  FLIGHT DIVERTED TO BOS AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE WINDSHIELD AND THE WINDSHIELD HEAT CONTROLLER.  (X)


REMARKS:
PHL - FLT 451 - UNABLE TO PRESSURIZE AIRCRAFT.  FOLLOWED ALL USAIR PROCEDURES, NO HELP.  F/A ADVISED IN PHL THAT THE DOOR WAS HARD TO SHUT.  ALSO, HAD TO SHUT DOWN AND RESTART LEAVING DCA PRIOR TO STARTING ENGINE.  THERE WAS A PRESSURE BUMP.  FOUND CABIN DOOR NOT PROPERLY CLOSED.  FALSE LOCK INDICATION.  OPS CHECK DOOR OPERATION.  OPS CHECK GOOD.  PRESSURIZED AIRCRAFT AND INSPECTED DOOR.  OPS CHECK GOOD.  (X)


REMARKS:
DFW/DFW - FLT 224 - ON CLIMB-OUT AT APPROXIMATELY 5,000 FEET, THE CREW HEARD A LOUD BANG, MODERATE VIBRATION WAS FELT AND N1 READING DROPPED TO APPROXIMATELY 60 PERCENT.  CREW SHUT DOWN NR 2 ENGINE.  SUBSEQUENT TO ENGINE REMOVAL, ENGINE WAS BORESCOPED TO DETERMINE THE CAUSE OF FAILURE AND EXTENT OF DAMAGE.  BORESCOPE FINDINGS REVEALED 1ST STAGE TURBINE BLADE FAILURE WITH RESULTANT LPT TURBINE BLADE AND VANE DAMAGE (FAILURE WAS CONTAINED).  BORESCOPE FINDING OF THE HPC 6TH STAGE AND HPC 7TH AND 13TH STAGES WERE NORMAL.  ENGINE CHANGE IN PROCESS.


REMARKS:
ATL/MDW - FLT 59 - INBOARD FLAPS WOULD NOT RETRACT ABOVE 15 DEGREES.  AIR TURN BACK TO ATL.  ON SYSTEM OPS AND INSPECTION, FOUND FLAPS IN BYPASS MODE.  RESET ASSYMETRY.  FOUND LOOSE TORQUE TUBE COUPLING AT OUTBOARD FLAP POWER CONTROL UNIT. SECURED LOOSE TORQUE TUBE COUPLING, RETORQUED SCREWS.  OPS CHECK OK PER 27-51-01.  (X)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT FLOORBEAM TOP FLANGE RT LAV STA 1338 CORROSION TASK NR C58-53300.  REMOVED AND REPLACED TOP FLOOR ANGLE AND INSTALLED BEAM SPLICE PER USAIR TYPICAL REPAIR 53-10-14.  (W)


REMARKS:
LAX - DURING CHECK C-9C, FOUND AT AFT PRESSURE BULKHEAD, STR 56 SEVERED.  REPAIRED BY FITTING/FASTENERS INSTALLATION PER SB 093-53-105.  AIRCRAFT TOTAL TIME:  63,490 HOUS; 23,355 CYCLES.


REMARKS:
STL - FLT 721 - DURING APPROACH, LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT.  COMPLETED APPROACH AND LANDING.  FOUND FUEL PUMP, MFG PN 706800, MALFUNCTION.  REPLACED ENGINE FUEL PUMP AND ENGINE FUEL CONTROL, MFG PN 773333-21.  ENGINE OPERATION THEN CHECKED NORMAL.  CHECK C-1C - 12-28-95 - LAX.


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND THREE 1-2 INCH CRACKS, BL 0 BS 500 G TO BS 520 INTERCOSTAL.  REMOVED, FABRICATED AND INSTALLED NEW UPPER CHORD ANGLE.  REPAIRED PER DRAWING 65C34688.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ONE .5 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 312 TO BS 328 INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK S-10 L TIE CLIP STATION 747.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 727 BULKHEAD STIFFENER ATTACH FITTING BL 0, WL 202.5.  REPLACED FITTING.  REPAIRED PER EO 5394G176.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 3L TIE CLIP STATION 707.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
CLT - CLT INSPECTION, FOUND BY EDDY CURRENT 1 INCH CRACK AT FLOOR BEAM AT STATION 520 EXTENDING .5 INCH OUTBOARD AND .5INCH INBOARD OF LBL 45.5.  REPAIR DOUBLER INSTALLED AS PER USAIR EA NR 40294.  (M)


REMARKS:
FLT NR 263 - ATL - CABIN PRESSURIZATION STARTED TO INCREASE AT 1K FEET PER MINUTE.  FLT DIVERTED TO ATL DUE TO HIGH FUEL CONSUMPTION AT LOWER FLIGHT LEVEL THAT THE A/C WAS REQUIRED TO FLY AT.  NO EMERGENCY WAS DECLARED AND THE OXYGEN MASKSWERE NOT DEPLOYED.  (M)


REMARKS:
FLT 2301 - SYR - ON TAKEOFF, AUTO PRESSURIZATION FAILED.  STANDBY WOULD NOT PRESSURIZE THE AIRCRAFT.  LEVELED OFF AT 8000 FEET AND RETURNED TO SYR.  (M)


REMARKS:
FLT NR 8582 - RSW - AFTER SECOND APU START ATTEMPT APU FIRE LIGHT ILLUMINATED APU FIRE SWITCH PULLED AND BOTTLE DISCHARGED.  REMOVED AND REPLACED THE APU FCU.  ADJUSTED CRACK PRESSURE.  CLEANED SHROUD DRAINS.  REPLACED IGNITOR LEADS.  APU OPS NORMALLY.  (M)


REMARKS:
FLT NR 1177 - BWI - RETURN TO FIELD, UNABLE TO RETRACT LANDING GEAR.  GEAR HANDLE WOULD NOT GO TO UP, DID NOT ATTEMPT TO OVERRIDE.  (M)


REMARKS:
TPA/MDW - FLT 42 - DIVERTED TO ATL WHEN CABIN RATE OF CLIMB WENT TO 1,000 FPM UP, COULD NOT CONTROL RATE IN AUTO OR MANUAL.  FOUND LEFT PACK VALVE NOT OPENING.  REMOVED AND REPLACED LEFT PACK VALVE, PRESSURIZATION AND OPS CHECK OK PER MM 21-30-0.  (X)


REMARKS:
ATL/TPA - FLT 17 - DURING CLIMB-OUT, UNABLE TO CONTROL CABIN PRESSURIZATION.  AIRCRAFT RETURNED TO ATL DUE ONE PACK OUT.  FOUND WIRES BAD ON 210 DEGREE SENSOR BULB WHICH CAUSED PACK TEMP OVERHEAT LIGHT AND TRIPPED OFF LEFT PACK.  REPAIRED WIRES AND PERFORMED PRESSURIZATION AND OPS CHECK OK PER MM 21-30-0.  (X)


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BS 178 BULKHEAD CRACK INDICATIONS AROUND RIVET HEAD FWD SIDE, WL 234, RBL 0.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND TRANSVERSE FLOORBEAM AT BS 312 CRACKED ON LOWER CHORD AFT FLANGE, LBL 62.  REPAIREDPER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AIRSTAIR DOORWAY UPPER STOP SUPPORT INTERCOSTAL CRACKED AROUND UPPER/FWD STOP FITTING.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR HINGE CUTOUT CRACKED AT UPPER HINGE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT CRACKED AT BOTTOM RADIUS.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FRAME CRACKED ABOVE FWD I/B DOOR STOP.  REPAIRED PER SWA ACO 577-52.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND CENTER FLOORBEAM STRAP BROKEN IN E AND E COMPARTMENT.  REPAIRED PER BOEING SRM.


REMARKS:
AFTER FLAP RETRACTION, TRANSIT INDICATION LIGHT REMAINED ILLUMINATED ON FWD AND OVERHEAD PANELS.  CYCLED FLAPS TWICE, NO HELP.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  CYCLED SLATS/FLAPS PER BOEING M/M, VERIFIED PROBLEM TO BE INDICATION, DEFERRED AND CONTINUED PER MEL 27-3.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND S17L CRACKED AT END, BS 1088.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE SKIN CRACKS AT BS 178 WL 217 LBL 11 TO 12, AT WL 218 RBL 10 TO 12, AT WL 212 TO 213 RBL 5, AT WL 200 TO 201 RBL 5, AT WL 197 TO 199 LBL 5 AND WL 201 TO 202.5 LBL 5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S15L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AND STRINGER AT BS 333, S8R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED BS 616, S5L, S8R AND AT BS 277, S10 AND 11R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED BETWEEN S15L AND 14L, BS 360, WL 228.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED, BS 294.5, WL 208, RBL 54.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT WING L/E RIB LOWER SURFACE PANEL SUPPORT AT STA 571 CRACKED.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E HAS VEHICLE STRIKE DAMAGE AT STA 567.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E RIB HAS VEHICLE STRIKE DAMAGE AT STA 571.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD UPPER RADIUS OF TORQUE TUBE CUTOUT AT AFT SERVICE DOOR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT THRUST BEAM UPPER I/B ATTACH ANGLE CRACKED AT BS 1113.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 312, S4L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT ON OUTER SKIN CRACKED IN BOTTOM RADIUS.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN BS 420 AND 440, BETWEEN S14 AND 15L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED CHECK, FOUND EGG SHAPED HOLES ON NR 2 VHF ANTENNA DOUBLER.  REPAIRED PER SWA ACO 6470-53.


REMARKS:
DURING SCHEDULED CHECK, FOUND FLOORBEAM SUPPORT AT BS 540, BL 0 TO LBL 25, WL 208 CRACKED.  REPLACED PER SWA ACO 6470-53.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND TRANSVERSE FLOORBEAM AT BS 312 CRACKED ON LOWER CHORD AFT FLANGE, LBL 62.0.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED CHECK, FOUND LT AND RT FWD OUTSIDE EMERGENCY LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED BC1 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT ON FUSELAGE TOP FWD CORNER CRACKED.  REPAIRED PER SWA RA 1-353-909.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT FWD UPPER LOCK CAM PLATE.  REPLACED PER BOEING SRM.


REMARKS:
AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRD STRIKE INSPECTION, FOUND SEVERAL BENT BLADES ON NUMBER 1 ENGINE.  COMPLIED WITH BORESCOPE INSPECTION AND REPLACED BENT BLADES PER BOEING M/M.


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES IN SEVERAL AREAS, BS 302 TO BS 362 LEFT SIDE Z-ANGLE.  REMOVED CORRODED Z-ANGLE, REPLACED AND COMPLETED INSTALLATION.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  REFERENCE USAA951365.


REMARKS:
ROA - DURING CX-6 CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC FOUND FUSELAGE SKIN CRACK, 4.25 INCH LONG, STRINGER 18L,STATION 780.  INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT 3 NUTPLATE HOLES, .075 INCH AT EACH HOLE AFT UPPER SIDE OF STATION 344 FLOOR BEAM, BL 9R TO BL 9L.  T-CAP REPAIR AT FLOOR BEAM LBL 24 TO RBL 24 AS PER BOEING SRM 53-10-03.  (M)


REMARKS:
CLT - CLT INSPECTION FOUND BY EDDY CURRENT, A 2 INCH CRACK LOCATED AT FLOOR BEAM AT STATION 520 EXTENDING 1 INCH OUTBOARD AND 1 INCH INBOARD OF LBL 24.  INSTALLED REPAIR DOUBLER AS PER USAIR EA NR 40294.  (M)


REMARKS:
CLT - CLT INSPECTION FOUND LEVEL 2 CORROSION TOP AND BOTTOM OF UPPER CHORD, T-CAP 986.5 FLOOR BEAM LBL 45.5 TO RBL 45.5.  INSTALLED T-CAP REPLACEMENT PER BOEING SRM 53-10-05 AND USAIR TYPICAL REPAIR 53-10-05.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND A 1 INCH BY .75 INCH AREA OF LEVEL 2 CORROSION ON 986.5 FLOOR BEAM FWD SIDE OF 986.5 FLOOR BEAM LBL 45.5.  INSTALLED UPPER T-CAP REPLACEMENT PER BOEING SRM 53-10-05 AND USAIR TYPICAL REPAIR 53-10-05.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT CLIP UNIT LOCATOR ON FLOOR BEAM TOP SURFACE BS 328 RBL12-RBL22.  ADDED CERAMIC STRAPS TO FLOOR BEAM UPPER CHORD AS PER USAIR TYPICAL REPAIR 53-10-01A.  (M)


REMARKS:
CLT - CLT INSPECTION FOUND BY EDDY CURRENT, A 1.2 INCH FLOOR BEAM CRACK LOCATED AT STATION 520 EXTENDING .7 INCH INBOARD AND .5 INCH  OUTBOARD OF RBL 45.5.  INSTALLED REPAIR DOUBLER AS PER USAIR EA NR 40294.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND LEVEL 2 CORROSION UPPER CHORD OF FLOOR BEAM AT NUTPLATE HOLES, 48 INCH TOTAL LENGTHBETWEEN FS 344 BETWEEN LBL 24 AND RBL 24.  INSTALLED FLOOR BEAM T-CAP REPAIR 48 INCHES TOTAL LENGTH AS PER USAIR TYPICAL REPAIR 53-10-05 AND BOEING SRM 53-10-03.  (M)


REMARKS:
CLT - CLT INSPECTION FOUND A FUSELAGE SKIN CRACK 2 INCHES LONG, LOCATED AT STATION 727, STRINGER 17L.  INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 6.  (M)


REMARKS:
PIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 AT STATION 12791 TO STATION 13851.  SPLICED IN NEW SECTION OF STRINGER NR 3 PER SRM 51-70-06 REPAIR NR 5.  (M)


REMARKS:
PIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 STATION 11257.  SPLICED IN NEW SECTION OF STRINGER PER SRM 51-70-06 REPAIR NR 5.  (M)


