# SDR

REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER 19R CRACKED AT BS 500B.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


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


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTS AT BS 380 TO 384, BETWEEN STRINGERS 16 AND 17L, AT BS 310 TO 315, BETWEEN S18 AND 19R, AT BS 430-450, BETWEEN S25 AND 26R, AT BS 266, BETWEEN S17 AND 18L AND AT BS 500B+8, BETWEEN S24 AND25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND A 4 INCH CRACK AT NUMBER 2 ENGINE PYLON LOWER FRAME AT DRAIN HOLE.  REPLACED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND VERTICAL WEB CRUSHED AND DENTED AT BS 804, WL 160, RBL 19.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME SUPPORT ANGLE CRACKED AT BS 500D, RBL 60, WL 192.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME WEB CRACKED AT BS 493, WL 160, RBL 33.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 94-0864.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 2 ENGINE PYLON INBOARD LOWER CORNER L ANGLE BROKEN.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 4 SLAT T/E SKIN CRACKED.  REPAIRED PER TRAMCO EWO 94-0852.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SUB THRESHOLD VERTICAL WEB CRUSHED AND DENTED AT BS 440-494, RBL 24, WL 152-156.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING BETWEEN STRINGERS 20 AND 21R, BS 902.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 987, WL 207, LBL 42.  REPAIRED PER SWA RA 1-353-542 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 27L CORRODED AT BS 500A+10.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME VERTICAL WEB GOUGED AT BS 188, LBL 12, WL 151.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTS AT BS 385, 2 INCHES ABOVE S16L, AND FROM BS 178 TO 196, BL0 TO LBL 30.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 902, BETWEEN STRINGERS 20 AND 21R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 968, BETWEEN S18 AND 19L AND AT BS 767, BELOW S25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
FLT 62 - JFK - WHEN LANDING GEAR WAS LOWERED FOR LANDING THE NOSE GEAR UNSAFE WARNING LIGHT REMAINED ON.  EXTENDED LANDING GEAR BY ALTERNATE MEANS.  CHECKS REVEALED A MALFUNCTIONING PROXIMITY WARNING BOX.  REPLACED BOX, MFG P/N 008-0004-003.  OP CHECKS NORMAL.  CHECK C-5-13-94 - PHX.


REMARKS:
STL - ON APPROACH THE LEFT ENGINE LOST POWER, SHUT DOWN ENGINE.  FOUND METAL IN TAIL PIPE.  REPLACED ENGINE S/N 3231.  ENGINE TOTAL TIME 28,202.  ENGINE TOTAL CYCLES 15,036.  CHECK C-10 - 1-13-94 MCI.


REMARKS:
JFK - DURING CHECK C-2D, FOUND NR 6 LEADING EDGE SLAT EXTERNAL SURFACE DENTED.  REPAIRED PER 767-300 SRM 57-41-01.  AIRCRAFT TOTAL TIME 7,963, TOTAL CYCLES 3,141.


REMARKS:
SFO - FLT NR 0073 - E/MGEAR DISAGREE AND GEAR AMBER LIGHT ILLUMINATED WIHT THE GEAR ALL GREEN AND DOWN.  THE GEAR WAS RECYCLED AND THE LIGHTS EXTINGUISHED.  MAINTENANCE PERFORMED OPERATIONAL TEST OF THE LANDING GEAR CONTROL PER THE MAINTENANCE MANUAL.  SYSTEM CHECKS GOOD.  (Z)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 16 INCHES CORRODED AREA, RBL 54 SEAT TRACK BS 344-360.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 16 INCHES OF SEAT TRACK CORRODED, BS 344-360 RBL 48 INCHES.  REPAIRED PER SRM53-10-05.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH AREA CORROSION ON SEAT TRACK AT BS 344-360, RBL12 INCHES.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 12 INCHES CORRODED AREA AT HAT CHANNEL, LBL 12, BS 270-282.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
ISP - FLT 1147 - ON TAKEOFF, SEVERAL SMALL BIRDS STRUCK THE LEFT LEADING EDGE AND LEFT ENGINE COWLING.  FLIGHT RETURNEDTO ISP WHERE AN OVERWEIGHT LANDING WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT.  MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION PER MM REF 05-51-201, AND OVERWEIGHT LANDING INSPECTION PER MM REF 05-51-74.  NO DAMAGE FOUND.  (W)


REMARKS:
PIT - FLT 1450 - ON CLIMB-OUT, AIRCRAFT ENCOUNTERED LIGHTNING STRIKE.  FLIGHT RETURNED TO PIT, WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE CHECKED AIRCRAFT PER MM 5-51-151 PG 201-206.  NO DAMAGE FOUND.  (W)


REMARKS:
TPA - FLT 176 - FLIGHT DIVERTED TO TPA DUE TO THE CADC FAILING.  MAINTENANCE SWAPPED THE NR 1 AND NR 2 CADC.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 1296 - DURING CLIMB-OUT THE UTILITY SYSTEM HYDRAULIC QUANTITY WENT TO ZERO, AND THE HYD PUMP LIGHS ILLUMINATED AMBER.  AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED A BAD 0-RING AT THE GEAR GROUND RESTRICTOR.  ALSO, REPLACED BOTH NR 1 AND 2 ENGINE DRIVEN PUMPS PER MM, OPERATION CHECKS NORMAL.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION .75 INCH BY .75 INCH ANCHOR NUT HOLES STA 967-986 RBL 25 L AND R.  REPAIRED PER SRM 52-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  REF 94ZZZW    .


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION .75 INCH BY .75 INCH ANCHOR NUT HOLES STA 967-986 RBL 25 L AND R.  REPAIRED PER SRM 52-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  REF USAA940937.  (W)


REMARKS:
DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 20 INCHES CORROSION AT Z ANGLE AFT SERVICE DOOR, STA 1016-986.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-01.  CORROSION LEVEL 2.  (W)


REMARKS:
TPA - FLT 942 - AFTER TAKEOFF THE FLAPS WOULD NOT RETRACT BEYOND 6 DEGREES.  AIRCRAFT RETURNED THE FLAP DRIVE MOTOR ANDGEAR BOX PER MM 27-51-03.  OPERATION CHECKS NORMAL.  REF USAA940942.  (W)


REMARKS:
CLT - FLT 1993 - DURING FLIGHT, THE RADAR INDICATED NARROW BAND OF RED BOUNDED BY GREEN ARCING ENTIRE RADIUS OF SCREEN. AIRCRAFT RETURNED TO FIELD AND LANDED      WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RADAR RT UNIT.  SYSTEM FUNCTIONAL CHECK NORMAL.  (W)


REMARKS:
IAD - FLT 121 - AFTER TAKEOFF, BOTH PACKS SHOWED OFF-LINE AND AIR PRESSURE WAS ZERO.  RECYCLED ALL PACK AND BLEED SWITCHES, STILL NO AIR.  AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE BACK UP VALVEPER MM.  GROUND AND LEAK CHECK GOOD.  (W)


REMARKS:
CLT - FLT 1086 - THE AFT BULKHEAD WAS NOT SEATED PROPERLY CAUSING AN UNUSUAL NOISE AND PRESSURIZATION PROBLEMS.  THE CREW DECIDED TO RETURN TO FIELD.  MAINTENANCE ADJUSTED THE SEAL ON THE AFT CABIN PRESSURE BULKHEAD.  (W)


REMARKS:
EWR - FLT 71 - UPION GEAR RETRACTION, THE GEAR DOOR LIGHT STAYED ILLUMINATED, AND A EICAS MESSAGE FOR THE GEAR DOOR WASRECEIVED.  THE CREW WAS UNABLE TO RETRACT THE GEAR AND DECIDED TO RETURN TO FIELD.  MAINTENANCE REPLAAAACED THE POWER PACK.  THE GEAR DOOR OPERATION WAS NORMAL.  (W)


REMARKS:
LGW - FLT 199 - ON CLIMB-OUT AT 300 KNOTS, THE LEFT MAIN LANDING GEAR WARNING LIGHT ILLUMINATED.  THE CREW SLOWED TH 270 KNOTS AND THE LIGHT WENT OUT.  RETURNING TO A HIGHER SPEED CAUSED THE WARNING TO REAPPEAR.  AN EICAS LANDING GEAR MONITOR MESSAGE WAS ALSO NOTED.  THE CREW DECIDED TO RETURN TO FIELD.  MAINTENANCE CHECKED THE PROX SENSOR UNIT M162 AND ALLSENSORS PLUS SYSTEM 1 AND 2.  ALL FOUND TO BE SATISFACTORY.  (W)


REMARKS:
CLT - FLT 2376 - AFTER TAKEOFF, THE SLAT DISAGREEMENT LIGHT REMAINED ON AFTER THE SLATS AND FLAPS WERE FULLY RETRACTED. THE SLATS INDICATED FULL UP ON GAUGE AND FELT RETRACTED.  THE SLAT HANDLE RETURNED TO THE SLAT EXTENDED POSITION AND THE LIGHT WENT OUT.  THE CREW DECIDED TO RETURN TO CLT.  MAINTENANCE ADJUSTED THE DOOR AND SLATS.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
FOUND 2.5 INCH FUSELAGE SKIN CRACK BS 867, S24R, AFT OF AFT CARGO DOOR.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND 2 INCH FUSELAGE SKIN CRACK AFT OF RIGHT WING TO BODY FAIRING.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND INBOARD CREASE BEAM CHORD CRACKED AT BS 639, RBL 65, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 16R CRACKED AT BS 500C +4.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND RIGHT WING ILLUMINATION LIGHT SUPPORT STRINGER 16R CRACKED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD INTERCOSTAL CRACKED.  REPAIRED PER SWA RA 1-253-1188.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 25L CORRODED AT BS 366.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND BELTFRAME CRACKED AT BS 360, STRINGER 20R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK,  FOUND WEB CRACKS FROM BS 706 TO 716, RBL 24.5.  REPAIRED PER SWA ACO 658-57.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STABILIZER STRAPS  BELOW FLOOR BEAM CRACKED AT BS 312, RBL 31 AND AT BS 328, RBL 45.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, LBL 6.  REPAIRED PER SWA RA 1-253-1182.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, RBL 8, UNDER FASTENER HOLE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT BS 178, RBL 26, WL 196.  REPAIRED PER SWA RA 1-253-1188.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO COMPARTMENT STRINGER SPLICE CORRODED AT BS 907, S26R.  REPAIRED SPLICE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT BS 178, LBL 26, WL 196.  REPAIRED PER SWA RA 1-253-1189.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND SHEAR TIE CRACKED AT BS 1104, BETWEEN S17 AND 18L INSIDE LEFT TORQUE BOX AREA.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK,  FOUND AFT CARGO FUSELAGE STRINGER SPLICE CORRODED AT FORWARD END BS 907.  REPLACED  PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND NOSE WHEEL WELL UPPER LEFT ACCESS PANEL OPENING CRACKED AT AFT I/B CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE CIRCUMFERENTIAL BELTFRAME SHEAR TIE CORRODED AT BS 277, S27R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW C-D POST SKIN CRACKED.  REPAIRED PER SWA RA 1-353-1186.


REMARKS:
STL - INVESTIGATION OF LEFT ENGINE S/N 2131, POWER LOSS AND SUBSEQUENT SHUTDOWN, REVEALED LPT 4 VANE, MFG P/N 777739, SHIFTED AFT WHICH RUBBED ON LPT 4 BLADES UNTIL LIBERATION.  ENGINE S/N 3231 WAS REPAIRED, TESTED AND RETURNED TO SERVICE.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON FLOOR BEAM UPPER CHORD, STATION 1700, LBL 34 AND 76.  REPAIRED PER SRM 53-10-07, FIGURE 10.  TOTAL CYCLES 14,767.


REMARKS:
MCI - DURING OP-16, FOUND CRACK APPROXIMATELY 1.5 INCH IN FLOOR BEAM CAP, FS 480, LBL 108.  REPAIRED PER SRM 53-10-07.TOTAL CYCLES 14,767.


REMARKS:
MCI - DURING CHECK C-02, FOUND .75 INCH CRACK IN RT INBOARD FLANGE OF REAR SPAR UPPER SPLICE FITTING, RUNNING AFT TOWARD EDGE.  REPAIRED PER SRM 57-10-303 AND SERVICE BULLETIN 747-57-2110.  TOTAL CYCLES 15,865.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION IN CENTER CHANNEL OF STRINGER 44R, FS 2215.  REPLACED STRINGER SECTION PER SRM 53-10-02.  TOTAL CYCLES 14,767.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON STRINGER 39L, FS 736 TO FS 798.  REPAIRED PER SRM 53-00-03 AND STANDARD PRACTICES.  TOTAL CYCLES 11,798.


REMARKS:
MCI - DURING OP-16, FOUND WORN SEAL, WORN AREA APPROXIMATELY 9 INCHES LONG, .030 INCH DEEP, .300 INCH WIDE, BELOW RIGHTSTABILIZER AT MOVABLE SEAL, FS 1788-1797.  REPAIRED PER SRM 53-80-01.  TOTAL CYCLES 11,798.


REMARKS:
SLC - THE LEFT ENGINE, S/N 1208, THAT INCURRED A LOW RUMBLE AND VIBRATION WITH METAL IN THE OIL SCREEN, WAS FOUND TO HAVE NR 3 BEARING FAILURE, MFG P/N 804059.  ENGINE S/N 1208 WAS REPAIRED, BEARING REPLACED, TESTED AND RETURNED TO SERVICE.


REMARKS:
JFK - DURING CHECK C-8C, FOUND TWO .25 INCH CRACKS IN FUSELAGE SKIN BETWEEN STRINGERS 45 AND 46, STATION 983 TO STATION981.  REPAIRED PER LOCKHEED REPAIR SCHEME LCC 7622-48 AND ARA 7286A.  TOTAL CYCLES 22,438.


REMARKS:
JFK - DURING CHECK C-8C, FOUND LONGERON AT FS 983 CRACKED THROUGH.  REMOVED AND REPLACED LONGERON PER SRM 51-10-01, PAGE 2, PARAGRAPH D.  TOTAL CYCLES 22,438.


REMARKS:
JFK - DURING CHECK C-8C, FOUND RING FORMER DAMAGED, STRINGER 46L, STATION 963.  REPAIRED PER SRM 53-12-00, FIGURE 804.TOTAL CYCLES 22,438.


REMARKS:
STL - DURING OP-15, FOUND .5 INCH CRACK IN LONGERON 29L END FITTING, STATION 756.  REPAIRED PER DOUGLAS DWG 5911418 ANDSRM 53-04, FIGURE 42.  TOTAL CYCLES 73,171.


REMARKS:
JFK - DURING CHECK C-8C, FOUND .21875 INCH SKIN CRACK EXTENDING FROM LOWER AFT .3125 INCH FASTENER HOLE, STATION 983 LEFT LONGERON CHORD.  REPAIRED PER ARA 7286A AND LOCKHEED REPAIR SCHEME LCC 7622-48.  TOTAL CYCLES 22,438.


REMARKS:
STL - DURING OP-15, FOUND POPPED RIVET HEAD AND SKIN BULGED AFT OF MLG WHEELWELL, LONGERON 30, STATION 756.  REPAIRED PER SRM 53-04, FIGURE 42, SHEETS 1-7 AND ARA 8040.  TOTAL CYCLES 73,171.


REMARKS:
STL - DURING OP-15, FOUND ONE .25 INCH CRACK IN LONGERON 30L END FITTING, STATION 756.  REPAIRED PER DOUGLAS DWG 5911418 AND SRM 53-04, FIGURE 42.  TOTAL CYCLES 73,171.


REMARKS:
DURING OP-15, FOUND A 1 INCH CRACK IN LONGERON 29R END FITTING, STATION 756.  REPAIRED PER DOUGLAS DWG 5911418 AND SRM 53-04, FIGURE 42.  TOTAL CYCLES 73,171.


REMARKS:
STL - DURING OP-15, FOUND ONE .5 INCH CRACK IN LONGERON 30 R END FITTING, STATION 756.  REPAIRED PER DOUGLAS DWG 5911418 AND SRM 53-04, FIGURE 42.  TOTAL CYCLES 73,171.


REMARKS:
STL - DURING OP-15, FOUND CORROSION ON LONGERON 29R, STATION 667 TO 756.  REPAIRED PER SRM 53-04, FIGURE 42 AND ARA 8038.  TOTAL CYCLES 73,171.


REMARKS:
STL - DURING OP-15, FOUND ONE .75 INCH CRACK IN FORWARD PASSENGER DOOR PAN AT TOP FORWARD CORNER.  REPLACED PAN PER DOUGLAS DWG 5910081.  TOTAL CYCLES 73,171.


REMARKS:
STL - DURING OP-15, FOUND A ONE INCH CRACK IN KEEL BEAM LONGERON 30, STATION 756.  REPAIRED PER SRM 53-04, FIGURE 42, SHEET 1-7.  TOTAL CYCLES 73,171.


REMARKS:
PHL - CENTER, AFT AND FORWARD AISLE EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACKS AND CHARGER.  REFERENCE USAA940977.


REMARKS:
CLT - 8 INCHES BY .5 INCH CORROSION AT STATION 325 RBR 40 - RBR 48.  INSTALLED DOUBLER, CORROSION REMOVED, AREA ALODINED AND PRIMED.  DOUBLER DUCT INSTALLED WET, PER EA 37836 SRM 53-00-51, SRM 53-10-91.  (Z)


REMARKS:
PHL - LOW LEVEL EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLAMPED AND REPAIRED WIRING.  (Z)


REMARKS:
GSO - EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED CENTER OVERHEAD BATTERY CHARGER.  (Z)


REMARKS:
PHL - CENTER, AFT AND FORWARD AISLE EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACKS AND CHARGER.  REFERENCE 94ZZZZ1922.


REMARKS:
CLT - FLT 1175 - RETURN TO FIELD DUE TO AIRCRAFT SYSTEM PRESSURE NOT ABLE TO PRESSURIZE.  MAINTENANCE REPLACED THE OUTFLOW VALVE.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND LEVEL I CORROSION (PIEV REWORKED) ON FLOOR SUPPORT UNDER GALLEY MOUNT PLATE AT STATION 160, 12 INCHES RIGHT OF CENTER LINE.  CORROSION WAS CLEANED AND REPAIR DOUBLER INSTALLED AS PER USAIR TYPICAL REPAIR 53-10-14.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .5 INCH CRACK IN ATTACH ANGLE FOR LEFT PYLON STATION 984 LONGERON 14 LEFT.  INSTALLED REPAIR DOUBLER AS PER SRM 53-04 FIG 10.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND 5 AREAS THAT HAD PREVIOUSLY BEEN TRIMMED OUT WITHIN 8 INCHES OF SKIN AT FORWARD EDGE OF GALLEY SERVICE DOOR FRAME.  REPAIR DOUBLER WAS INSTALLED AS PER SRM 53-05 FIG 82.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .375 INCH CRACK IN SKIN AT MAIN ENTRANCE DOOR TOP AFT STOP ADJUSTMENT CUTOUT.  DOUBLER REPAIR WAS INSTALLED AS PER SRM 53-05 FIG 26A.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND LEVEL I CORROSION (PREVIOUS REWORK) STATION 232-240 RT INBOARD SEAT TRACK (TASK NR 046-53305).  CUT OUT SECTION AND SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4D.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND LONGERON CRACKED AT BOTH ATTACH FLANGES AT BELTFRAME STATION 639 LONGERON 3L.SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND LONGERON CRACKED AT BOTH ATTACH FLANGES AT BELT FRAME STATION 718 AND 699 LONGERON 3L.  SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .875 INCH CRACK RT DORSAL FIN ATTACH ANGLE TRAILING EDGE.  SPLICED IN NEW SECTION OF ATTACH ANGLE PER SRM 53-05 FIG 23A.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 6 INCHES LONG DENT/SCRATCH OUT OF SRM LIMITS AT STATION 275 BETWEEN LONGERON 19R AND 20R IN THE SKIN.  INSTALLED FLUSH DOUBLER REPAIR 6.5 IINCHES BY .75 INCH PER USAIR TYPICAL REPAIR 53-30-08.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 17L STATION 965.  SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LEFT FWD EMERGENCY EXIT WINDOW PAN, CRACKED AT TOP AFT FITTING.  INSTALLED DOUBLER PER USAIR TYPICAL REPAIR 52-20-03.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT SKIN CLIP STATION 945 RT BETWEEN LONGERON 14R AND 15R.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 3.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .75 INCH CRACK IN THE UPPER LEFT PYLON ATTACH ANGLE AT STATION 945 LONGERON 15L.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 10.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND 1 INCH CRACK IN BELTFRAME STA 180, LONGERON 4 AND 5.  REPAIR DOUBLER WAS INSTALLED AS PERSRM 53-03 FIG 36.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .5 INCH CRACK IN RIB NR 4 AT RIGHT HORIZONTAL STABILIZER (INTERNAL).  REPAIR DOUBLER WAS INSTALLED AS PER SRM 55-02 FIG 18.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .25 INCH CRACK IN PAN FOR LEFT FWD EMERGENCY EXIT WINDOW TOP AFT DOOR STOP.  REPAIR DOUBLER WAS INSTALLED AS PER TYPICAL REPAIR 52-20-03.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .25 INCH CRACK IN LONGERON 14R STA 1069.  NEW SECTION OF LONGERON WAS SPLICED IN AS PER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND CLASS III REPAIR ON LONGERON 22L STA 162-170.  INSTALLED CLASS I REPAIR EXTERNAL DOUBLER AS PER DACO SR 09530219-7001.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .875 CRACK ON LONGERON 24 RIGHT AT STA 200.  SPLICED IN NEW SETION OF LONGERON AS PER USAIR TYPICAL REPAIR 53-10-17.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND 1 INCH CRACK IN LONGERON 23 LEFT STA 200.  NEW SECTION OF LONGERON WAS SPLICED IN AS PER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND 1 INCH CRACK IN SKIN LOWER AFT CORNER OF FWD SERVICE DOOR STA 200.  REPAIR DOUBLER WAS INSTALLED AS PER SRM 53-05 FIG 35.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND 2 EA CRACKS .375 INCH IN SKIN AT STA 69, LONGERON 2 PLUS 3 RIGHT.  FLUSH DOUBLER REPAIR WAS INSTALLED AS PER DACO SRO9530239 AND EA 27503.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND LEVEL I CORROSION (PREV REWORK) ON RT O/B SEAT TRACK STA 225-294.  NEW SECTION OF SEAT TRACK WAS SPLICED IN AS PER SRM 53-05 FIG 4F.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND LEVEL I CORROSION (PREV REWORK) ON FLOOR SUPPORT STA 980 LEFT LAV.  REPAIR DOUBLER WAS INSTALLED AS PER USAIR TYPICAL REPAIR 53-10-19.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND LEVEL I CORROSION (PREV REWORK) ON FLOOR SUPPORT FOR LEFT LAV, STA 980.  REPAIR DOUBLER WAS INSTALLED AS PER USAIR TYPICAL REPAIR 53-10-19.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND CLASS III REPAIR AT TOP FUSELAGE ADF LOOP ANTENNA.  DOUBLER REPAIR WAS INSTALLED AS PER DACO SR 09530005.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .25 INCH CRACK IN SKIN AT STA 503 LONGERON 3 AND 4 LEFT.  REPAIR DOUBLER INSTALLED AS PERSRM 53-04 FIG 12B CLASS I.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND TEMPORARY REPAIR TO SKIN ON BOTTOM AREA OF EXTERNAL POWER DOOR.  REPAIR DOUBLER WAS INSTALLED AS PER SRM 53-04 FIG 48.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, FOUND .125 INCH CRACK IN SKIN AT MAIN ENTRANCE DOOR HOLD OPEN LATCH CUTOUT, FWD EDGE.  REPAIR DOUBLER WAS INSTALLED AS PER SRM 53-04 FIG 24 AND EA 27504.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND DENTS/SCRATCHES .011-.025-.018 AND .020 DEEP LT SIDE OF FUSELAGE SKIN FROM STA207-237, LONGERON 21L.  INSTALLED FLUSH DOUBLER REPAIR 32.5 INCHES BY 4 INCHES PER USAIR EA 27781.  (W)


REMARKS:
DEN - FLT 870 - INVESTIGATION OF ENGINE SN 3230 STALL AND POWER LOSS REVEALED HPT BLADE, MFG PN 5002201-1, AIRFOIL FAILED AT OUTER END.  SENT FAILED BLADE TO PRATT AND WHITNEY FOR LABORATORY ANALYSIS.  ENGINE SN 3230 REPAIRED AND RETURNED TO SERVICE.


REMARKS:
CLT - FLT 1752 - WHILE ON APPROACH TO CLT AT APPROXIMATELY 2000 FEET, ENGINE NR 2 OIL PRESSURE WENT TO ZERO.  THE CAPTAIN SHUTDOWN THE ENGINE AND DECLARED AND EMERGENCY.  THE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE, FOR LOW OIL PRESSURE.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
GRR - FLT 862 - UPON LANDING, THE BRAKES WERE APPLIED, BUT DID NOT WORK.  THE BRAKES CAUGHT WHEN THE AIRCRAFT WAS ALMOST STOPPED.  MAINTENANCE FOUND PINS BROKEN IN THE ANTI-SKID BOX.  THEY REPLACED THE ANTI-SKID CONTROL BOX.  SYSTEM BYTE TESTED NORMAL.  (W)


REMARKS:
TPA - FLT 942 - AFTER TAKEOFF THE FLAPS WOULD NOT RETRACT BEYOND 6 DEGREES.  AIRCRAFT RETURNED THE FLAP DRIVE MOTOR ANDGEAR BOX PER MM 27-51-03.  OPERATION CHECKS NORMAL.  REF 94ZZZW3154.


REMARKS:
EVV - FLT 480 - AFTER TAKEOFF, THE FIRST OFFICERS FWD WINDSHIELD SHATTERED IN THE LOWER RT CORNER.  AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE F/O WINDSHIELD PER MM 56-10-06, ALL CHECKS NORMAL.  (W)


REMARKS:
ABE - MADE UNSCHEDULED LANDING ACCOUNT DURING CRUISE THE RIGHT ENGINE THROTTLE DID NOT RESPOND TO POWER REDUCTION.  SHUT DOWN ENGINE.  FOUND BOLT, MFG P/N NAS1204-18D, DISENGAGED FROM THROTTLE PUSH-PULL CABLE AT ENGINE CROSS-SHAFT.  REPLACED BOLT, NUT AND COTTER PIN.  OP CHECKS NORMAL.  CHECK C-1D - 1-13-94 - MCI.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 27L CORRODED AT BS 487 AND STRINGER 28R AT BS 470.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 987, WL 208 FROM RBL 26 TO 29.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 727D AT STRINGER 24L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND NUMEROUS FUSELAGE SKIN DENTS FROM BS 847 TO 877, STRINGER 18 TO 20 R.  REPAIRED PER TRAMCO EWO 94-0885.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND TEMP REPAIR AT BS 178 BULKHEAD.  PERFORMED PERMANENT REPAIR PER TRAMCO EWO 94-0887 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, AT STRINGER 26L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM UNDERSIDE CRACKED AT ATTACH POINT, BS 460, RBL 14.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND SIDEWALL ANGLE CRACKED AT BS 380 AT STRINGER 20R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK,  FOUND AFT ENTRY DOOR AFT FRAME CRACKED AT LOWER HINGE ARM CUTOUT.  REPAIRED PER SWA RA 1-252-201.


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK LONGERON 9L STATION 1089.  SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-02 FIG 2.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .5 INCH CRACK AT CANTED BELT FRAME ATTACH ANGLE BETWEEN LONGERON 17R AND 18R AT STATION 1121.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 27-503.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND PREVIOUS REPAIR CLASS III (TEMPORARY) RT SIDE OF NOSE SKIN STATION 110 TO STATION 135.5 BETWEEN LONGERON 18R-21R.  SPLICED IN NEW SECTION OF SKIN 28 INCHES BY 17 INCHES PER USAIR EA 27737.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK IN FRAME STATION 1074 LONGERON 6L.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 30, SHT4-7017.  (Z)


REMARKS:
AT EWR WHILE PARKED ON HARDSTAND, AIRCRAFT WAS STRUCK AT NR 2 ENG REVERSER BY RIGHT WING OF WESTLAKES CONVAIR A/C N32KABEING TOWED BEHIND KIWI AIRCRAFT.  NR 2 ENGINE REVERSER WAS DAMAGED.  REMOVED AND REPLACED NR 2 ENGINE REVERSER, OPS CHECK PER 78-30-0.  (Z)


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB SHEAR TIE AT BELT FRAME CRACKED AT BS 294, STRINGER 12L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB DAMAGE AT AFT CARGO DOOR, FORWARD LOWER CORNER OF DOOR FRAME OPENING.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK,  OUND STRINGER TIE CLIPS CRACKED AT I/B END, AT BS 380 AND S22L AND AT S21L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LEFT HORIZONTAL STAB CENTER SECTION REAR SPAR LOWER AFT LUG GOUGED ON BOTTOM SURFACE AT BS 1156.  REPAIRED PER TRAMCO EWO 94-0900.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 265, BELOW S16L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CORROSION FROM BS 1006 TO 1016, LBL 10, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR INSPECTION OF FUSELAGE SKIN LAPS, FOUND FUSELAGE SKIN CRACKS AT BS 700 AT S4R, BS 827 AT S4 AND S10R, BS 747 AT S4R, BS 767 AT S4R, BS 896 AT S10R, BS 866 AT S10R, BS 480 AT S4 AND S10R, BS 742 AT S10R, BS 744 AT S10R, BS 640 AT S4R, BS 627 AT S4R, BS 877 AT S4R, BS 500B+10 AT S4R, BS 500A+10 AT S4R AND L, BS 490 AT S4R, BS 489 AT S4R, BS 489 AT S4R, BS 410 AT S4R, BS 846 AT S14L, BS 727A+10 AT S14L, BS 651.5 AND 652.5 AT S4L, BS 294 AT S24L, BS 295 AT 24L, BS 294 AT 24L, BS 296 AT S24L, AND BS 351 AT S19R.  REPAIRED PER TRAMCO EWO'S 94-0922 AND 94-0931.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR INSPECTION OF FUSELAGE SKIN LAPS, FOUND FUSELAGE SKIN CRACKS AT BS 627 AT S4L, BS 578.5 AT S4L, BS 588 AT S4L, BS 596.5 AT S4L, BS 292 AT S19R, BS 276 AT S19R, BS 480.5 AT S4L, BS 887 AT 14R, BS 766.5 AT S4L, BS 767.5, S4L, BS 458 AT S14R, BS 440 AT S14R, BS 695 AT S4L AND BS 380 AT 14R.  REPAIRED PER TRAMCO EWO'S 94-0922 AND 94-0931.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR INSPECTION OF FUSELAGE SKIN LAPS, FOUND SHEAR TIE CRACKED AT BS 294.5 AT S24L, 5 INCHES BELOW S24L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND T ANGLE CRACKED AT BS 178, LBL 6.  REPAIRED PER SWA RA 1-253-1184.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WING INBOARD AUX TRACK CUTOUT CRACKED INBOARD OF NUMBER 1 SLAT.  REPAIRED PER SWA RA 1-257-255.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND SHEAR TIE WEB CRACKED FORWARD INBOARD CORNER AT BS 294 ,S8L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND STABILIZATION STRAP CRACKED AT FWD I/B FASTENER OF REPAIR DOUBLER, BS 344 AND LBL 45.5.  REPAIRED PER SWA RA 1-A53-1157.


REMARKS:
DURING SHOP SLIDE TEST, THE TOP OF THE REGULATOR ON BOTTLE CAME OFF.  SLIDE DEPLOYED NORMALLY.  MAINTENANCE RETURNED BOTTLE TO VENDOR FOR FURTHER ANALYSIS.  (Z)


REMARKS:
PHL - FLT 244 - PRIOR TO DEPARTURE, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK FOR COCKPIT.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
PIT - FLT NR 378 - CREW RECEIVEDHYD SYSTEM 2 LOW QUANTITY MESSAGE.  QUANTITY DROPPED TO 14 PERCENT THEN ROSE TO 34 PERCENT WHEN PUMPS TURNED OFF.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND NR 2 RUDDER ACTUATOR CONTROL VALVE SIGHT GAUGE LEAKING.  REMOVED AND REPLACED SIGHT GAUGE O-RING.  LEAK CHECKED OK.  (Z)


REMARKS:
PIT - FLT 324 - DURING FLIGHT, THE RT MLG DOOR LOCK SWITCH MESSAGE APPEARED ON MULTI FUNCTION DISPLAY UNIT.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 1 SENSOR.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 3 INCH AREA OF SURFACE CORROSION, STATION 992.T AT WL 207 TO WL 210 MAIN FRAME.  REPAIRED PER SRM 51-70-11.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND KEEL BEAM WITH 1 INCH WIDE, 2 INCH LONG LEVEL 2 CORROSION S-27 R AFT OFSTATION 520.  REPAIRED PER EA 37923.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND STRINGER 2 INCHES LONG, 2 INCHES WIDE LEVEL 2 CORROSION S-26 R STATION 500D.  REPAIRED PER SRM 53-30-3.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 6 INCH BY 2 INCH AREA OF SURFACE CORROSION FORWARD SERVICE ENTRY Z-ANGE AT APPROXIMATELY STATION 300.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 15 INCHES BY 2 INCHES OF SURFACE CORROSION FORWARD ENTRY Z-ANGLE STATION 312 TO STATION 332.  REPAIRED PER SRM 51-70-11.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND AN ANGLE WITH 1 INCH BY 1.5 INCH CORRODED AREA BS 1013.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CARGO TRACK WITH 13 INCH BY 1 INCH CORRODED AREA RBL 13.80 BS 787 TO 847.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSEPCTION, FOUND APPROXIMATELY .5 INCH BY 3 INCH AREA OF CORROSION CARGO FLOOR BEAM AT BS 772 AT RBL 7.5.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY .5 INCH BY 3 INCH AREA SURFACE CORRODED.  CARGO FLOOR BEAM AT BS 772 LBL 7.5.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
PIT - DURING Q-4 CHECK, FOUND 12 INCH CRACK IN HORIZONTAL PANEL STATION 101.550 LEFT SIDE FLIGHT COMPARTMENT.  SPLICED IN NEW SECTION AS PER DACO SKETCH 94-08-23-008 AND EA 27364.  (Z)


REMARKS:
AFTER TAKEOFF, NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH.  CYCLED NOSE GEAR, NO HELP.  AIRCRAFT RETURNED TO LAS AND MADEAN UNEVENTFUL LANDING.  AIRCRAFT MAINTENANCE FERRIED TO PHX.  REPLACED NOSE GEAR UPLOCK ACTUATOR AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
AFTER TAKEOFF AND FLAPS RETRACTED, NUMBER 3 L/E SLAT TRANSIT LIGHT REMAINED ILLUMINATED.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 3 SLAT ACTUATOR PER BOEING M/M.


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 30 INCH OF HEAVY SURFACE CORROSION AFT ENTRANCEDOOR SILL Z-ANGLE AT STATION 960 TO 986.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
PIT - FLT 1821 - DURING FLIGHT, HEARD AND FELT VIBRATION DOWN LEFT SIDE OF THE AIRCRAFT.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE CHECKED AIRCRAFT EXTERIOR, RAN ENGINES, AND TAXIED.  ALL CHECKS GOOD.  FOUND RADAR ANTENNA SHUDDERS CAUSING AIRFRAME TO VIBRATE.  REPLACED RADAR ANTENNA.  AIRCRAFT AIRWORTHY FOR SERVICE.  (W)


REMARKS:
GSO - FLT 2151 - WITH TAKEOFF POWER SET, CREW HEARD A LOUD THUMP SOUND.  AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REINSTALLED AIR CONDITIONING DUCT.  PRESSURIZED AIRCRAFT, ALL CHECKS NORMAL.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND PREVIOUS REPAIR TO MAIN ENTRANCE DOOR UPPER CORNER STA 160.  OLD REPAIR REMOVED.  CRACK WAS CUT OUT AND FILLER PLUS EXTERNAL OVERLAPPING DOUBLER INSTALLED PER SRM 53-05, FIGURE 26 (X)


REMARKS:
PIT - DURING Q-4 CHECK, FOUND PREVIOUS REPAIR TO E & E COMPARTMENT DOOR.  REMOVED OLD REPAIR AND INSTALLED FINGER DOUBLER AND LAYERED EXTERNAL DOUBLERS PER E. A. 27789.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND .75 INCH CRACK AT STA 579, LT FLOOR SUPPORT.  REPAIR ANGLES INSTALLED PER SRM 53-01, FIGURE 2.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND 1 INCH CRACK AT STA 598 RT FLOOR SUPPORT.  REPAIR ANGLES WERE INSTALLED PER SRM 53-01, FIGURE 2.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND 1 INCH CRACK AT STA 522, LT FLOOR SUPPORT.  REPAIR ANGLE WAS INSTALLED PER SRM 53-01, FIGURE 2.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND 1 INCH CRACK AT STA 522 LT FLOOR SUPPORT.  REPAIR ANGLES WERE INSTALLED PER SRM 53-01, FIGURE 2.  (X)


REMARKS:
PIT  DURING Q4 CHECK, FOUND .8750 INCH CRACK AT STA 541, LT FLOOR SUPPORT.  REPAIR ANGLES WERE INSTALLED PER SRM 53-01,FIGURE 2.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND 1 INCH CRACK AT STA 560, LT FLOOR SUPPORT.  REPAIR ANGLES WERE INSTALLED PER SRM 53-01, FIGURE 2. (X)


REMARKS:
PIT - DURNG Q4 CHECK FOUND .8750 INCH CRACK ON FRAME AT STA 446 ABOVE LONGERON 30.  CRACK WAS STOP DRILLED AND DOUBLER INSTALLED PER SRM 53-03, FIGURE 2A.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND .3750 INCH CRACK IN SKIN AT STA 200 BETWEEN LONGERON 4 AND LONGERON 5 LEFT.  CUT OUT CRACKAND INSTALLED FILLER PLUF AND INTERNAL FINGER DOUBLER PER SRM 53-04, FIGURE 38.  (X)


REMARKS:
PIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK IN LT WING SKIN LEADING EDGE AT XRS-98.  CRACK WAS STOP DRILLED AND DOUBLER INSTALLED PER EA 27643.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND 2 INCH CRACK IN WEB ON RIGHT FLIGHT COMPARTMENT HORIZONTAL PRESSURE PANEL FS 101.550.  CRACK WAS CUT OUT.  FILLER AND FINGER DOUBLER WERE INSTALLED PER EA 27602.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND 1.6250 INCH CRACK IN WEB BETWEEN STA 218 AND STA 237 RT CUSP LINE.  REPLACED WEB BETWEEN STA 218 AND STA 237 PER SRM 53-05, FIGURE 97.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND LEVEL I CORROSION (PREVIOUS REWORK) ON RT OUTBOARD SEAT TRACK BETWEEN STA 237 AND STA 256. SPLICED IN NEW SECTION OF SEAT TRACK FROM STA 237 TO STA 256 PER SRM 53-05, FIGURE 4.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND LEVEL I CORROSION (PREVIOUS REWORK) ON LT LAV FLOOR BEAM ST STA 980.  REMOVED CORROSION AND INSTALLED ANGLE REPAIR STRAP PER TYPICAL REPAIR 53-01-19.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND LEVEL I CORROSION (PREVIOUS REOWORK) ON LT LAV FLOOR BEAM AT STA 996.  TOP OF FLOOR BEAM REMOVED AND NOW TOP ANGLE INSTALLED PER SRM 53-11-3, AND TYPICAL REPAIR 53-10-19.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND LEVEL I CORROSION (PREVIOUSLY REWORKED) ON THRESHOLD PANEL IN LT LAV AT STA 965 AND STA 966.  THRESHOLD PANEL WAS REPLACED PER MM.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND LEVEL I CORROSION (PREVIOUS REWORK) ON RT INBOARD SEAT TRACK AT STA 256 AND STA 275.  NEW SEAT TRACK WAS SPLICED IN BETWEEN STA 256 AND STA 275 PER SRM 53-05, FIGURE 4F.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND LEVEL I CORROSION (PREVIOUS REWORK) ON STR NR 21 IN RT WING FUEL TANK.  REPLACED STR NR 21AND SPLICED WITH REPAIR ANGLES PER SRM 57-08, FIGURE 1, PAGE 5.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND .50 INCH CRACK IN LONGERON 3 LT AT STA 160.  SPLICED IN NEW SECTION OF LONGERON PER TYPICAL REPAIR 53-10-17.  (X)


REMARKS:
PIT - DURING Q4 CHECK, FOUND .050 GAUGE IN SKIN AT STA 215 LONGERON 5 LEFT.  DAMAGED AREA REMOVED.  INSTALLED FILLER, DOUBLER, AND FINGER DOUBLER PER SRM 53-04, FIGURE 38.  (X)


REMARKS:
PIT - ONE SECTION OF LOW LEVEL EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPAIRED BROKEN WIRE TO FLOOR EMERGENCY LIGHTS.  (X)


REMARKS:
CMH - FLT 1731 - DURING FLIGHT, THE NR 2 EMUX EXPERIENCED A SINGLE CHANNEL FAILURE.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 EMUX.  OPERATION CHECKS GOOD PER MM 77-41-01.  (W)


REMARKS:
PIT - FLT 441 - ON GEAR RETRACTION THE NOSE GEAR DID NOT RETRACT.  NO CORRECTION. AIRCRAFT RETURNED TO FIELD AND LANDEDWITHOUT INCIDENT.  MAINTENANCE REPLACED THE NLG DOOR CYLINDER PER MM 32-32-16.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
CLT - FLT 1232 - PRIOR TO DEPARTURE, THE FLOOR EMERGENCY LIGHTING BY ROW 3 AND 4 WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED POWER AND LIGHT STRIP.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
MBS - FLT 683 - THE NR 1 ENGINE SHUTDOWN AFTER TAKEOFF DUE TO OIL OVERTEMP WARNING, HIGH TGT WARNING AND VARIOUS OTHER WARNINGS ON MFDU.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND ADHESIVE TAPE IN FIREWALL CONNECTOR J-304-D.  REMOVED TAPE,RESECURED CONNECTOR,AND RAN ENGINE.  ENGINE OPERATION NORMAL, ALL PARAMETERS NORMAL.  (W)


REMARKS:
BOS - FLT 2166 - PRIOR TO DEPARTURE, THE SERVICE DOOR SLIDE PARTIALLY OPENED.  MAINTENANCE REPLACED SERVICE DOOR ESCAPESLIDE.  ALL CHECKS NORMAL.  (W)


REMARKS:
CLT - FLT 346 - DURING CLIMB-OUT, THE ESS FAULTED AND THE STALL WARNING COMPUTER ALERTED.  AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE RESET CIRCUIT BREAKER, PEFORMED BITE GPCU WITH NO FAULTS FOUND.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 27L CORRODED AT BS 487.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND TWO SECTIONS OF CABIN  FLOOR EMERGENCY ESCAPE PATH LIGHTING INOP.  REPAIRED BROKEN WIRES PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN OVERHEAD EXIT SIGN INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


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


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LOWER STOP AREA UNDER LATCH SUPPORT.  REPAIRED PERSWA ACO 3194-52.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND FLOOR STRAP CRACKED UNDER FLOOR BEAM AT BS 312, RBL 30.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND CRACK IN AFT END OF STRINGER 15R TO BELTFRAME INBOARD CHORD ANGLE, BS 619.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND CRACK IN VERTICAL WEB, BS 713-714, LBL 24.75, MAIN WHEEL WELL PRESSURE DECK.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND SHEAR TIE CRACK AT FWD FASTENERS AT LBL 26, AFT OF BS 178, WL 195.2.  REPAIRED PER SWA RA 1-253-1163.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND GOUGE IN BELTFRAME FROM NUTPLATE CHAFING, AT RIGHT TORQUE BOX, S16R.  REPAIRED PER SWA RA 1-253-1170.


REMARKS:
DURING SCHEDULED D CHECK, FOUND CHORD CRACKED AT BS 1156, WL 280, LBL 22.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND TEAR STRAP SUPPORT WEB CORRODED AT AFT CARGO BAY AT BS 787-794, RBL 19.5, WL 158.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER 16L UPPER STIFFENER FLANGE DENTED AND CRACKED AT BS 895.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND MOPSILL CORROSION FROM BS 312 TO 350, WL 208, LBL 55.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND CHORD NUTPLATE HOLE CORROSION AT BS 986.5, LBL 2 TO 45, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 294.5, WL 208, RBL 8 AND 12.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, WL 208, RBL 42.5 TO 49.5 AND LBL 49 ON LOWER SIDE OF CHORD.  REPLACED PER SWA RA 1-353-424.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 759, S7L, LBL 59, WL 277.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 894, BETWEEN STRINGERS 19 AND 20L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND KEEL BEAM LOWER O/B FLANGE CORRODED FROM BS 500D TO 520, S28L.  REPAIRED PER TRAMCO EWO 94-0881 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 1088 BULKHEAD 2 PLACES, FWD SIDE AT BL 9.75 AND ATAFT SIDE AT RBL 11.5.  REPAIRED PER TRAMCO EWO 94-0880.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES CRACKED AT BS 908, S4L AND AT 4R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 898, BETWEEN S26L AND R.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CORRODED AT BS 500, STRINGER 28L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT ENTRY DOOR UPPER FRAME CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
STL - DURING OP-15, FOUND A 4 INCH CRACK IN FLOOR BEAM, STA 680 LEFT SIDE.  REPAIRED PER SRM 53-01 PG 1.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FWD CARGO DOOR BEAM, THIRD DOWN FROM TOP OF DOOR.  REMOVED CORROSION AND INSTALLED REPAIR PER ARA 8480A.  TOTAL CYCLES 11,798.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR SUPPORT BEAM UPPER FLANGE, STA 287 RBL 14.  REPAIRED PER SRM 53-00-51 FIG 201 AND ARA 8483.  TOTAL CYCLES 11,798.


REMARKS:
STL - DURING OP-15, FOUND .75 INCH LONG CRACK IN FLOOR BEAM VERTICAL SUPPORT, STA 680 LT O/B SUPPORT.  REPAIRED PER SRM53-01 PG 1.


REMARKS:
STL - DURING CHECK C, FOUND A 2 INCH CRACK IN SKIN, STA 916, LONGERON 2R.  REPAIRED PER DOUGLAS DRAWINGS 4918093 AND 9911840.


REMARKS:
MCI - DURING OP-16, FOUND A 1 INCH CRACK IN FWD CARGO STA 486, STRINGER 34L, LOWER I/B CORNER OF HAT SECTION.  REPAIREDPER SRM 53-00-03 FIG 202.  TOTAL CYCLES 11,798.


REMARKS:
JFK - DURING CHECK C, FOUND CRACK ON O/B RIB OF NR 1 LEADING EDGE SLAT.  REPAIRED PER SRM 51-10-01 PG 2.  TOTAL CYCLES 20,224.


REMARKS:
STL - DURING OP-15, FOUND .0312 INCH CRACK IN COUNTERSINK OF RIVET HOLE IN FUSELAGE SKIN, STA 996, BETWEEN LONGERONS 9RAND 10R.  REPAIRED PER DOUGLAS DWG J060138.


REMARKS:
STL - DURING OP-15, FOUND .0625 INCH CRACK IN FUSELAGE SKIN BETWEEN TWO RIVETS, STA 996, BETWEEN LONGERONS 8R AND 9R.  REPAIRED PER DOUGLAS DWG J060138.


REMARKS:
STL - DURING OP-15, FOUND .0312 INCH CRACK IN COUNTERSINK OF RIVET HOLE IN FUSELAGE SKIN, STA 996, AT LONGERON 4R.  REPAIRED PER DOUGLAS DWG J060138.


REMARKS:
STL - FLT 649 - DURING CRUISE, RIGHT ENGINE SPOOLED DOWN ON OWN ACCORD.  FOUND ENGINE FUEL PUMP SHAFT SHEARED.  REPLACED PUMP, MFG (P/N 378201-7), AND PRECAUTIONARY REPLACED JFC.  OPS CHECKS NORMAL.  CHECK C - 6-24-94 - STL.


REMARKS:
LGA - FLT 274 - PRIOR TO LANDIND, THE R1 DOOR SLIDE PARTIALLY DEPLOYED AS THE RESULT OF A FOOD SERVICE CART BECOMING ENTANGLED WITH THE ACTIVATION LANYARD.  THE SLIDE WAS DEFLATED WITH DAMAGE TO THE SLIDE PACK AND DOOR COVERING.  THE SLIDE, MFG (P/N BFG-7A1274-8), (S/N 8088), WAS REPLACED AND COVERINGS REPAIRED.  CHECK C -1D - 1-13-94 - MCI.


REMARKS:
SEA - FLT 30 - RETURNED FROM FLIGHT ACCOUNT RIGHT ENGINE INCURRED STALLS.  RETARDED THROTTLE.  FOUND METAL IN PNEUMATICDUCT END CAP.  REPLACED ENGINE TWA (S/N 1422), MFG (S/N 725487).  CHECK C - 1-13-94.


REMARKS:
PIT - DURING Q4 CHECK, FOUND .008 INCH CHAFED SKIN IN PYLON LEADING EDGE AT STA 945, LONGERON 15 AND LONGERON 16 LEFT.CHAFED AREA WAS BLENDED OUT AND INTERNAL FINGER DOUBLER INSTALLED PER SRM 53-04.  (X)


REMARKS:
TLH - FLT 1141 - THE LT ENGINE FAILED ON DESCENT THROUGH 24,000 FEET.  RELIGHT WORKED, BUT WOULD NOT MAINTAIN IDLE.  SHUT DOWN CHECK LIST ACCOMPLISHED.  AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT INCIDENT.  MAINTENANCE REPLACED LT ENGINE FUEL REGULATOR AND HIGH PRESSURE PUMP.  ALL PARAMETERS NORMAL PER MM.  NO LEAKS NOTED.  REFERENCE CONTROL NR USAA940953.  (X)


REMARKS:
TLH - FLT 1141 - THE LT ENGINE FAILED ON DESCENT THROUGH 24,000 FEET.  RELIGHT WORKED, BUT WOULD NOT MAINTAIN IDLE.  SHUT DOWN CHECK LIST ACCOMPLISHED.  AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT INCIDENT.  MAINTENANCE REPLACED LT ENGINE FUEL REGULATOR AND HIGH PRESSURE PUMP.  ALL PARAMETERS NORMAL PER MM.  NO LEAKS NOTED.  REFERENCE CONTROL NR 94ZZZX6711.  (X)


REMARKS:
DURING SCHEDULED HALF D CHECK, FOUND T ANGLE CRACKED AT BS 178, RBL 6.  REPAIRED PER SWA RA 1-253-1184.


REMARKS:
AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT.  AIRCRAFT DIVERTED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACEDNOSE GEAR UPLOCK ACTUATOR HYDRAULIC LINE AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM STABILIZATION STRAPS CRACKED AT BS 330, LBL 48  AND AT BS 314, RBL 31.6.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM ANGLE CRACKED AT BS 320, BBL 0.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D CHECK, FOUND FLOOR BEAM CRACKED AT LANYARD ATTACH RADIUS, BS 790, RT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500B, S24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR TO SIDEWALL SUPPORT CORRODED FROM BS 767 TO 794.5, WL 165, RBL 22.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED AT BS 794, LBL 17, WL 156.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1019 TO 1031, WL 223 TO 238, S11 TO 13L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FORWARD AND AFT EDGES OF AIR INTAKE CUTOUT CORRODED FROM BS 1112 TO 1122.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
IN FLIGHT, NUMBER 2 ENGINE OVERHEAT LIGHT ILLUMINATED,  THEN FLICKERED, AND THEN REMAINED ON.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST AND EXPENDED FIRE BOTTLES.  AIRCRAFT LANDED WITHOUT INCIDENT AT SEA.  INSPECTED AND FOUND NO EVIDENCE OF FIRE.  REPLACED FIRE BOTTLES AND SQUIBS PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 1006, RBL 9.25, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 25R BENT AND CRACKED AT BS 390.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
PIT - DURING Q4 CHECK, FOUND PREVIOUSLY INSTALLED REPAIR AT STA 1087, LONERON 2 AND 3 LEFT ON SKIN.  OLD REPAIR WAS REMOVED AND DAMAGED AREA CUT OUT (GOUGE 1 INCH BY 1 INCH) WITH FILLER AND DOUBLER INSTALLED AS PER SRM 53-04 FIG 38.  (W)


REMARKS:
LAX - FLT 2135 - ON TAKEOFF, LOUD NOISE AROUND FORWARD ENTRY DOOR.  FLIGHT RETURNED TO LAX WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED TORN SEAL ON L1 DOOR.  (W)


REMARKS:
RIC - FLT 1762 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF.  FLIGHT RETURNED TO RIC WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE RESET PRESSURE CONTROL CIRCUIT BREAKERS.  (W)


REMARKS:
DFW - FLT 1085 - EN ROUTE RT WING BODY OVERHEAT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH.  CREW DECLARED AN EMERGENCYAND DIVERTED TO DFW WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FERRIED FLIGHT TO CLT WHERE RT STRUT CAVITY LEADING EDGE OVERHEAT DETECTOR WAS REPLACED.  (W)


REMARKS:
PHL - FLT 1766 - SHORTLY AFTER TAKEOFF, RT PACK TRIPPED FOLLOWED BY SMOKE AND FUMES IN CABIN AND COCKPIT.  FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED RT ACM.  OPS CHECK OF RT PACK CHECKS NORMAL.  NO FUMES OF SMOKE NOTED IN CABIN.  (W)


REMARKS:
PIT - FLT 2238 - ON CLIMB-OUT OF LGA, OFF SCHEDULE DESCENT LIGHT ILLUMINATED.  UNABLE TO CONTROL PRESSURIZATION.  FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED DELTA P MODULE.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.75 INCH BY 8.5 INCHES OF CORROSION AFT OF BS 380 LEFT SIDE.  REPAIREDPER SRM 51-10-02 PAGE 15.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
IN FLIGHT, NUMBER 2 ENGINE OVERHEAT LIGHT ILLUMINATED, THEN FLICKERED, AND THEN REMAINED ON.  CREW PERFORMED NUMBER 2 ENGINE SHUTDOWN CHECKLIST AND DISCHARGED FIRE BOTTLES.  OVERHEAT LIGHT REMAINED ILUMINATED.  AIRCRAFT LANDED WITHOUT INCIDENT AT SEA.  INSPECTED AND FOUND NO EVIDENCE OF FIRE.  REPAIRED ENGINE LOWER FIRE DETECTION LOOP AND REPLACED FIRE BOTTLES AND SQUIBS PER BOEING M/M.


REMARKS:
IN FLIGHT, NUMBER 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED.  DUE TO APU PREVIOUSLY INOP AND ON MEL, CREW DIVERTED TO SFO AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 1 CSD OIL COOLER AND INLET FILTER PER BOEING M/M.


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND STRAP AND WEB 40 INCHES BY 1 INCH CORRODED AREA BS 787 - 847.  REPAIREDPER SRM 51-10-02.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  REFERENCE USAA941023.


REMARKS:
CLT - FLT 779 - THE AVIONICS COOLING VALVE LIGHT ILLUMINATED DURING FLIGHT.  THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  THE LIGHT EXTINGUISHED ON THE GROUND.  MAINTENANCE REPLACED THE EQUIPMENT COOLING VALVE.  PRESSURIZEDAIRCRAFT TO TO 3.5 PSI, NO FLUCTUATION.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND STRINGER WITH 3 INCH BY 8 INCH CORRODED AREA STATION S-26 R STATION 1006-1016.  REPAIRED PER BOEING DRAWING 65-45776 AND SRM 51-10-02.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND KEEL BEAM WITH 1 INCH WIDE, 2 INCH LONG LEVEL 2 CORROSION S-27 R AFT OFSTATION 500D.  REPAIRED PER EA 37923.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TRANSITION ANGLE WITH 2 INCH BY 6 INCH CORROSION AFT OF BS 380 RIGHT SIDE.  REPAIRED PER SRM 51-30-02.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND STRAP AND WEB 40 INCHES BY 1 INCH CORRODED AREA BS 787 - 847.  REPAIREDPER SRM 51-10-02.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  REFERENCE 94ZZZZ2183.


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND HAT CHANNEL CORRODED BS 993 RBL 14 BS 993 RBL 14 (RT AFT LAV).  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FASTENER HOLES HAT CHANNEL SUPPORT ANGLE, BS 993 RBL 14 (RT AFT LAV).  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND FLOOR SUPPORT CHANNEL SEVERLY CORRODED 1 INCH BY 8 INCH BS 1006 - BS 1016 LBL 7 INCHES.  REPAIRED PER SRM 51-10-00.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND FLOOR SUPPORT CHANNEL SEVERLY CORRODED BS 1006 - BS 1016 RBL 7 INCHES.REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-1007-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND INTERCOSTAL CORRODED AROUND FASTENER HOLES BS 986.5 RBL 19 TO BS 1006 RBL 10.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY INTERCOSTAL WITH 2 INCH BY 6 INCH AREA OF SURFACE CORROSION, STATION 952, LB 52 TO LBL 46.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 50 INCHES OF LEVEL 2 CORROSION STATION 986.5 FLOOR BEAM UPPER T-CAP.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
DURING Q-1 CHECK INSPECTION, FOUND 25.5 INCH BY 13.25 INCH DEBOND OF INNER SKIN PANEL, SKIN TO STRINGER 52 AND 53, AT STA 24011 AND 24611 RT SIDE (VISUAL AND CONDUCTIVITY INSPECTION).  CUT OUT DAMAGED AREA AND INSTALLED FILLERS, DOUBLERS AND STRINGER SECTIONS PER USAIR EA NR 27950.  (W)


REMARKS:
DURING Q-1 CHECK INSPECTION, FOUND 11 INCHES BY 9.5 INCHES DEBOND OF INNER SKIN PANEL, SKIN AND STR 22 AND 23 BETWEEN FRAMES 24011 AND 24611 LT SIDE (VISUAL AND CONDUCTIVITY INSPECTION).  CUT OUT DAMAGED AREA AND INSTALLED A FILLER AND DOUBLER AND NEW STRINGER PER USAIR EA 27949.  (W)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM UPPER CHORD DAMAGE AT BS 328, LBL 49, WL 208.  REPAIRED PER SWA RA 1-353-424.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION UPPER AND LOWER O/B BEAM SUPPORT ANGLES CRACKED 2 PLACESAT RIGHT SIDE OF BEAM JUNCTION, BS 1121.  REPLACED BEAM SUPPORT ANGLES PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD SERVICE DOOR FRAME CRACKED AT BS 294, S7R, WL 275.  INSTALLED REPAIR DOUBLER PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD SERVICE DOOR FRAME CRACKED AT BS 294, RBL 55, WL 208.  REPLACED FRAME SECTION PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION HAS CRACKED BEAM SUPPORT ANGLE AT I/B SIDE OF UPPER CHORD AT BEAM JUNCTION, BS 1121, LBL 10.  REPLACED BEAM SUPPORT ANGLES PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION HAS 2 CRACKED SUPPORT ANGLES ON I/B AND O/B SIDES OF LOWER CHORD AT BEAM JUNCTION, BS 1121, LBL 10.  REPLACED BEAM SUPPORT ANGLES PER BOEING STRUCTURAL REPAIR MANUAL.


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


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOORWAY THRESHOLD PLATE WEB DAMAGED BEYOND LIMITS.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND HAT CHANNEL CORRODED AT BS 992, LBL 40.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CORRODED AT BS 955, RBL TO 18, WL 208 AND FROM BS 1006 TO 1016, LBL 10, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORDS CORRODED AT BS 986, RBL 43, 14.3, 5, LBL 3.5, 5, 12, 14,  AND 43, WL 208.  REPLACED UPPER CHORDS BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO COMPT FRAME BENT AT BS 480, BETWEEN S24L AND 25L.  REPAIRED UPPER CHORDSBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD CARGO COMPT FRAME CRACKED AT BS 500, BL 0, WL 148.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM I/B CHORD BRACKET CRACKED AT BS 638, WL 208, RIGHT SIDE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CRACKED AT BS 178, RBL 26, LBL 26.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTS AT BS 500C+2, S18L, AT BS 333, S11R, AT BS 847, S26 TO 27R, AT BS 931, BETWEEN S20 AND 21L, AT BS 980, BETWEEN 22 AND 23L, AT BS 480, S16L, AT BS 992-996, BETWEEN S14 AND 15R, AT BS 1080,S23 AND 24L, AT BS 277, S4L TO 5L, AND AT E/E DOOR OUTER SKIN.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND TEAR STRAP SUPPORT WEBS CRACKED AT BS 847-867, WL 162.5, RBL 18 AND AT BS 767 TO 787, RBL 19.5, WL 158.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME TOP FLANGE CORRODED AT BS 787, RBL 19.5, WL 156.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE PRESSURE BULKHEAD CRACKED AT RIVET LOCATION, BS 178, WL 235.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 947, LBL 5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663.75, S10L AND 10R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND SKATE ANGLE CRACKED AT BS 560, WL 180, RBL 40.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


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


REMARKS:
DURING SCHEDULED D CHECK, FOUND KEEL BEAM LOWER CHORD CORRODED AT BS BS 520, RBL 8.  REPAIRED PER SWA EWO 94-0965.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 947, S18L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT CARGO COMPARTMENT SUB THRESHOLD WEB CORRODED FROM BS 790-845, RBL 20-29, WL 160.  REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FIXED L/E RIB GOUGED AT WS 208.  REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CORRODED AT BS 947, S25R.  REPLACED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU COWL DOOR DENTED LOWER SURFACE 8 INCHES AFT OF FORWARD EDGE.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 21L CORRODED FROM BS 809 TO 817.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 759, S7L, LBL 59, WL 277, AT BS  269, BELOW S16L, AT BS 294, AT S21R, AND AT BS 905, BETWEEN S27 AND 28L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD GOUGED AT BS 344, LBL 20.5, WL 208.  REPAIRED PER SWA RA1-353-427.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, LBL 49, RBL 42.5 AND 49.5, WL 208.  REPAIRED PER SWA RA 1-353-427.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND CRACK AT LEFT WING ON LOWER T/E OF NUMBER 3 SLAT, 6 INCHES I/B OF ACTUATOR.  REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1113, WL 240, RBL 16.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED AND CREASED FROM BS 996 TO 1012, WL 238 TO 246, BETWEEN S10 AND 14L, FROM WL 221 TO 228, BETWEEN S14 AND 15L, AND AT BS 1060, WL 208, AT S17R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 382, S22R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND OVERWING EXIT DOOR RIGHT SIDE UPPER SUPPORT CASTING CORRODED AROUND HANDLE.  REPLACED CASTING PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER 25R GOUGED FROM BS 767-787.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR SUPPORT CORRODED FROM BS 967 TO 986.5, LBL 20, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AT GATE, LEFT FORWARD ENTRY DOOR ESCAPE ACCIDENTALLY DEPLOYED.  REPLACED PER BOEING M/M.


REMARKS:
CLT - FLT 323 - DURING FLIGHT THE CREW RECEIVED A NOSE GEAR UNSAFE INDICATION.  CLT TOWER VERIFIED THAT THE NLG DOORS WERE OPEN, BUT THE LANDING GEAR WAS NOT EXTENDED.  ACFT WAS SAFELY LANDED.  THE INVESTIGATION REVEALED THAT THE MOST PROBABLY CAUSE OF THIS INCIDENT WAS THAT THE NLG FEEDBACK CABLE WAS BELOW SPEC TENSION.  (W)


REMARKS:
RSW - FLT 1082 - DURING PREFLIGHT, THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE.  MAINTENANCE FOUND THE FLIGHT ATTENDANT'SEMERGENCY EXIT LIGHT SWITCH IN THE ON POSITION.  EXTERNAL POWER WAS SUPPLIED TO ACFT TO RECHARGE THE BATTERIES.  ACFT RELEASED FOR SERVICE.  (W)


REMARKS:
LGA - EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED AFT RIGHT BATTERY PACK FOR EMERGENCY LIGHTING.  CHECK GOOD.  (X)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION AREA BS 1006 TO 1016 LBL 5.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 EACH 2 INCH DIA SPOTS OF CORROSION AND VARIOUS SMALL SPOTS, BS 986 RBL 30, RBL 36, AND RBL 38.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 10 INCH CORRODED AREA STA 1006 TO 1016 RBL 3 AND LBL 4.  REPAIRED PER BOEING DRAWING 65-46812.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORRODED AREA STA 990 RBL 10.  REPAIRED PER BOEING DRAWING 65C19883.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH AREA OF CORROSION STA 990 LBL TO LBL 48.  REPAIRED PER BOEING DRAWING 65C19883.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 36 INCH BY .5 INCH CORRODED AREA BS 1006 LBL 19.5 TO RBL 19.5.  REPAIRED PER SRM 53-00-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND (2) 1 INCH CRACKS BS 178, APPROX RBL 6 WL 201 AND 198.  REPAIRED PER EA37901.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK, BS 998 BETWEEN S-24L AND S-25L.  REPAIRED PER SRM 53-00-01 FIG 201.  (W)


REMARKS:
STL - FLT 163 - DURING FLIGHT, THE ENGINE SYSTEM 2 HYD PUMP FAULTED.  PUMP WAS TURNED OFF.  APPROXIMATELY 45 SECOND LATER THE SYSTEM 2 LOW PRESSURE LIGHT ILLUMINATED.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR1 ENGINE NR 2 SYTEM HYD PUMP.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
PIT - FLT 718 - THE FLOOR LEVEL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK FOR THE FWD SECTION OF THE FLOOR EMERGENCY LIGHTS.  LIGHTS OPERATED NORMAL.  (W)


REMARKS:
PHL - THE EMERGENCY LIGHTS L63 AND L64 WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY ASSEMBLY.  (W)


REMARKS:
CLT - FLT 1583 - ON TAKEOFF, THE FWD CABIN ENTRY DOOR BECAME VERY NOISY.  NO DOOR LIGHT WAS ILLUMINATED.  THE ACFT RETURNED TO FIELD.  MX ADJUSTED THE OVERCENTER DUE TO WEAKNESS.  DOOR OPERATED NORMALLY.  (W)


REMARKS:
CLT - FLT 339 - THE ACFT WOULD NOT PRESSURIZE.  THE CREW DECIDED TO RETURN TO FIELD.  MX FOUND THE NOSE WHEEL STEERING OVERIDE CAM ASSEMBLY OBSTRUCTING THE GROUND SHIFT MECHANISM.  THE CAM WAS SERVICED WITH NEW HARDWARE.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
CLT - FLT 399 - DURING FLIGHT, THE LT ENG POWER WAS UNCONTROLLABLE BY CREW.  ACFT RETURNED TO FIELD WITH LT ENG AT IDLEPOWER.  ACFT LANDED WITHOUT INCIDENT.  MX REPLACED THE T26 THERMAL UNIT ON THE LT ENG.  OPERATION AND LEAK CHECK GOOD.(W)


REMARKS:
PIT - FLT 1143 - FLIGHT EN ROUTE BWI TO LAX WHEN APU SHUTDOWN WITH OVERSPEED LIGHT ON.  THE NR 1 GEN WAS ON MEL.  FLIGHT DIVERTED TO PIT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MX REPLACED APU 3 SPEED SWITCH.  APU OPS CHECKED NORMAL.  ADJUSTED GEN FREQUENCY TO PROPER LEVEL AND REMOVED MEL.  PERFORMED OVERWEIGHT LANDING CHECK.  ACFT OK FOR SERVICE.  (W)


REMARKS:
SNA - FLT 8620 - DURING MISSED APPROACH UNABLE TO RETRACT FLAPS.  FLIGHT DIVERTED TO SNA WHERE A NORMAL LANDING WAS MADE.  AFTER LANDING FLAPS RETRACTED.  MX REPLACED FLAP/SLAT ACCESSORY UNIT.  CYCLED FLAPS SEVERAL TIMES.  OPERATIONAL CHECK GOOD.  (W)


REMARKS:
MCI - FLT 1103 - UNABLE TO PRESSURIZE ACFT.  FLIGHT RETURNED TO MCI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE TIGHTENED LOOSE FITTING ON CHAMBERA SUPPLY LINE.  PRESSURIZED ACFT ON GROUND.  OPS CHECKS GOOD.  (W)


REMARKS:
FLL-LGA - FLT 2203 - FLIGHT EN ROUTE, WHEN ANTI-SKID LIGHT CAME ON IN FLIGHT.  FLIGHT DIVERTED TO EWR WHERE LANDING WASWITHOUT INCIDENT.  MAINTENANCE RELEASED ON MEL 32-2.  REPLACED LT O/B ANTI-SKID VALVE.  (W)


REMARKS:
CLT - FLT 670 - FLIGHT EN ROUTE FLL TO PIT WHEN NR 2 GENERATOR DROPPED OFF LINE, AND APU WOULD NOT START.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CSD.  APU GROUND CHECKS NORMAL.  (W)


REMARKS:
CLT - FLT 1094 - AFTER RAISING THE LANDING GEAR ON TAKEOFF, MFDU SHOWED ALL GEAR UNSAFE.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND THAT PSEU BITE CHECKS GOOD.  VERTIFIED CONDITION AND OPERATION OF NORMAL AND ALTERNATE GEAR HANDLE SWITCHES.  JACKED ACFT, ACCOMPLISHED L/G ADJUSTMENT TEST PER MM 32-00-00-720-815-A.  NO DEFECTS NOTED.  L/G OPERATION AND INDICATION CHECK NORMAL.  (W)


REMARKS:
MCO - FLT 244 - ON TAKEOFF, FUEL WAS DUMPED FROM BOTH WING VENT VALVES.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE SUSPECTED VENT VALVE STUCK.  FUELED ACFT AND PERFORMED HIGH SPEED TAXI.  NO EVIDENCE OF FUEL COMING FROM VENT SYSTEM.  ALL INDICATIONS NORMAL.  (W)


REMARKS:
PHL - FLT 143 - ON DESCENT INTO PHL WHEN LANDING GEAR WAS DEPLOYED, RT MLG DID NOT EXTEND.  CREW RECYCLED LANDING GEAR AND DID FLYBY TOWER.  TOWER CONFIRMED LANDING GEAR WAS STILL UP.  CREW IMPLEMENTED MANUAL GEAR EXTENSION AND GEAR DEPLOYED.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE ACCOMPLISHED OPERATION TEST.  RETRACTED GEAR AND ACCOMPLISHED INSPECTION OF GEAR.  OPS CHECK OKAY.  LUBED RT MAIN GEAR.  OKAY FOR SERVICE.  (X)


REMARKS:
PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT CENTER SECTION OF ACFT.  REMOVED ANDREPLACED BATTERY ASSEMBLY, OPS CHECK GOOD.  (W)


REMARKS:
CLE - THE FWD CEILING EMERGENCY LIGHTS WOULD NOT SHUT OFF.  THEY WOULD COME BACK ON THE ACFT BATTERY OFF.  MAINTENANCE REPLACED THE POWER SUPPLY.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 1810 - THE RT AFT THREE EXIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERYPACK.  (W)


REMARKS:
CLT - FLT 261 - AFTER TAKEOFF CRUISE, THERE WAS A HOT OILY SMELL FROM THE AIR CONDITIONER IN LEFT LAVATORY.  MAINTENANCE REPLACED THE APU ASSEMBLY.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
STL - FLT 1898 - AT FL 350, THE OIL QUANTITY WAS LOST ON THE LT ENGINE. THE PRESSURE DROPPED AND THE CAPTAIN THROTTLED THE ENGINE BACK TO IDLE.  THE ACFT DIVERTED TO STL.  MAINTENANCE FOUND THE LT ENGINE RADIAL DRIVE SHAFT UPPER SHROUD BOLTS LOOSE.  THE BOLTS WERE REPLACED.  (W)


REMARKS:
LGA - NUMEROUS EMERGENCY LIGHTS INOPERATIVE.  BATTERY PACK WILL NOT HOLD CHARGE.  MAINTENANCE REPLACED BATTERY PACKS M1132, M1133, M1134, M1135, M1137, AND M1179.  ALL EMERGENCY LIGHTS OPS CHECK GOOD.  (W)


REMARKS:
PIT - FLT 1774 - DURING FLIGHT, THE DUCT LEAK LIGHT ILLUMINATED.  AFTER FOLLOWING ABNORMAL PROCEDURES, THE POWER REDUCED AND THE LIGHT EXTINGUISHED.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED SEALS ON THE TAIL DUCT SECTIONS.  OPERATION CHECKS GOOD.  (W)


REMARKS:
EWR - FLT 190 - DURING FLIGHT, LOST HYDRAULIC UTILITY SYSTEM.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED O-RING AT LANDING GEAR SELECTOR VALVE UNION.  SERVICED HYD SYSTEM, CHECKS FILTERS, RAN ENGINES.  OPERATION AND LEAK CHECK NORMAL.  (W)USAA94117


REMARKS:
YUL - FLT 449 - CLIMBING THROUGH 3000 FEET, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN.  THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD.  THE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE CLEANED THE OIL OUT OF THE RT ENGINE. OIL CONTAMINATION OF THE RT AIR CONDITIONING SYSTEM WAS FOUND.  THE RT ENGINE INLET FAN CASE WAS REPLACED.  MAINTENANCE THAN RAN THE ENGINE AND CHECKED THE AIR CONDITIONING SYSTEM.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
TRI - FLT 2416 - THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY BATTERIES.  SYSTEM CHECKED GOOD.  (W)


REMARKS:
DURING HEAVY MAINTENANCE VISIT, FOUND TWO .1875 INCH CRACKS AT FUSELAGE FRAME STA 1104 LONGERON 20R.  INSTALLED DOUBLERREPAIR PER SRM 53-03 FIG 30.  (W)


REMARKS:
DURING HEAVY MAINTENANCE VISIT, FOUND ROUTE OUT OF INNER PAN DOUBLER FWD CARGO DOOR CRACKED .25 INCH.  CRACK IS JUST ABOVE NR 1 AFT BEAM END IN THE RADIUS.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-30-05.  (W)


REMARKS:
DURING HEAVY MAINTENANCE VISIT, FOUND 1.25 INCH CRACK AT FWD CARGO DOOR NR 5 BEAM FWD TEE CAP.  INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2.  (W)


REMARKS:
DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION LT LAV FLOOR BEAM AT STA 965.  CUT OUT CORROSION AND INSTALLED DOUBLER REPAIR PER DACO ROD SKETCH 92-08-26-009 AND USAIR EA NR 16933B.  (W)


REMARKS:
DURING HEAVY MAINTENANCE VISIT, FOUND .3750 INCH CRACK IN SKIN AT TOP AFT PAX DOOR STOP HOLE.  VISUAL AND EDDY CURRENT SID INSPECTION PSE NR 53-09-031.  INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-05 FIG 26A.  (W)


REMARKS:
LGA - FLT 1583 - ON TAKEOFF, BOTH OMEGAS STAYED IN HOLD.  AFTER COMING OUT OF HOLD THEY FROZE THEN QUIT.  THE CREW RETURNED TO FIELD.  MAINTENANCE ACCOMPLISHED OMEGA CHECK-OUT.  SYSTEM CHECKS NORMAL.  (W)


REMARKS:
PHL - THE L3 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE CHARGER AND BATTERY PACK. REF 94ZZZW3224.  (W)


REMARKS:
CLT - FLT 2219 - EN ROUTE MCO TO LGA, WHEN A BURNING ODOR, NO SMOKE WAS DETECTED IN CABIN.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE INSPECTED ACFT FOR LEAKS AND INSPECTED ENGINE AND PACK INTAKE,FOUND NORMAL.  OPERATED PACKS AND GALLEY EQUIPMENT, NO DEFECTS NOTED.  REPLACED BOTH WATER SEPERATOR BAGS, PRECAUTIONARY.  (W)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 360, S16R, WL 214.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT UPPER LATCH BRACKET AREA.  REPAIRED PER SWA ACO 3194-52.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR CRACKED AT FWD LOWER DOOR STOP CUOUT.  REPAIRED PER SWA ACO 3194-52.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR CRACKED AT FWD LOWER DOOR STOP CUTOUT.  REPAIRED PER SWA ACO 3194-52.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FWD CARGO DOOR CRACKED ABOVE FWD LWR DOOR FITTING.  REPAIRED PER SWA ACO 3194-52.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WING STRINGER 16L CRACKED AT FWD SIDE OF WING ICE LIGHT.  REPAIRED PER SWA ACO 6403-53.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT BOTTOM CORNER, BS 294.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING C-CHECK INSPECTION, FOUND RT HORIZONTAL STABILIZER SLIDE PLATE FORWARD TRACK SPLIT.  FABRICATED REPLACEMENT TRACK AND REASSEMBLED.  TREATED AND PRIMED REF. SRM 51-10-2, SRM 51-30-2, SRM 51-30-8, AND MM 55-10-61.


REMARKS:
DURING C-CHECK AND S.S.I. INSPECTIONS, FOUND CORROSION UNDER TOP RT WING SKIN ABOVE SPAR AT WS 295.  REMOVED CORROSION DAMAGE AND TREATED.  OVERSIZED FASTENER HOLES, AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION.  NO DEFECTS NOTED.FLAP PEENED REWORK AREAS AND INSTALLED PROTECTIVE FINISHES.  REASSEMBLED.  REF. BOEING REPAIR M-7272-94-4743, OHM 20-10-3, SRM 51-10-6 AND SRM 51-10-2.


REMARKS:
SAV - FLT 1494 - EN ROUTE PIT TO MCO WHEN APU GENERATOR QUIT.  THE NR 1 GENERATOR ON MEL.  FLIGHT DIVERTED TO SAV WHERELANDING WAS WITHOUT FURTHER INCIDENT.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 664 RBL 24 INCH.  REPAIRED PER EO 5791G632.  (Z)


REMARKS:
DURING APPROACH INTO BUR, FLIGHT ATTENDANTS NOTED FUMES IN CABIN AREA.  COCKPIT CREW NOTED NORMAL AIRCRAFT SYSTEMS OPERATION WITH FUMES NOT DETECTABLE IN COCKPIT.  AIRCRAFT LANDED AT BUR WITHOUT INCIDENT.  INSPECTED AIRCRAFT AND SYSTEMS, OPERATED ENGINES AND AC PACKS PER BOEING M/M.  NO DISCREPANCIES NOTED.


REMARKS:
AFTER TAKEOFF AND NORMAL GEAR RETRACTION, NOSE GEAR RED LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  ADJUSTED NOSE GEAR UPLOCK SENSOR AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND NOSE WHEEL WELL CEILING LEFT PRESSURE PANEL CUTOUT CRACKED 1.25 INCH LONG AT LEFTCORNER RADIUS.  REPAIRED PER SWA RA 1-253-1196.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AND GOUGED AT BS 500 AND 504 AT S23 AND 24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN  GOUGED AT BS 937 AND 948, S18L.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, WL 208, RBL 50 TO LBL 20.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 12 TO 50 WL 208.  REPAIRED PER SWA 1-353-424.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND NOSE LANDING GEAR WHEEL WELL CEILING WEB CRACKED 2 INCH LONG NEAR GROUND CALL HORN.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT FWD VERTICAL SUPPORT CHANNEL CRACKED AT E1 EQUIPMENT RACK.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
MCI - DURING OP-17, FOUND CRACK INBOARD AND OUTBOARD OF FORMER FRAME UPPER CHORD, STA 580, STR 25L.  REPAIRED PER SSRM 53-60-202 AND STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  36,455 HOURS; 23,628 CYCLES.


REMARKS:
MCI - DURING OP-17, FOUND CORROSION AND SKIN PILLOWING OUTBOARD OF STR 28R BETWEEN FS 700 AND FS 720.  CUT OUT CORRODEDSECTION AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3, FIGURE 3A, SHEETS 1-3, AND STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  36,455 HOURS; 23,628 CYCLES.


REMARKS:
JFK - DURING CRUISE, SINGLE SERVING CART, PN 953000-119, SHORTED, EMITTING SMOKE.  TURNED OFF ELECTRICAL POWER.  REPLACED SERVING CART, SN 0531.  OPERATION CHECKED NORMAL.  CHECK C-1 - 9-27-94 - MCI.


REMARKS:
MCI - DURING OP-17, FOUND CORROSION ON FORMER RING FOOT FORWARD SIDE, FS 700 BETWEEN STRINGERS 27R AND 28R.  REPAIRED PER SRM 53-10-04.   AIRCRAFT TOTAL TIME:  36,455 HOURS; 23,628 CYCLES.


REMARKS:
MCI - DURING OP-17, FOUND CRACK IN UPPER FUSELAGE SKIN STA 1097, STR 1.  REPAIRED PER SB 727-53A-0204.  AIRCRAFT TOTAL TIME:  36,455 HOURS; 23,628 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN RT INTERIOR RIB AT IWS 555, FORWARD SIDE OF LOWER STR NR 10 INTO RADIUS OF RIB CASTELLATION.  REMOVED AND REPLACED RIB PER SRM 51-10-01.  AIRCRAFT TOTAL TIME:  60,963 HOURS; 22,438 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN INBOARD SIDE OF STA RIB 686.5 AT LOWER WS NR 6.  REPAIRED PER SRM57-10-05, FIGURE 2.  AIRCRAFT TOTAL TIME:  65,695 HOURS; 44,464 CYCLES.


REMARKS:
STL - DURING OP-15, FOUND CORROSION IN FORWARD CARGO COMPARTMENT FORWARD SIDE OF T-ANGLE, STA 604, LONGERONS 29L AND 30L.  REPAIRED PER SRM 53-03, PAGE 21, FIGURE 10, SHEET 4.  AIRCRAFT TOTAL TIME:  62,526 HOURS; 77,459 CYCLES.


REMARKS:
MCI - DURING CHECK-C, FOUND CORROSION AT STR 28R, STA 702 TO STA 704.  REPAIRED PER ATA 8618A.  AIRCRAFT TOTAL TIME:  36,455 HOURS; 23,628 CYCLES.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION IN FLOOR MEMBRANE AFT OF SERVICE DOOR, FS 1174.  REPAIRED BY INSTALLING DOUBLER ANDFILLER PER ARA 8955.  AIRCRAFT TOTAL TIME:  32,694 HOURS; 17,502 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A 3-INCH CRACK IN UPPER  WS NR 17, AT WS 294, OF NR 1 FUEL TANK.  REPAIRED PER SRM 57-10-4.  AIRCRAFT TOTAL TIME:  65,696 HOURS; 44,464 CYCLES.


REMARKS:
DURING CHECK-C, FOUND .25 INCH CRACK IN FORWARD LE FRAME OF CAPTAIN L-4 WINDOW.  REPAIRED BY STOP DRILLING AND INSTALLING DOUBLER PER SRM 53-30-3, PAGES 30, 31, 32, AND 38.  AIRCRAFT TOTAL TIME:  63,289 HOURSA; 42,875 CYCLES.


REMARKS:
STL - AFTER TAKEOFF, RT MLG WOULD NOT RETRACT; CYCLED LANDING GEAR AND LANDING GEAR RETRACTED.  FOUND RT MAIN LANDING GEAR ACTUATOR, MFG PN 65-17830-13, BYPASSING HYDRAULIC PRESSURE.  REPLACED RT MLG ACTUATOR, OPERATION CHECKED NORMAL.  CHECK C-2 - 1-28-94 - MCI.


REMARKS:
MCI - DURING CHECK-C, FOUND A 3-INCH CRACK APPROXIMATELY 6 INCHES BELOW WHEELWELL CEILING BETWEEN FASTENERS IN LT SIDEWALL PRESSURE WEB, BS 261-BS 264.  STOP DRILLED PER SSRM 53-10-211, PAGE 201, AND INSTALLED DOUBLER PER SRM 51-40-02, ANDSSRM 53-10-212, NOTE A.  AIRCRAFT TOTAL TIME:  60,941 HOURS; 41,615 CYCLES.


REMARKS:
MCI - DURING CHECK-C, FOUND A 3-INCH CRACK APPROXIMATELY 6 INCHES BELOW WHEELWELL CEILING BETWEEN FASTENERS IN LT SIDEWALL PRESSURE WEB.  BS 270-BS 273.  STOP DRILLED PER SSRM 53-10-211, PAGE 201, AND INSTALLED DOUBLER PER SRM 51-40-02 ANDSSRM 53-10-212, NOTE A.  AIRCRAFT TOTAL TIME:  60,941 HOURS; 41,615 CYCLES.


REMARKS:
STL - DURING OP-15 FOUND SKIN CORROSION IN FORWARD CARGO COMPARTMENT, LONGERON 30, STA 560.  REPAIRED PER SRM 53-01, PAGE 1.  AIRCRAFT TOTAL TIME:  62,526 HOURS; 77,459 CYCLES.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A 1.25 INCH CRACK IN LONGERON 5L AT STA 756, AND LONGERON 4L AT STA 737.  REPAIRED LONGERONS PER SRM 53-02, FIGURE 2.  AIRCRAFT TOTAL TIME:  65,261 HOUS; 73,330 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A CRACK .75 INCH LONG IN WING INTERIOR RIB AT IWS 503, FORMER UPPER FORWARD SIDE OF UPPER STR 16, INTO RADIUS OF RIB CASTELLATION.  REPAIRED BY STOP DRILLING CRACK PER SB 093-57-207, PARAGRAPH 2B.  AIRCRAFT TOTAL TIME:  60,963 HOURS; 22,438 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND RT WING INTERIOR RIB AT IWS 555 CRACKED APPROXIMATELY ONE INCH, FROM UPPER FORWARD SIDE, STR 11, INTO RADIUS OF RIB CASTELLATION.  REPAIRED BY STOP DRILLING CRACK PER SB 093-57-207, PARAGRAPH 2B.  AIRCRAFTTOTAL TIME:  60,963 HOURS; 22,438 CYCLES.


REMARKS:
MCI - DURING OP-15, FOUND LOWER FUSELAGE SKIN BULGED AND RIVET HEAD POPPED AT STA 1309, STR 21L-STR 22L.  REMOVED CORROSION PER SRM 51-10-3, AND REPAIRED PER ARA 8530, AND STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  32,694 HOURS; 17,502 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND .25 INCH CRACK IN RT WING INTERIOR RIB AT IWS 555, FROM AFT SIDE OF LOWER STR 7 INTO RIB CASTELLATION.  REPAIRED BY STOP DRILLING CRACK PER SB 093-57-207, PARAGRAPH 2B.  AIRCRAFT TOTAL TIME:  60,963 HOURS;22,438 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND .75 INCH CRACK IN WING INTERIOR RIB AT IWS 503, FROM UPPER FORWARD SIDE OF UPPER STR 21 INTO RADIUS OF RIB CASTELLATION.  REPAIRED BY STOP DRILLING CRACK PER SB 093-57-207, PARAGRAPH 2B.  AIRCRAFT TOTAL TIME:  60,963 HOURS; 22,438 CYCLES.


REMARKS:
DURING OP-15, FOUND CORROSION BETWEEN NR 2 AND NR 3 TRACK IN FLOOR BEAM CAP, STA 1250.  REMOVED CORROSION PER SRM 51-10-3, AND INSTALLED NEW FLOOR SUPPORT PER SRM 51-01, PAGE 1, ITEM C.  AIRCRAFT TOTAL TIME:  32,694 HOURS; 17,502 CYCLES.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION ON FLOOR ATTACH BRACKET OF AFT SERVICE DOOR, FS 1160.  REPAIRED BY CUTTING OUT CORROSION AND INSTALLING FILLER AND DOUBLER PER ARA 8531. AIRCRAFT TOTAL TIME:  32,694 HOURS; 17,502 CYCLES.


REMARKS:
STL - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 1501, DUE TO HIGH VIBRATION AND OIL FILTER BYPASS LIGHT CAME ON.  FOUND METAL PARTICLES IN OIL FILTER.  REPLACED ENGINE SN 1501.  GROUND OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  33,361 HOURS; 21,663 CYCLES.  CHECK C-2 - 1-30-94 - MCI.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND AFT PLUG DOOR LOWER HINGE CASTING LUG BROKEN.  REPAIRED BY REPLACING AFT PLUG DOOR HINGE CASTING PER SRM 51-10-03.  AIRCRAFT TOTAL TIME:  65,351 HOURS; 72,593 CYCLES.


REMARKS:
MCI - DURING CHECK-C, SKIN CORROSION FOUND BETWEEN STR 20R AND STR 19R, STA 440.  CUT OUT CORROSION AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3, PAGE 14, B, C, AND D.  AIRCRAFT TOTAL TIME:  64,880 HOURS; 44,013 CYCLES.


REMARKS:
MCI - DURING CHECK-C, FOUND THREE 1-INCH CRACKS IN WHEELWELL NOSE GEAR AT RIVET HEADS, STA 276, RBL 14,  STOP DRILLED CRACKS AND REPAIRED PER SSRM 55-10-211.  AIRCRAFT TOTAL TIME:  64,880 HOURS; 44,013 CYCLES.


REMARKS:
MCI - DURING CHECK-C, FOUND FORMER FOOT CRACKED IN 2 PLACES AT FS 1166 BETWEEN STR 30L AND STR 29L.  REPAIRED PER SRM 51-40-3.  AIRCRAFT TOTAL TIME:  61,561 HOURS; 41,655 CYCLES.


REMARKS:
MCI - DURING CHECK-C, FOUND BS 178 BULKHEAD WEB CRACKED AT FASTENER, WL 234.  REPAIRED PER SRM 51-10-07 AND SRM 51-10-01, PAGE 4.  AIRCRAFT TOTAL TIME:  61,561 HOURS; 41,655 CYCLES.


REMARKS:
MCI - DURING CHECK-C, FOUND CORROSION AT STRINGER 29R BETWEEN FS 950E AND FS 950F.  REMOVED CORROSION, REPAIRED PER ARA8605.  AIRCRAFT TOTAL TIME:  36,496 HOURS; 23,144 CYCLES.


REMARKS:
EWR - FLT 11 - AFTER TAKEOFF, NR 3 ENGINE SHUT DOWN DUE TO VIBRATION, RETURNED TO GATE.  AIRCRAFT FERRIED TO HGR FOR NR3 ENGINE CHANGE PER MM 71-21-03.  EVALUATION OF ENGINE TEAR DOWN DETERMINED CAUSE OF FAILURE DUE TO INTERNAL FOD FROM N2 COMPRESSOR TIE ROD FAILURE.  CYCLES, 21,732.  (X)


REMARKS:
SEA - INVESTIGATION INTO ENGINE TWA S/N 1422, MFG S/N 725487, STALLS REVEALED AND 8TH STAGE COMPRESSOR BLADE, P/N 802808, FRACTURED AT PLATFORM, LIBERATING BLADE WITH DOWNSTREAM DAMAGE AND PENETRATED 8TH STAGE COMPRESSOR STATOR CASE, CAUSING A .375 INCH BY 4 INCH HOLE.  ENGINE REPAIRED AND RETURNED TO SERVICE.  (Z)


REMARKS:
MCI - DURING C-CHECK, FOUND A 1 INCH CRACK, AND CORROSION ON LOWER BELLY SKIN AROUND NR 2 RADIO ALTIMETER ANTENNA, WITHSTRESSED RIVET HEADS.  REMOVED CORROSION, MADE REPAIR PLATE PER SRM 53-30-3, FIGURE 1, AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 1.  TOTAL CYCLES 40745.


REMARKS:
MCI - DURING C-CHECK, FOUND A FOUR INCH CRACK IN RIGHT MAIN LANGINE GEAR WHEELWELL FS 870 BULKHEAD, BELOW CUTOUT FOR APU BLEED AIR DUCT.  INSTALLED DOUBLER PER TWA DRAWING C03242 AND TWS STANDARD PROCEDURES.  TOTAL CYCLES 40,745.


REMARKS:
MCI - DURING OP-8 FOUND CORROSION ON FUSELAGE LAP SEAM, STA 680-715, STRINGERS 25L AND 26L.  REPAIRED PER BOEING DWG NR69-61590.  TOTAL CYCLES 42,376.


REMARKS:
MCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN FUSELAGE SKIN AT UPPER HINGE ARM CUTOUT FOR FORWARD ENTRY DOOR.  INSTALLED DOUBLER PER SSRM 53-10-219, PARAGRAPH 209, DETAIL 33.  TOTAL CYCLES 40,745.


REMARKS:
RDU - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON.  VISUALLY CHECKED LANDING GEAR DOWN.  REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH, MFG P/N H14-6.  LANDING GEAR LIGHT INDICATION CHECKED NORMAL.  CHECK C 5-2-94 STL.


REMARKS:
MCI - DURING C-CHECK, FOUND CRACKS EXTENDING .25 INCH FROM RIVET HOLES IN LEFT PRESSURE BULKHEAD, BELOW AFT COVERPLATE,STATION 274, LBL 23.  STOP DRILLED CRACKS AND INSTALLED REPAIR PER SSRM 53-10-211, PAGE 201.  TOTAL CYCLES 39,407.


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION IN FUSELAGE SKIN BELOW FORWARD LAV SERVICE ACCESS DOOR.  REPAIRED PER SRM 53-30-3, PAGES 6, 7 AND 8.  TOTAL CYCLES 43,889.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CORROSION AT FORWARD CARGO STRINGER 25L, AND CRACK IN BOTTOM AT STATION 600.  REMOVEDCORROSION AND REPAIRED PER SRM 53-10-3, DETAIL 1, FIGURE 1, AND STANDARD PRACTICES.  TOTAL CYCLES 42,376.


REMARKS:
MCI - DURING OP-17 FOUND A TWO INCH CRACK IN FRAME AT STRINGER 16L, FS 303.  REPAIRED PER DWG 65C20303 AND TWA STANDARDPRACTICES.  TOTAL CYCLES 24,619.


REMARKS:
MCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN FORWARD ENTRY DOOR FRAME, BEHIND LOWER FORWARD DOOR STOP CASTING.  REPAIRED PER BOEING DWG 65C20303.  TOTAL CYCLES 39,177.


REMARKS:
MCI - DURING C-CHECK, FOUND CRACK APPROXIMATELY 1.5 INCHES LONG BETWEEN RIVETS ON RT BULKHEAD WEB, STATION 256.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER SSRM 53-10-211, PAGE 201.  TOTAL CYCLES 44,342.


REMARKS:
MCI - DURING C-CHECK, FOUND CRACKS BETWEEN RIVETS ON UPPER PRESSURE BULKHEAD WEB, STATION 285 RBL 0 THROUGH 10.  INSTALLED REPAIR DOUBLER PER SSRM 53-10-211, PAGE 201, A-3.  TOTAL CYCLES 44,342.


REMARKS:
MCO - TEARDOWN OF NR 2 ENGINES S/N 4021, THAT WAS SHUTDOWN DUE TO VIBRATION, REVEALED FRONT COMPRESSOR DRIVE SHAFT, MFGP/N 670869, WAS TWISTED AND BENT, CAUSING ROTOR TO VIBRATE.  THE SHAFT WAS SOFTENED FROM EXCESSIVE HEAT.  ENGINE S/N 4021 WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
INVESTIGATION INTO THE SHUTDOWN OF ENGINE S/N 4385 FOR OIL LOSS, REVEALED NR 3 BEARING HOUSING WAS OUT OF ROUND CAUSINGSEALS TO WEAR, CAUSING OIL LEAKAGE.  ENGINE S/N 4285 REPAIRED AND RETURNED TO SERVICE.


REMARKS:
LGA - INVESTIGATION INTO THE SHUTDOWN OF ENGINE S/N 1527 DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION, REVEALED NR 3 BEARING, P/N 804059, RETAINER BROKE.  ENGINE S/N 1527 REPAIRED AND RETURNED TO SERVICE.


REMARKS:
JFK - ON TAKEOFF AFTER LANDING GEAR RETRACTION, NOSE LANDING GEAR DOOR WOULD NOT CLOSE.  FOUND LEFT NOSE LANDING GEAR DOOR SEAL RETAINER BENT.  REPAIRED DOOR SEAL RETAINER.  CHECK OPERATION OF DOOR AND BUNGEE, OPERATION CHECKED NORMAL.  CHECK C-3C, 11-15-94 JFK.


REMARKS:
MCI - DURING C-CHECK, FOUND BULKHEAD WEB CRACKED 3.5 INCHES, BELOW APU LOAD CONTROL VALVE WELL, STATION 870.  STOP DRILLED CRACKED AND REPAIRED PER TWA DRAWING C03242.  TOTAL CYCLES 48,555.


REMARKS:
MCI - DURING OP- 17 FOUND CORROSION AROUND FASTENERS IN AFT CARGO BIN OUTBOARD FLANGE, STRINGER 29L, STATION 970 AND STATION 990.  REMOVED CORROSION PER SRM 51-10-6, REPAIRED PER ARA 8961 AND STANDARD PRACTICES.  TOTAL CYCLES 23,628.


REMARKS:
MCI - DURING OP-17 FOUND 4 INCH LONG CRACK IN AFT CARGO BIN KEEL BEAM, STRINGER 29R, STATION 990.  REPAIRED PER ARA 8637 AND STANDARD PRACTICES.  TOTAL CYCLES 23,628.


REMARKS:
PIT - THE EMERGENCY LIGHTING ALONG THE FLOOR IN CABIN WAS COMING LOOSE IN PLACES.  MAINTENANCE REPLACED THE NR 1 SECTION OF LOW LEVEL LIGHTING.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 971 - THE EMERGENCY EXIT OVERWING AT 12F HAS A LOUD SQUEAL.  MAINTENANCE RESEALED THE RT SIDE MAIN FRAME SEAM.  NO LEAKS NOTED.  ACFT OK FOR SERVICE.  (W)


REMARKS:
PIT - LEFT AFT EXTERIOR EMERGENCY LIGHT LOCATED BEHIND LEFT I/B FLAPS INOPERATIVE.  MAINTENANCE REPLACED LIGHT SOCKET ASSEMBLY, NO HELP.  RELEASED ON MEL 33-14.  FOUND BAD WIRE IN AFT CARGO BIN.  REPAIRED WIRE AND REPLACED BATTERY PACK POWER SUPPLY M1136.  OPS CHECK NORMAL.  REMOVED MEL.  (W)


REMARKS:
LGA - FLT 1879 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF.  LOUD SQUEAL HEARD FROM MAIN ENTRANCE DOOR.  FLIGHT RETURNED TO LGA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED MAIN CABIN DOOR GUIDE ARM, AND TIGHTENED LOWER CAM PLATE.  PRESSURIZED ACFT TO 35 PSI, NO LEAKS NOTED.  PROGRAMMMED MAIN DOOR HINGES, PRECAUTIONARY.  (W)


REMARKS:
CLT - FLT 1538 - AFTER TAKEOFF, THE FWD PASSENGER DOOR INDICATED CLOSED AND LOCKED.  HOWEVER, THERE WAS A LOUD AIR NOISE AROUND THE DOOR.  THE CREW RETURNED TO THE FIELD.  MAINTENANCE FOUND THE FWD PASSENGER DOOR NOT FULLY CLOSED.  THEY CLOSED THE DOOR.  ACFT OK FOR SERVICE.  (W)


REMARKS:
TPA - FLT 1873 - ON CLIMBOUT AT 22000 FEET, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON.  THE CREW RETARDED THE NR 3 THROTTLE, LIGHT EXTINGUISHED AFTER ONE MINUTE.  THE CREW RETURNED TO THE FIELD.  MAINTENANCE FOUND THE RT PRECOOLER EXHAUST DUCT CRACKED AND WITH A HOLE IN IT.  THE DUCT WAS REPLACED.  ACFT OK FOR SERVICE.  (W)


REMARKS:
PIT - DURING OVERNIGHT CHECK, FOUND 1 INCH BY 2 INCH DENT AND .5625 INCH CRACK IN THE SKIN AT STA 508 ON STRINGER 27L.INSTALLED STRINGER SPLICE AND SKIN DOUBLER REPAIR PER SRM 53-00-03 FIG 201 AND SRM 53-00-01, FIG 201.  (W)


REMARKS:
DURING C-8 CHECK INSPECTION, FOUND CORROSION (PITS BEYOND LIMITS) BETWEEN STA 160 AND 180, ALSO BETWEEN LONERONS 27L AND 30L.  CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-04 FIG 12B SHT 1 AND USAIR EA NR 28129.  (W)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTS AT BS 355, BETWEEN S17 AND 18R, AT BS 1006 TO 1014, WL 234-242, LEFT SIDE, AT BS 192, WL 238, LEFT SIDE, AT BS 410-420, BETWEEN S21 AND 22R, AT BS 367, BETWEEN S17 AND 18R, AND AT BS 339, BETWEEN S19 AND 20 RIGHT SIDE.  REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND KEEL BEAM NUTPLATE HOLES CORRODED AT BS 672-676, LBL 8.  REPAIRED ALL PER TRAMCO EWO 94-0990.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318, S18R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, GEAR RETRACTED, GEAR UNSAFE RED LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 1 THROTTLE SWITCH S139 AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
DURING SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 389.5, S19L, BS 470, S19L, BS 493,S19L, BS 500+1, S19L, BS 500+10, S19L, BS 500A+9, S19L, BS 351 AND 352, S24R, BS 303.5, S24L, BS 380, S14R, BS 390 AND 391, S14R, BS 411 AND 420, S14R, BS 420, S14R, BS 470.5, S10L, BS 500B, S10L, BS 500B+9, S10L, BS 674, S4L.  REPAIRED PER TRAMCO EWO 94-0962.


REMARKS:
DURING SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 747, S4L, BS 857, S4R, BS 490, S4L, BS 569, SS4L, BS674, S4R, BS727+10, S4R, BS747, S4R, BS 285.5, S4R, 328, S4R, BS 588, S4R, BS 639, S4R, BS 369.5, S19R, BS 380 AND 381, S14L.  REPAIRED PER TRAMCO EWO 94-0962.


REMARKS:
MCI - DURING OP-16 FOUND FLOOR BEAM BROKEN AT FUSELAGE FORMER RING FRAME, STA 1183, LBL 113.  REPLACED FLOOR BEAM PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CRACK .5 INCH LONG IN RT WING AT IWS 503, IN CASTELLATION ON FWD SIDE OF UPPER STRINGER 18.  REPAIRED PER LOCKHEED DWG 1647070.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR SUPPORT IN LOWER GALLEY, FS 806, RBL 44 TO LBL 44.  REPAIRED BY INSTALLATION OF NEW FLOOR SUPPORT PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON FLOOR SUPPORT BEAM, BL O, FS 806 TO FS 901.  REPAIRED BY INSTALLATION OF NEW H-BEAM PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON SKIN AND STRINGER 27 AT FS 1620.  REMOVED CORROSION AND INSTALLED DOUBLER PER SRM51-21-01 AND ARA 8640, AND SRM 51-50-02.  TOTAL CYCLES 17032


REMARKS:
MCI - DURIG OP-16 FOUND CORROSION ON FORMER FOOT BETWEEN STRINGERS 33 AND 34, AND CORROSION ON STRINGER 34, STA 1585.  REMOVED CORROSION PER SRM 51-21-01, AND REPLACED PART PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION LOWER GALLEY FLOOR SUPPORT, STA 886, RBL 24 TO RBL 46.  REPLACED FLOOR SUPPORT PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON LOWER GALLEY FLOOR SUPPORT, LBL 26, STA 901 TO STA 920.  REPLACED FLOOR SUPPORT PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON SKIN UNDER TEAR STRAP AT FS 1715, STRINGER 39.  CORROSION REMOVED, AND DOUBLER INSTALLED PER SRM 53-31-00 AND ARA 8639.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON SKIN BETWEEN FS 1463-1480, BETWEEN STRINGERS 28 AND 29, ON STRINGER 29.  DOUBLER INSTALLED AND STRINGER 29 SPLICED PER SRM 53-30-03 AND SRM 53-31-01, FIG 804.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON SKIN UNDER FAIL SAFE STRAP AT FS 1755, STRINGER 36-37.  REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-21-01 AND ARA 8648.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON FUSELAGE BELLY SKIN, FS 1520 TO FS 1620, STRINGER 35 TO STRINGER 41.  REMOVED CORROSION PER SRM 51-21-01 AND REPAIRED PER SRM 53-31-30, FIG 827. TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON LOWER GALLEY FLOOR SUPPORT H-BEAM, STA 709 TO STA 901.  REPAIRED BY INSTALLING NEW H-BEAM PER SRM 51-01-10.  TOTAL CYCLES 17032.


REMARKS:
BOS - FLT 2417 - THE NOSE WHEEL LIGHT TO INDICATE GEAR DOWN DID NOT ILLUMINATE.  THE CREW DECLARED AN EMERGENCY.  ALL OTHER INDICTIONS NORMAL.  MAINTENANCE REPLACED A FAULTY NOSE GEAR LIGHT SOCKET.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
TPA - FLT 2497 - UNABLE TO RETRACT MAIN LANDING GEAR AFTER TAKEOFF.  FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  'MAINTENANCE FOUND LEVER LATCH CIRCUIT BREAKER POPPED.'  RESET CIRCUIT BREAKER AND LANDING GEAR HANDLEOPERATED NORMALLY.  OK FOR SERVICE.  (Z)


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON LOWER GALLEY FLOOR SUPPORT BEAM, ST 901 LBL24 TO LBL 46.  REPLACED FLOOR SUPPORT BEAM PER SRM 51-10-01.   TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON STRINGER 29, FS 1655-1685.  CORROSION REMOVED AND DOUBLER INSTALLED PER SRM 51-21-01 AND ARA 8643.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON LOWER GALLEY FLOOR SUPPORT RBL 24, STA 886 TO STA 901.  REPLACED FLOOR SUPPORT PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND SKIN CORROSION UNDER FAIL-SAFE STRAP AT FS 1770, STRINGER 37.  CORROSION REMOVED AND DOUBLER INSTALLED PER SRM 51-21-01 AND ARA 8641.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CORROSION ON WEB NEAR FORMER RING, FS 1585, BETWEEN STRINGERS 33 AND 34.  REMOVED CORROSION PER SRM 51-21-01, AND REPLACED PART PER SRM 51-10-01.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND .5 INCH CRACK IN RADIUS OF RT WING RIB AT IWS 555, FWD UPPER SIDE OF STRINGER 18. REPAIRED BY STOP DRILLING PER EMLR 64328.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND FLOOR PANEL SUPPORT ANGLE BROKEN BETWEEN FLOOR PANELS 96 AND 106, STA 983.  REPAIRED PER SRM 57-10-05, PG 9, PARAGRAPH 1.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURINGS OP-16 FOUND CRACK IN CABIN RT SHEAR TIE ANGLE ABOVR RADIUS, STA 1183.  REPAIRED PER SRM 57-11-00, FIG 808, AND SB 093-53-197.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND .5 INCH CRACK IN RT WING RIB INTO RADIUS OF RIB AT IWS 555, FWD SIDE OF STRINGER 12.  REPAIREDBY STOP DRILLING PER EMLR 64328.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CRACK IN RT SHEAR TIE ANGLE ABOVE RADIUS, AT STA 1203.  REPAIRED PER SRM 57-11-00, FIG 808, SB093-53-197.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CRACK .25 INCH LONG IN RT WING RIB AT IWS 503, IN CASTELLATION ON FWD SIDE OF UPPER STRINGER 20.  REPAIRED PER LOCKHEED DWG 1647070.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CRACK .75 INCH LONG IN RT WING RIB AT IWS 503, IN CASTELLATION ON FWD SIDE OF UPPER STRINGER 19.  REPAIRED PER LOCKHEED DWG 1647070.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CRACKED RT SHEAR TIE ANGLE AT STA 1063.  REPAIRED PER SB 093-53-197.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND CRACKED FORMER RING FRAME BELOW FLOOR LEVEL, STA 1063.  REPAIRED BY REPLACING CRACKED PART PERSB 093-53-197.  TOTAL CYCLES 17032.


REMARKS:
MCI - DURING OP-16 FOUND 2.5 INCH CRACK IN CABIN, RT STA 1083 FRAME, JUST BELOW FLOOR LINE.  REPAIRED PER SRM 51-10-01 AND STANDARD PRACTICES.  TOTAL CYCLES 17032.


REMARKS:
DURING OP-16 FOUND CABIN RT FORMER RING FRAME BROKEN AT FLOOR LEVEL, STA 1103.  REPAIRED PER SRM 53-10-05 AND STANDARD PRACTICES.  TOTAL CYCLES 17032.


REMARKS:
SAT - FLT 335 - ON APPROACH WHEN LANDING GEAR WAS LOWERED, THE NOSE GEAR WARNING LIGHT FAILED TO INDICATE DOWN AND LOCKED.  FOUND PROXIMITY SWITCH TARGET MISSING.  REPLACED TARGET, MFG (P/N 3928161).  OP CHECKS NORMAL.  CHECK C 3-14-94 PHX.


REMARKS:
LANDING GEAR FAILED UP LATCH CHECK, AND HAD UNSAFE LIGHTS ON WITH GEAR RETRACTED.  LANDING GEAR OK IN DOWN POSITION.  REMOVED AND REPLACED LT AND RT TORQUE LINK BUMPER PADS, OPS CHECK GOOD PER MM 32-30.


REMARKS:
ATL-IND - FLT 562 - AFTER TAKEOFF,TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED FOR 5 SECONDS.  ACFT RETURNED TO ATL WITHOUT INCIDENT.  MAINTENANCE CHECKED DUCTING AND FOUND THE SECONDARY HEAT EXCHANGER AT FAULT.  REMOVED AND REPLACED (P/N184060-3-2).


REMARKS:
ATL-IND - FLT 562 - UPON TAXIING THE TAKEOFF WARNING HORN SOUNDED, CREW CYCLED FLAPS AND THE HORN SHUT OFF.  AS CREW APPLIED POWER FOR TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED, CREW ABORTED TAKEOFF.  MANTENANCE READJUSTED FLAP SWITCH.


REMARKS:
LEFT HORIZONTAL STAB LWR AFT O/B SKIN CRACKED AT AFT RIVET ROW.  EXCEEDS 4 INCHES IN LENGTH.  DURING C CHECK.  REMOVED AND REPLACED HORZ STAB IAW MM 55-10-0.  BOTH ELEVATORS TRANSFERRED FROM OFF STAB ONTO NEW STAB S/N 0174ML IAW MM 27-30-2.


REMARKS:
LT WING I/B SPOILER DELAMINATED AT LOWER SURFACE, 10 INCHES DIA AT XFS145 AND UPPER SURFACE 5 INCHES DIA DURING C CHECK.  REPLACED SPOILER PANEL IAW MM 27-61-1.


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, FOUND .50 INCH CRACK RIGHT ENGINE PYLON ATACH ANGLE FWD UPPER LEADING EDGE.  INSTALLED DOUBLER REPAIR PER SRM 54-04, FIGURE 10.  (X)


REMARKS:
INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 12 INCH CORROSION AT STR BS 907 S-27 L.  REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING REVISION 'F' VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES AT S-26 L, LT SIDE OF E & E COMPARTMENT.  REPAIRED PER BOEING DRAWING 65-59664.  CORROSION TASK NR C55-202-02.  CORROSION LEVEL 2.  (X)


REMARKS:
GO - FLT 489 - GEAR WOULD NOT RETRACT ON TAKEOFF.  FLIGHT RETURNED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE CLEANED AND LUBED GEAR LEVER LOCK SOLENOID, AIR/GROUND SENSE CABLE AND MECHANISM.  RETRACTED GEAR NUMEROUS TIMES AND ALL CHECKS NORMAL.  (X)


REMARKS:
CLT - FLT 2525 - AFTER TAKEOFF IN CLT, CREW RECEIVED AN AIR TO GROUND SENSOR FAILURE AND WERE UNABLE TO RETRACT LANDINGGEAR.  FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS ACCOMPLISHED.  MAINTENANCE FOUND AIR/GROUND TELEFLEX CABLE OUT OF ADJUSTMENT.  PERFORMED GROUND AND AIR SAETY SENSOR TARGET ADJUSTEMNTS AND GROUND SPOILER INTERLOCK VALVE TARGETADJUSTMENT.  SYSTEM CHECKED OKAY.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION BS 1016 LBL 6 AND RBL 4.  REPAIRED PER SRM51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION BS 967 LBL 24.  REPAIRED PER TR 53-10-05 C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LT AND RT SIDE.  FOUR FASTENER HOLES OVERSIZED BS 1156, LT AND RT O/B.  REPAIRED PER E.O. 5391G569.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2.25 INCH CRACK 6 INCHES ABOVE FLOOR LEVEL STA 639 STR 17 L.  REPAIRED PER SRM 51-10-01 PAGE 5.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 1 INCH AREA (SEVERAL PLACES) CORRODED.  FLOOR BEAM UPPER 'T' BS 328, LBL - 12 TO RBL 55.  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 .50 INCH BY .50 INCH AREA CORRODED (2 PLACES) BS 277 TO BS 294, LBL 11, WL 208.  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 1 INCH BY .50 INCH AREA CORRODED (2 PLACES) FLOOR BEAM BS 277, LBL 11TO LBL 26, WL 208.  REPAIRED PER TR 53-10-01 A.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CORRODED BEAM CAP FASTENER HOLES.  BS 360 BL ZERO LBL 10.  REPAIRED PER E.A. 37937 TR 53-10-05.  CORROSION TASK NR C53-107-1.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 11 INCH CORROSION BS 344 FROM LBL 9 INCH TO RBL 9 INCH.  REPAIRED PER SRM 53-10-13.  CORROSION TASK NR C53-107-1.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORRODED AREA BS 253 FLOOR BEAM CAP LBL 6 TO RBL 6. REPAIRED PER TR 53-10-16 AND EA 37888.  CORROSION TASK NR C53-101-01.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION FOUND 8 INCH CORROSION BS 927 S-25L.  REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 328, RLB 52.  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 1.50 INCH BY 1.50 INCH CORROSION BS 987 LBL 43.  REPAIRED PER TR BG 53-10-05.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 5 INCH BY 5 INCH CORROSION BS 1012 LBL 4.  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 5 INCH BY 2 INCH CORROSION BS 987 AND .75 INCH SPOT BS 1006.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
TUL - FLT 1111 - FLIGHT EN ROUTE PHL TO DFW WHEN CREW NOTICED LEFT ENGINE OIL QUANTITY INDICATING ZERO AND OIL PRESSURE40 TO 45 POUNDS.  CREW SHUT DOWN LEFT ENGINE AND DIVERTED TO TUL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 1 ENGINE AND NR 1 ENGINE MAIN OIL PUMP.  (X)


REMARKS:
BWI - FLT 927 - UNABLE TO PRESSURIZE AIRCRAFT AFTER DEPARTURE FROM DCA.  FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND PRECONDITIONED GROUND AIR CHECK VALVE LEAKING.  SECURED VALVE IN CLOSED POSITIONPER MEL 21-26.  REPLACED VALVE.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA, FORWARD CARGO S-25 R AT DOOR OPENING. REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 12 INCH CORROSION Z-ANGLE FORWARD ENTRY.  REPAIRED PER SRM 51-10-06.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
CLT - LOW LEVEL EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN AC POWER IS REMOVED.  MAINTENANCE REPAIRED WIRE AT SEAT ROW 12 ABC.  OPS CHECK GOOD.  (X)


REMARKS:
DURING ACCOMPLISHEMNT OF Q-3 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT RT LAV FLOOR BEAM STA 980COROSION TASK NR C58-53300.  INSTALLED DOUBLER REPAIR PER US AIR TYPICAL REPAIR 53-10-19.  (X)


REMARKS:
DURING ACCOMPLISHEMNT OF A Q-3 CHECK INSPECTION, 2 CRACKS FOUND .50 INCH LONG EACH IN ANGLE AND SKIN IN PASSENGER ENTRANCE DOOR OPENING RT UPPER CORNER.  INSTALLED DOUBLER REPAIR PER DACO DWG J060088-507 CONFIG.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 INSPECTION, LEVEL 1 CORROSION PREVOUSLY REWORKED AT LEFT LAV STA 980 FLOOR BEAM.  CORROSION TASK NR C58-5330.  SPLICED IN NEW SECTION OF FLOOR BEAM PER US AIR TYPICAL REPAIR 53-10-19.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, LEVEL 1 CORROSION PREVIOUSLY REWORKED IN LEFT LAV STA 996 FLOOR BEAM CORROSION.  SPLICED IN NEW SECTION OF FLOOR BEAM PER US AIR TYPICAL REPAIR 53-10-14.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF Q-3 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT LEFT OUTBOARD SEAT TRACK STA 200 CORROSION TASK NR C58-53302.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05, FIGURE 4F.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, FOUND SKIN CHAFED .028 DEEP AT STA 813 LONGERON 26R AND AT 26L.  INSTALLED INTERNAL DOUBLERS PER SRM 53-04, FIGURE 38, SHT 17.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK OF LOWER FLANGE LONGERON 20L AT LEFT WING FRONT SPAR.  INSTALLED DOUBLER REPAIR PER SB 57-103.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, FOUND .3750 INCH CRACK STA 756 LONGERON 3R.  SPLICED IN NEW SECTION OFLONGERON PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, FOUND A .50 INCH CRACK LONGERON 4L AT STA 160 BELT FRAME ATTACH POINT. SPLICED IN NEW SECTION OF LONGERON PER US AIR TYPICAL REPAIR 53-10-17.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, FOUND A .50 INCH CRACK RIGHT LOWER PYLON ATTACH ANGLE AT STA 945 LONGERON 15R.  INSTALLED DOUBLER REPAIR PER SRM 53-04, FIGURE 10.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 INSPECTION, FOUND .25 INCH CRACK IN SKIN AT STA 1109 BELOW LONGERON 3R.  INSTALLED DOUBLER REPAIR PER SRM 53-40, FIGURE 27.  (X)


REMARKS:
DURING ACCOMPLISHMENT OF A Q-3 CHECK INSPECTION, FOUND .50 INCH CRACK IN LEFT OVERWING AFT EMERG. EXIT WINDOW TOP AFT STOP, CRACKED IN PAN TOP INBRD CORNER.  INSTALLED DOUBLER REPAIR PER US AIR TYPICAL REPAIR 52-20-3.  (X)


REMARKS:
RDU - FLT 1481 - DURING CRUISE, NR 2 ENGINE MADE A LOUD POP AND THEN THE N1 AND N2 RPMS ROLLED BACK.  THE CAPTAIN TRIEDTO ADVANCE THROTTLES BACK TO A HIGHER SETTING, BUT THE ENGINE WOULD NOT RESPOND TO THROTTLE COMMANDS.  THE CAPTAIN REQUESTED AN EMERGENCY LANDING IN RDU AND HAD AN UNEVENTFUL APPROACH.  MAINTENANCE REPLACED NR 2 ENGINE.  OPERATIONS CHECKEDGOOD.  (X).


REMARKS:
PHL - FLT 0836 - ON APPROACH TO PHL, THE GREEN NOSE GEAR LIGHT DID NOT ILLUMINATE AS THE GEAR WAS LOWERED.  THE CREW RECYCLED GEAR, BUT GREEN LIGHT STILL DID NOT ILLUMINATE.  THE CREW THEN RESEATED THE BULBS FOR THE NOSE GEAR LIGHT AND THELIGHT FINALLY ILLUMINATED.  THE AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NOSE GEAR SAFE LIGHT SOCKET.  OPERATIONS CHECKED GOOD.  (X)


REMARKS:
STL - FLT 0754 - AFTER TAKEOFF, GEAR WOULD NOT RETRACT.  CREW RETURNED TO STL AND LANDED WITHOUT INCIDENT.  MAINTENANCEADJUSTED GROUND SHIFT ANTI-RETRACTION CABLE.  OPERATIONS CHECKED GOOD.  (X)


REMARKS:
DCA - FLT 516 - FLT EN ROUTE IAH TO PHL WHEN R1 WINDOW ARCED AND CRACKED, FLIGHT DIVERTED TO DCA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED R1 WINDOW.  (X)


REMARKS:
CHS - FLT 531 - FLIGHT EN ROUTE PBI TO PHL AT FL 370, WHEN NR 2 LOW OIL PRESSURE LIGHT CAME ON.  PRESSURE GAUGE INDICATED ZERO.  CREW SHUT DOWN NR 2 ENGINE AND DIVERTED TO CHS WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE DUE TO OPERATION AT ZERO OIL PRESSURE.  (X)


REMARKS:
IAH - FLT 54 - CLIMBING THROUGH 6,000 FEET, LOUD NOISE AND AIRFRAME VIBRATION OCCURRED.  FLIGHT RETURNED TO IAH WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE CHECKED FLIGHT CONTROLS, WING/BODY FAIRING HYDRAULIC LINES, ELEVATOR AND TAB, SPOILERS, AILERONS AND TABS.  RAN ENGINE FOR VIBRATION.  EVERYTHING CHECKED OKAY.  AIRCRAFT OKAY FOR SERVICE.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND CORROSION AT STA 945 AND LONGERON 28R IN SKIN.  CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04, FIGURE 12B, CLASS I REPAIR.  (X)


REMARKS:
DURING Q-2 CHECK, FOUND .3750 INCH CRACK IN LONGERON 17R JUST AFT OF STA 965.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
DURING Q-2 CHECK, FOUND .25 INCH CRACK IN SERVICE DOOR SUPPORT ANGLE AT STA 150, LONGERON 10R AREA.  INSTALLED DOUBLER REPAIR PER US AIR TYPICAL REPAIR 53-10-09.  (X)


REMARKS:
DURING Q-2 CHECK FOUND .3750 INCH CRACK AT LONGERON 17R AT STA 965.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
DURING Q-2 CHECK, FOUND CORROSION .070 INCH IN DEPTH RT INBD SEAT TRACK AT STA 203.  SPLICED IN SECTION OF SEAT TRACK PER SRM 53-04, FIGURE 5.  (X)


REMARKS:
DURING Q-2 CHECK, FOUND LEVEL I CORROSION AT LEFT LAV FLOOR BEAM AT STA 980 SCREW ATTACH HOLES.  REF CORROSION TASK NR C58-53300.  INSTALLED DOUBLER REPAIR AND REMOVED CORROSION - REPAIR INSTALLED PER SRM 53-05, FIGURE 20A.  (X)


REMARKS:
DURING Q-2 CHECK, FOUND .25 INCH CRACK AT HI-LOC IN LONGERON 17R JUST AFT OF STA 965.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
DURING Q-2 CHECK, FOUND A .045 INCH DEEP DENT AT STA 256 BETWEEN LONGERON 19R AND 20R.  INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-04, FIGURE 38.  (X)


REMARKS:
DURING Q-2 CHECK, INSPECTION, FOUND .6250 INCH CRACK STA 965, LONGERON 17L.  CUT DAMAGED SECTION AND SPLICED IN NEW SECTION OF LONGERON PER US AIR TYPICAL REPAIR 53-10-17.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND .8750 INCH CRACK STA 965 LONGERON 17L.  CUT OUT DAMAGED AREA AND SPLICED IN NEW SECTION OF LONGERON PER US AIR TYPICAL REPAIR 53-10-17.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION. FOUND .75 INCH CRACK STA 965 LONGERON 13R.  SPLICED IN NEW SECTION OF LONGERON PER US AIR TYPICAL REPAIR 53-10-17.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND A .75 INCH BY .8750 INCH X .079 INCH DEEP DENT STA 996 BETWEEN LONGERON 27L AND 27R IN FRAME WEB AND SUPPORT ANGLE.  CUT OUT DAMAGED AREA, INSTALLED NEW WEB AND SPLICED IN DOUBLER PER US AIR TYPICAL REPAIR 53-30-10.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND .25 INCH CRACK STA 69.5 UPPER NOSE SKIN FWD OF CAPT. WINDSHIELD.  PREVIOUS REPAIR INSTALLED.  REMOVED PREVIOUS REPAIR.  (PSE 53.09.029).  INSTALLED FLUSH REPAIR AFTER AREA WAS ROUTED OUT PER DACO SRO 9530239.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND .25 INCH CRACK STA 617 LONGERON 5L.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND .3750 INCH CRACK STA 680 LONGERON 6L.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND .3750 INCH CRACK STA 680 LONGERON 6R.  SPLICED IN NEW SECTION OF LONGERON PER US AIRTYPICAL REPAIR 53-10-17.  (X)


REMARKS:
DURING Q-2 CHECK INSPECTION, FOUND CORROSION AT STA 960 BETWEEN LONGERON 22L AND 23L BELOW OUTFLOW VALVE IN AFT CARGO COMPARTMENT.  REMOVED CORROSION AND INSTALLED INTERNAL FINGER DOUBLER AND EXTERNAL DOUBLER PER SRM 53-021, FIGURE 17, SHT2, AND US AIR EA NR 28117A.  (X)


REMARKS:
CLT - FLT 2291 - ON CLIMB-OUT CLT, NR 1 SLAT WOULD NOT RETRACT.  FLIGHT RETURNED TO FIELD WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANACE FOUND SLAT COCKED AND BOLT MISSING.  REALIGNED SLAT AND REPLACED MISSING BOLT.  (Z)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK IN DOUBLER BS 664 LBL 24 INCHES.  REPAIRED PER EO 5791G632.  (W)


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CRACKED, LOWER SIDE FROM BS 804 TO 809.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


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


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


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


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOP IN CABIN AREA AND AT RIGHT OVERWING EXIT.  REPLACEDEXIT LIGHTS AND BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATIONS AT BS 917, S4R, AT BS 420.5 AND 263, S10L, AT BS 320, S4R, AT BS 280, S14R, AT BS 510, S19R, AT BS 745, S20L, AND AT BS 777, 767, 787, 807, 817, 827, 490, 491, 500, 500+1, 500A+6 AND 847, STRINGER 4R.  REPAIRED PER TRAMCO EWO 94-1188.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATIONS AT BS 408, 420, 520, 570, 590,  591, 707,  AND 747, STRINGER 4R.  ALSO AT BS 500+13, 421, 494, 737, 916, 867, 500B, STRINGER 4L AND AT BS 520, 460, 480, STRINGER 14R, BS 470.5, AT S10L, AND AT BS 761, S20R.  REPAIRED PER TRAMCO EWO 94-1047.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATION AT BS 500B+.5, STRINGER 10L.  REPAIRED PER TRAMCO EWO'S 94-1047, 94-1172 AND 94-1192.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATIONS AT BS 368, 378, 388 AND 389, STRINGER 4R.  REPAIRED PER TRAMCO EWO'S 94-1047 AND 94-1173.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATIONS AT LOWER ROW OF FASTENERS AT BS 1007, 1014 AND 1013, STRINGER 4L.  REPAIRED PER TRAMCO EWO'S 94-1174 AND 1047.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATION AT LOWER ROW OF FASTENERS AT BS 786, STRINGER 20R.  REPAIRED PER TRAMCO EWO'S 94-1189, 94-1047, AND 94-1192.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATION AT BS 263, AT S10R.  REPAIRED PER TRAMCO EWO 94-1169.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATION AT BS 254, S19L.  REPAIRED PER TRAMCO EWO 94-1178.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATION AT BS 410, S19L.  REPAIRED PER TRAMCO EWO'S 94-1187 AND 94-1047.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATION AT BS 877.5, S10L.  REPAIRED PER TRAMCO EWO 94-1185.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT LOWER FASTENER HOLES AT BS 390.5, 399, 368.5, 380, 365.5, STRINGER 4L.  REPAIRED PER TRAMCO EWO'S 94-1184 AND 94-1047.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK EMITTING FROM STRINGER SPLICE FASTENER HOLE,  BS 907, S4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND STRINGER LOWER FLANGE CRACKED, BS 1012, S4L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION,  FOUND CRACK INDICATION AT LOWER FASTENER HOLES, BS 480 AND 481, STRINGER 4R.  REPAIRED PER TRAMCO EWO'S 94-1191 AND 94-1047.


REMARKS:
CLT - FLT 698 - FLIGHT EN ROUTE TPA TO PHL, WHEN RT WING BODY OVERHEAT LIGHT CAME ON IN FLIGHT, COULD NOT EXTINGUISH.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND OVERHEAT LOOPS M488 AND M1204 OUT OF LIMITS.  REPLACED LOOPS.  OPS CHECKED GOOD.  (W)


REMARKS:
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE OF FIRST CLASS CABIN INOPERATIVE.  RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT R2 DOOR.  SYSTEM GROUND CHECKED NORMAL OPERATION.  (W)


REMARKS:
EWR-ATL - FLT 19 - THE NR 1 ENGINE START VALVE LIGHT ILLUMINATED IN FLIGHT, FOLLOWED BY NR 1 ENGINE WARNING.  RETURNED EWR.  FOUND 13TH STAGE SADDLE DUCT CLAMP FOR CSD EJECTOR VALVE BROKEN.  REMOVED AND REPLACED CLAMP, RAN ENGINE, OPS CHECK OK PER 75-21.   REPLACED NR 1 ENGINE START VALVE ASSEMBLY, AND STARTER PRESS SWITCH.  OPS CHECK OK PER MM 80-10-01.  (W)


REMARKS:
LGW-BWI - FLT 195 - EN ROUTE, THE RT MID AND AFT RT LAVATORIES STOPPED WORKING.  THE CREW DECIDED TO RETURN TO LGW.  MAINTENANCE FOUND THAT BOTH REAR TANK SENSORS FAILED TO TEST.  BOTH SENSORS WERE CLEANED AND REPLACED.  SYSTEM WORKS SATISFACTORY.  (W)


REMARKS:
PHL - FLT 1789 - SHORTLY AFTER ROTATION, THE E/E COMPARTMENT DOOR INDICATEDOPEN, THE CREW RETURNED TO FIELD.  MAINTENANCE FOUND THE DOOR TO BE CLOSED.  THE DOOR SENSORS WERE CHECKED, AND THE ACFT WAS RELEASED.  (W)


REMARKS:
JAX-BWI - FLT 2101 - EN ROUTE, A P1 AIR LINE WAS LOST ON THE RT ENGINE.  THE ENGINE WOULD NOT PRODUCE FULL POWER.  THE CREW DECIDED TO DIVERT TO JAX.  NO FURTHER INCIDENTS WERE NOTED.  MAINTENANCE FOUND THE RT ENGINE P1 LINE TO HAVE A HOLEIN IT.  IT WAS REMOVED AND REPLACED.  NO LEAKS WERE NOTED.  OK FOR SERVICE.  (W)


REMARKS:
PIT - PASSENGER EMERGENCY EXIT LIGHT CIRCUIT BREAKER WOULD NOT RESET.  EXIT LIGHTS ON IN CABIN.  MAINTENANCE REPAIRED DAMAGED WIRE AT SEAT 5A.  (W)


REMARKS:
IN FLIGHT, NUMBER 1 ENGINE HYDRAULIC PUMP LOP LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED OVERHEAD CONTROL PANEL AND NUMBER 1 ENGINE 'A' SYSTEM HYDRAULIC PUMP PER BOEING M/M.


REMARKS:
IN FLIGHT, CAPTAIN'S HSI BECAME INOP, THEN HSI CIRCUIT BREAKER TRIPPED REMOVING POWER FROM SEVERAL INSTRUMENTS.  AIRCRAFT RETURNED TO SEA AND MADE AN UNEVENTFUL LANDING.  REPLACED CAPTAIN'S HSI PER BOEING M/M.


REMARKS:
DURING SCHEDULED B CHECK, FOUND A .75 INCH CRACK IN UPPER RADIUS OUTBOARD OF LOWER FWD CARGO DOOR FRAME.  REPAIRED PER SWA ACO 3194-52.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 18A CRACKED AT FASTENER LOCATION AT AFT END OF WHEEL WELL, BEHIND FIRE BOTTLE.  REPAIRED PER SWA RA 1-553-1222.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AREAS OF BARE METAL AND CORROSION AROUND NUTPLATES ON LOWER SIDE OF BEAM JUST BELOW WINDOW OF RIGHT OVERWING EXIT HATCH FRAME.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTS AT BS 427, STRINGER 16L, AT BS  384, STRINGER 17L, AT BS 500A, BETWEEN S26 AND 25R, AT BS 809, AT S16R, WL 217,  AND AT BS 311, BELOW S21R, WL 172.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LEFT WING NUMBER 2 FLAP TRACK FITTING ON REAR SPAR CORRODED.  REPLACED PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 312, LBL 60 - RBL 60, WL 208.  REPLACED UPPER CHORDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORROSION AROUND CLIP NUT HOLES AT BS 986, LBL 25 TO RBL 5.  REPLACED UPPER CHORD PER SWA RA 1-353-542 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME DAMAGE AT BS 727D, AT S20L, WL 182, LBL 57.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD GALLEY DOORWAY FRAME CRACKED IN RADIUS, BS 295.5, BETWEEN S6 AND 7R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, S10R, AT BS 663.75.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER S16R CRACKED AT BS 500B+8 AND +5.  REPLACED PER SWA ACO 6405-53.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY DOOR AND FLOOR TRACK LIGHTING INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND OUTSIDE AFT EMERGENCY LIGHTS ILLUMINATED WITH POWER OFF.  REPLACED AFT LEFT BATTERY POWER SUPPLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CABIN MID SECTION EMERGENCY LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND TWO LEFT CABIN EMERGENCY LIGHTS VERY WEAK.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN CEILING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AISLE EMERGENCY  LIGHTS FLICKERING WHEN LIGHTS SWITCHED OFF.  CHARGED FORWARD BATTERY PACK PER BOEING M/M.


REMARKS:
JFK - DURING CHECK C-3D, FOUND RT O/B TRAILING EDGE FLAP WEDGE DELAMINATED BETWEEN FLAP CANOES AND AT O/B END OF FLAP.REPLACED HONEYCOMB AND REPAIRED PER SRM 51-70-02 AND 51-50-05.  TOTAL CYCLES 10890.


REMARKS:
CLE - FLT 508 - DURING APPROACH, WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND.  CYCLED LANDING GEARAND LANDING GEAR EXTEND.  FOUND NOSE LANDING GEAR HYDRAULIC TRANFER CYLINDER (P/N 69-14106-5), BYPASSING HYDRAULIC PRESSURE.  REPLACED NOSE LANDING GEAR HYDRAULIC TRANDFER CYLINDER AND NOSE LANDING GEAR.  OPERATION CHECKED NORMAL.  CHECK C-2 - 9-18-94 - MCI.


REMARKS:
STL - DURING OP-15, FOUND CORROSION IN RT CANTED KEEL, STA 677 ON BOTTOM OF WING AT FUEL DRIPSTICK.  REPAIRED PER ARA 8165 AND SRM 57-03, FIG 26A SHT 1.  TOTAL CYCLES 39418.


REMARKS:
STL - DURING OP-15, FOUND A THREE INCH CRACK IN AFT LOWER CAST FITTING FRAME ATTACHMENT, STA 677.  REPAIRED PER SRM 51-30-3, 51-30-2, 51-30-5 AND 51-10-4.  TOTAL CYCLES 39418.


REMARKS:
STL - DURING OP-15, FOUND A ONE INCH CRACK IN TOP WEB ATTACH ANGLE ABOUT L30 BOTTOM OF CENTER FUEL TANK, STA 685.  REPAIRED PER ARA 6886.  TOTAL CYCLES 39418.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION ON FLOOR MEMBRANE AT FWD LT ENTRY DOOR THRESHOLD SUPPORT ANGLE.  REMOVED CORROSION PER SRM 51-10-03 AND INSTALLED DOUBLER PER SRM 53-01.  TOTAL CYCLES 17416.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION ON MEMBRANE UNDER FLOOR PANEL NR 12, FS 208 TO FS 242.  REMOVED CORROSION PER SRM  51-10-03 AND INSTALLED DOUBLER PER SRM 53-01 AND TWA STANDARD PRACTICES.  TOTAL CYCLES 17416.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION ON FUSELAGE SKIN UNDER FAIRING RUB STRIP, STA 760-780 AND STA 796-807, BETWEEN LONGERONS 27R AND 28R.  REMOVED CORROSION PER SRM 51-10-3 PAR 31-42, ADDED REPAIR DOUBLER PER ARA  8537.  TOTAL CYCLES 17416.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION AT FS 620, STRINGER 39L, AND STRINGER 39R CORRODED AND CRACKED.  REPAIRED PER SRM 53-00-03, PG 215 AND 53-00-02.  TOTAL CYCLES 10610.


REMARKS:
MCI - DURING CHECK C, FOUND CORROSION AT FS 960 FORMER FOOT, BETWEEN STRINGERS 47L AND 46L.  REMOVED CORROSION AND REPAIRED PER SRM 53-10-04, FIG 3A.  TOTAL CYCLES 17570.


REMARKS:
STL - FLT 488 - DURING CRUISE, LT MLG UNSAFE LIGHT ILLUMINATED.  RECYCLED LANDING GEAR.  REPLACED LT MLG DOWNLOCK SWITCH, (P/N H14-6).  LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL.  CHECK OP-16 - 1-12-94 - MCI.


REMARKS:
STL -FLT 844 - DURING APPROACH, WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR, AND FOUND LIGHT ASSEMBLY BASE (P/N 10648LD3), MALFUNCTIONING.  REPLACED LIGHT ASSEMBLY AND NOSE LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL.  CHECK C-9A - 11-30-94 - JFK.


REMARKS:
FLT 255 - DURING APPROACH, WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DOOR OPEN LIGHT REMAINED ON.  CYCLED LANDING GEAR, FOUND RT MLG DOOR PROXIMITY SWITCH TARGET MISSING.  INSTALLED A NEW PROIMITY SWITCH TARGET (P/N 3250-0032-01), AND LANDING GEAR DOOR OPEATION AND INDICATION CHECKED NORMAL.  CHECK OP-15 - 11-4-94 - MCI.


REMARKS:
MCI - DURING CHECK C, FOUND .75 INCH CRACK IN UPPER PRESSURE DECK, FS 269, RBL 18.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-211 PG 201A(3).  TOTAL CYCLES 43542.


REMARKS:
MCI - DURING CHECK C, FOUND THREE EACH .75 INCH CRACKS IN LT PRESSURE WEB, FS 293.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-211 PG 201A (3).  TOTAL CYCLES 43542.


REMARKS:
MCI - DURING CHECK C, FOUND A .75 INCH CRACK IN LT PRESSURE WEB, FS 243-21, BELOW PRESSURE DECK.  STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-10-211 PG 201 A(3).  TOTAL CYCLES 43542.


REMARKS:
MCI - DURING CHECK C, FOUND TWO EACH .75 INCH CRACKS IN RT PRESSURE WEB, FS 243, BELOW UPPER PRESSURE DECK.  STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-10-211 PG 201 A(3).  TOTAL CYCLES 43542.


REMARKS:
MCI - DURING CHECK C, FOUND TWO EACH .75 INCH CRACKS IN LT PRESSURE WEB OF NOSE LANDING GEAR WHEEL WELL, BELOW UPPER PRESSURE DECK, FS 264.  STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-10-211 FIG 201.  TOTAL CYCLES 43542.


REMARKS:
MCI - DURING CHECK C, FOUND CORROSION IN FUSELAGE SKIN AND CRACKS AT LOWER SKIN RIVET HOLE, STRINGER 19R, STA 400 TO 412.  REMOVED CORROSION AND REPAIRED PER SRM 53-30-3.  TOTAL CYCLES 43542.


REMARKS:
MCI - DURING CHECK C, FOUND A ONE INCH CRACK IN FUSELAGE SKIN AT RIVET, LOWER AFT CORNER OF RT FWD GALLEY DOOR OPENING. REPAIRED PER SRM 53-30-206, FIG 201.  TOTAL CYCLES 43452.


REMARKS:
MCI - DURING CHECK C, FOUND A CRACK 1.25 INCH LONG IN STA 870 BULKHEAD BELOW APU BLEED DUCT.  STOP DRILLED CRACK AND REPAIRED PER TWA DWG C03242.  TOTAL CYCLES 41752.


REMARKS:
MCI - DURING CHECK C, FOUND FUSELAGE SKIN CORROSION, STA 402 AND STA 433, STRINGER 19R.  REPAIRED CORROSION PER SRM 53-30-3.  TOTAL CYCLES 43452.


REMARKS:
MCI - DURING CHECK C, FOUND CORROSION ON LAP SEAM, STRINGER 19R, STA 360-500.  REPAIRED PER SRM 53-03-3, FIG 5.  TOTAL CYCLES 43452.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACKS EMITTING FROM FIVE RIVETS ON UPPER PRESSURE WEB, STA 285.5, BETWEEN LBL 0 THROUGH 10.  INSTALLED DOUBLER PER SRM 53-10-211 PG 211.  TOTAL CYCLES 44461.


REMARKS:
MCI - DURING CHECK C, FOUND .75 INCH CRACK AT FASTENER HOLE IN WHEEL WELL CEILING PRESSURE DECK OF NLG WHEEL WELL, BS 286, RBL 19.  STOP DRILLED AND INSTALLED DOUBLER PER SRM 53-10-211.  TOTAL CYCLES 41615.


REMARKS:
MCI - DURING CHECK C, FOUND .75 INCH CRACK AT FASTENER HOLE IN WHEEL WELL CEILING PRESSURE DECK OF NLG WHEEL WELL BS 278 RBL 19.  REPAIRED BY STOP DRILLING AND INSTALLING DOUBLER PER SRM 53-10-211.  TOTAL CYCLES 41615.


REMARKS:
MCI - DURING CHECK C, FOUND A TWO INCH CRACK IN WHEEL WELL CEILING PRESSURE DECK OF NLG WHEEL WELL, BETWEEN FASTENER BS264-266, RBL 14.  STOP DRILLED AND INSTALLED DOUBLER PER SRM 53-10-211.  TOTAL CYCLES 41615.


REMARKS:
FLT 57 - DURING APPROACH, WHEN LANDING GEAR WAS EXTENDED,C HYDRAULIC SYSTEM FLUID QUANTITY DEPLETED AND RT MLG ACTUATING CYLINDER (P/N 1535927-101), CRACKED.  REPLACED RT MLG ACTUATOR, REPLENISHED HYDRAULIC SYSTEM FLUID.  GROUND OPERATION OF LANDING GEAR CHECKED NORMAL.  CHECK C-9A - 11-30-94 - JFK.


REMARKS:
MCI - DURING CHECK C, FOUND A ONE INCH CRACK AT LOAD IN 870 BULKHEAD.  REPAIRED BY STOP DRILLING AND INSTALLED DOUBLER PER TWA DRAWING C03242.  TOTAL CYCLES 43542.


REMARKS:
NORMAL BRAKES ARE INEFFECTIVE ON LANDING.  BLED BRAKE CYLINDERS LT AND RT, OPERATIONAL CHECK GOOD.  ACFT RETURNED TO SERVICE.  (W)


REMARKS:
BWI - FLT 2142 - ON GEAR RETRACTION, LT GEAR RED LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION.  SAME INDICATION INOFF POSITION.  RECYCLED GEAR, ALL INDICATIONS NORMAL.  MAINTENANCE REPLACED LANDING GEAR ACCESSORY UNIT.  SWUNG GEAR NUMEROUS TIMES, ALL CHECKED GOOD.  (W)


REMARKS:
NOSE LANDING AND TAXI SWITCH IN GLARE SHIELD EXPLODED (SMOKE).  PULLED CIRCUIT BREAKERS K16 AND L16.  FOUND BAD HIGH BEAM TRANSFORMER.  REMOVED AND REPLACED TRANSFORMER PER MM CHAPTER 33-00.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM WEB GOUGED AND DAMAGED AT BS 620, RBL 25, WL 203.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
JFK - FLT 843 - RETURNED FROM FLIGHT ACCOUNT RT ENGINE INCURRED COMPRESSOR STALLS SHORTLY AFTER TAKEOFF.  ENGINE POWER REDUCED AND WAS NOT SHUT DOWN UNTIL AFTER LANDING.  INSPECTED ENGINE AND NO ANOMALIES WERE FOUND.  REPLACED ENGINE, TWA SN 4705, MFG. SN 724180-4060.  ENGINE TOTAL TIME:  6,107 HOURS; 2,731 CYCLES.  CHECK C-2D - 9-25-94 - JFK.  INVESTIGATION INTO COMPRESSOR STALLS AFTER TAKEOFF REVEALED NO OBVIOUS CAUSE OF THE STALLS.  ENGINE SN 4705, MFG. SN 724180-4060, REPAIRED BY PRATT AND WHITNEY TO INCORPORATE SB 72-514 SURGE IMPROVEMENT MODIFICATIONS.   (X)


REMARKS:
JFK - FLT 840 - RETURNED FROM FLIGHT ACCOUNT NR 3 ENGINE NACELLE TEMPERATURE IN OVERHEAT RANGE AT TAKEOFF THRUST.  TEMPERATURE RETURNED TO BOTTOM OF SCALE ON BOTH LOOPS WHEN POWER WAS REDUCED TO IDLE.  PRELIMINARY CHECKS INDICATE CASE AIR LEAKAGE.  REPLACED ENGINE SN 4198.  ENGINE TOTAL TIME 64,753.  ENGINE TOTAL CYCLES 11,929.  CHECK C-8B-3-21-94-JFK.  INVESTIGATION INTO NR 3 ENGINE NACELLE TEMPERATURE OVERHEAT REVEALED HIGH STAGE PNEUMATIC BLEED VALVE, MFG. PN 737109-7, FAILED IN OPEN POSITION CAUSING AN OVERPRESSURE IN HIGH PRESSURE DUCTING, CAUSING OVERHEAT CONDITION.  ENGINE SN 4198 REPAIRED AND RETURNED TO SERVICE.  (X)


REMARKS:
FLT 98 - INVESTIGATION INTO STALL AND HIGH VIBRATION IN ENGINE SN 99918 REVEALED FIRST STAGE TURBINE BLADE, MFG PN 836201-001, FRACTURED RESULTING IN TURBINE DAMAGE.  ENGINE SN 99918 WAS REPAIRED AND RETURNED TO SERVICE.  (X)


REMARKS:
STL - FLT 427 - INVESTIGATION OF ENGINE (S/N 3236) LOSS OF POWER DURING CLIMB, REVEALED THIRD STAGE TURBINE BLADE, MFG (P/N 798403), FRACTURED RESULTING IN TURBINE DAMAGE.  ENGINE 3236 WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
CDG - FLT 885 - DURING TAKEOFF, NR 2 ENGINE, SN 4118, HAD HIGH EGT AND NOISE.  SHUT DOWN NR 2 ENGINE PER CHECK LIST.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED NR 2 ENGINE, GROUND OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  67,233 HOURS; 24,478 CYCLES,  CHECK C-5A - 3-1594 - JFK.  INVESTIGATION INTO THE SHUT DOWN OF ENGINE, SN 4118, REVEALED A STAGE 2TURBINE VANE, MFG PN 769892, SUFFERED BURNING CAUSING STAGE 2 TURBINE BLADE, MFG PN 770102, TO FAIL AT THE AIRFOIL TO ROOT PLATFORM RADIUS.  ENGINE, SN 4118, WAS REPAIRED AND RETURNED TO SERVICE.  (X)


REMARKS:
JFK - DURING C-CHECK, FOUND 13 INCH CRACK ON Z-RING, LEFT SIDE, 11 O'CLOCK POSITION, THIRD RING FROM BOTTOM, FORWARD OFOLD REPAIR INSIDE S-DUCT.  STOP DRILLED CRACK AND INSTALLED Z-FRAME REPAIR PER SRM 54-26-00, PAGE 805.  TOTAL CYCLES 22,401.


REMARKS:
JFK - FLT 840 - AT TOP OF CLIMB, NR 3 ENG HAD POWER LOSS WITH VIBRATION.  FND METAL IN TAILPIPE.  REPLACED ENG, SN 4192.  ENG TT:  72,686 HRS; 14,147 CYCLES.  CHECK C-7B - 2-22-94 - JFK.  INVEST INTO NR 3 ENG, SN 4192, POWER LOSS & VIB, REVEALED 2 2ND STAGE TURB NOZZLE GUIDE VANES LOCATED AT 6 O'CLOCK POSITION, SUFFERED BURN-THRU ALONG T/E.  THIS CAUSED UNUSUAL LOADING OF 2ND STAGE TURB BLADES LEADING TO FAILURE OF 1 BLADE AT AIRFOIL ROOT.  REMAINING 2ND STAGE BLADES BATTERED & BROKEN.  DOWNSTREAM DAMAGE OF AIRFOIL BATTERING & TEARING EVIDENT IN STAGES 3 THRU 6.  ENG MODULES CHANGED OR REPAIRED IAW OPER SPECS & J59D-7AH ENG MAN.  2ND STAGE TURB VANE MFG PN 794782.  2ND STAGE TURB BLADE, MFG PN 770102.


REMARKS:
BOS - FLT 1989 - DURING CLIMB-OUT, NR 2 IRS DC FAIL ILLUMINATED.  TWO MINUTES LATER NR 1 DC FAIL LIGHT ILLUMINATED.  THE BATTERY VOLTAGE WAS 17 VOLTS.  FLIGHT RETURNED TO BOS WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED SHIP'SBATTERY CHARGER.  REF USAA940786.


REMARKS:
PHL - THE L3 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE CHARGER AND BATTERY PACK. REF USAA941181.  (W)


REMARKS:
AFTER TAKEOFF, EXPERIENCED NUMBER 1 ENGINE FLAMEOUT.  AIRCRAFT RETURNED TO AMA AND MADE AN UNEVENTFUL LANDING.  ENGINE REMOVED AND SHIPPED TO DAL.  SUSPECT ENGINE TRANSFER GEARBOX OR RADIAL DRIVE SHAFT FAILURE.  NUMBER 1 ENGINE REPLACED AND RUN UP PERFORMED PER BOEING M/M.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND UPPER HINGE CUTOUT ON FWD ENTRY DOOR CRACKED IN UPPER CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
CLT - THE EMERGENCY FLOOR LEVEL AND EXIT LIGHTING FOUND TO BE INTERMITTENT WITHOUT REGARD TO COCKPIT OR CABIN SWITCH POSITIONS.  FOUND AC SENSING RELAY LV997 BAD.  REPLACED SAME.  OPERATION CHECKS.  (W)


REMARKS:
PIT - DURING HEAVY MAINTENANCE SIP VISIT ACCOMPLISHED PCI 584 JOB CARD NR JE-42-53528, FOUND .25 INCH CRACK LT AFT CORNER OF NOSE LANDING GEAR TOP BAY COVER.  HFEC INSPECTION.  (W)


REMARKS:
PIT - DURING HEAVY MAINTENANCE SIP VISIT ACCOMPLISHED PCI 1492 JOB CARD NR JE-50-53502, FOUND .25 INCH CRACK IN THE AFTTOP CORNER OF THE DOOR OPENING.  VISUAL INSPECTION.  ROUTED OUT CRACKED SKIN AND INSTALLED PLUG AND 2 DOUBLERS PER SRM 53-02-16.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHES CORRODED AREA.  BS 500 PLUS 4 INCHES RBL 16 CARGO BAY FWD.  REPAIRED PER SRM 53-10-5 FIG 11.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 20 INCHES CORROSION AREA ON TOP OF FLOOR BEAM CAP, BS 259 LBL10 TO RBL 10.  REPAIRED PER EA 38173.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 4 INCHES BY 20 INCHES CORRODED AREA STA 380 TO 420 S-26 R.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHES CORRODED AREA LT FWD CARGO STA 380 BETWEEN S-26 L AND S-25 L.  REPAIRED PER SRM 51-40-03.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 CRACKS IN SKIN OF FWD PRESSURE BULKHEAD 178 RBL 5, 1 INCH LONG AT WL 202, AND 1,5 INCH LONG AT WL 198.  REPAIRED PER TR 53-10-11.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHES CORRODED TOP SIDE SEAT TRACK BS 937 LBL 48 INCHES.  REPAIRED PER SRM 10-05 FIG 2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 1.50 INCH CORROSION TRANSITION ANGLE BS 851 S-26 R.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCHES BY 2.50 INCHES CORROSION AROUND SCREW HOLES IN TRANSITION ANGLE BS 727 A TO 787.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2.25 INCHES FLOOR ATTACH ANGLE CORRODED, BS 380 S-26 L TO S-26 R.  REPAIRED PER DRAWING 65-53880.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 3 INCHES LONG, 1 INCH WIDE STRINGER BS 907 S-27 R.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOOR TO WALL ANGLE 3 INCHES BY 4 INCHES.  ALSO, FOUND CRACK .50 INCH, BS 380 BETWEEN S-26 L AND S-25 R.  REPAIRED PER SRM 51-40-2.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .75 INCH BY 8 INCHES AND .50 INCH BY 10 INCHES CORROSION BS 727 THROUGH948 LT SIDE AFT CARGO BIN.  REPAIRED PER SRM 51-10-1 PG 5.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 1 INCH LONG CORRODED AREA ON STRINGER SPLICE BS 907 S-27 L. REPAIRED PER SRM 51-40-03.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCHES CORROSION S-27 L AT BS 1016.  REPAIRED PER SRM 53-10-3 FIG 1 SRM 53-10-2 SRM 53-10-3 FIG 6.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING C CHECK VISUAL INSPECTION, FOUND CORROSION 10 INCH BY 3 INCH AREA, BS 967 TO BS 977 BELOW S-20 L.  REPAIRED PER 737 SRM 53-30-3.  CORROSION TASK NR C53-100-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING C CHECK VISUAL INSPECTION, FOUND SKIN BULGE 6 INCHES LONG STA 526 AT STR 28 L.  REPAIRED PER DRAWING 65-62125 AND SRM 53-10-3.  CORROSION TASK NR C53-100-01.  CORROSION LEVEL 2.  (W)


REMARKS:
GSO - DURING A CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 2 INCH SQUARE CORROSION 1.5 INCH CRACK (SAME AREA) STA 384 AND 1.5 INCH ABOVE STR 19 R (LAP SEAM).  REPAIRED PER SRM 53-30-3.  CORROSION LEVEL 2.  (W)


REMARKS:
GSO - DURING A CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1 INCH CRACK AFT CARGO DOOR CUTOUT SKIN AT LOWER FWD CORNER RADIUS.  REPAIRED PER SRM 53-30-03 FIG 8.  (W)


REMARKS:
INT - DURING A CHECK VISUAL EDDY CURRENT AND ULTRA SOUND INSPECTION, FOUND DISBOND BY 8 INCHES BY 3 INCHES STA 1016 R JUST ABOVE STR 4 R AT BUTT JOINT.  REPAIRED PER EA 28667.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND LEVEL I CORROSION (TASK NR C58-5330) PREVIOUSLY REWORKED AT RT LAVATORY FLOOR BEAM AT STA 996 UPPER SURFACE AND SCREW HOLES.  CUT OUT CORRODED AREA AND INSTALLED REPAIR ANGLES PER USAIR TYPICAL REPAIR NR 53-10-14.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND 2 INCH CRACK IN CANTED FRAME STA 1074 AT ATTACHMENT TO LONGERON 6L.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 30.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND 1 INCH CRACK IN CUSP MEMBRANE RT SIDE STA 598.  SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 96.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND .8750 INCH CRACK IN CUSP MEMBRANE RT SIDE STA 615.  SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 96.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND 2 INCH CRACK IN FRAME 1076 AT ATTACHMENT TO LONGERON 2L.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 31.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND 1 INCH BY .75 INCH DENT IN LT WING I/B LE PANEL AT WS 4000.  REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-40-02.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND 60 MM (2.50 INCHES) OF CORROSION IN FL0OR BEAM BETWEEN STA 4175 AND STA 4610.  REMOVED DAMAGED AREA AND INSTALLED SPLICE REPAIR PER USAIR EA 28593.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND 2 DENTS, 2 INCHES BY 2 INCHES AND 2 INCHES BY 4 INCHES.  ALSO,FOUND A CRACK .50 INCH IN PAX DOOR LOWER AFT CORNER FRAME AT STA 4765.  REPAIRED DENTED AREA AND CRACKED AREA WITH NEW SECTION OF SKIN PER USAIR EA NR 28433.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND 18 BOLT HOLES MISALIGNED (INTERFACE PROBLEM) AT LT AND RT FRAME STA 17011.  INSTALLED NAS1581A3T COUNTERSUNK BOLTS PER USAIR EA 28592.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND DEBOND CONDITION 21.50 INCHES BY 15.50 INCHES RT STUBWING I/B FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611 BETWEEN STRINGER 53A AND 51.  INSTALLED DOUBLER REPAIR PER USAIR EA 28432.(W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND DEBOND/OVERHEAT CONDITION 13.25 INCHES BY 21 INCHES LT STUBWING I/B FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611 BETWEEN STA 21A AND 24.  REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER USAIR EA 28432.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND DENTS 4 INCHES BY 8 INCHES AND 1 INCH BY 2 INCHES IN THE LT FUSELAGE BETWEEN STA 5805 AND 6305 AT WL 560.  REMOVED DAMAGED AREA AND INSTALLLED FILLER AND DOUBLER REPAIR PER USAIR EA 28434.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q CHECK INSPECTION, FOUND CRACKS AND BENT RIBS 1825 AND 2635 IN RT WING.  REPAIR DAMAGEDRIBS PER FOKKER AIRCRAFT SERVICES REPORT G100A-00-8117/FAS-S-141 AND USAIR EA NR 28662.  (W)


REMARKS:
CLT - FLT 2134 - ENROUTE, BWI TO TPA WHEN AT FL 310 FIRST OFFICER'S WINDSHIELD CRACKED.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED FIRST OFFICER'S WINDSHIELD.  (W)


REMARKS:
SFO - FLT 8050 - ON TAKEOFF ROTATION, DOOR LIGHT CAME ON AND ACFT WOULD NOT PRESSURIZE.  FLIGHT RETURNED TO SFO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE READJUSTED AND RIGGED L1 DOOR ASSEMBLY.  PRESSURIZED ACFT, FOUND SATISFACTORY. (W)


REMARKS:
LAX - FLT 53 - LEFT GEAR RED LIGHT REMAINED ON AFTER RETRACTION.  CYCLED GEAR AND LIGHT WENT OUT.  MAINTENANCE PERFORMED GEAR SWING, SATISFACTORY.  (W)


REMARKS:
PHL - FLT 1066 - WHEN GEAR WAS LOWERED FOR LANDING, THERE WERE NO RED OR GREEN GEAR LIGHT INDICATIONS WITH LIGHTS DIM.PLACED LIGHTS TO BRIGHT AND INDICATION WAS NORMAL.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED ANNUNCIATOR DIMMING MODULE.  OPS CHECK GOOD.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION OVER 1 INCH BY 48 INCH AREA, FWD CARGO, STA 500 D LBL24 TO RBL 24.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-208-2.  CORROSION LEVEL 2.  (W)


REMARKS:
CLT - FLT 221 - THE EMERGENCY LIGHTING IN ROWS 11-20 WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
ORD - FLT 907 - THE CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AND BATTERY FOR ROW 3 AND ROW 8 RT SIDE.  ALSO, REPLACED BATTERIES FOR POWER SUPPLY B5 IN CENTER CABIN CEILING.  ALL EMERGENCY LIGHTS CHECK SATISFACTORY.  (W)


REMARKS:
PIT - FLT 309 - AIR TRAFFIC CONTROL ADVISED THAT DURING TAKEOFF SPARKS WERE SHOOTING OUT OF THE RT ENGINE.  THE CREW DECIDED TO RETURN TO PIT.  MAINTENANCE REPLACED THE RT ENGINE ASSEMBLY.  (W)


REMARKS:
PIT - FLT 233 - ON DEPARTURE WHILE CLIMBING THROUGH 6000 FEET, WHEN THE CAPTAIN ADJUSTED THE THROTTLES TO CLIMB POWER THE LT ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED.  AN ABNORMAL CHECK LIST WAS INITIATED AND AN ENGINE SHUTDOWN PROCEDURE WAS ACCOMPLISHED AS A PRECAUTIONARY.  THE CREW RETURNED TO PIT WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LT ENGINE OIL FILTER.  THE ENGINE WAS RUN AND THE CLOG LIGHT EXTINGUISHED.  THE ENGINE OIL TEMPERATURE AND PRESSURE WERE NORMAL.  (W)


REMARKS:
CLT - FLT 395 - ON TAKEOFF, A VERY STRONG SMELL CAME INTO THE COCKPIT AND CABIN.  THE ODOR WAS REPORTED AS A RUBBER OR ELECTRICAL SMELL.  THE CREW RETURNED TO CLT AS A PRECAUTIONARY.  MAINTENANCE INSPECTED THE BAG BINS, TAILCONE AREA, WHEEL WELL AREA, ENGINE INTAKES/EXHAUST AND CABIN FLIGHT DECK.  THERE WAS NO INDICATION OF SMOKE AND VERY LITTLE ODOR.  THE PACKS WERE OPERATED AT VARIOUS TEMPERATURES WITH NO UNUSUAL ITEMS.  SUSPECT ODOR PULLED INTO PACK SYSTEM.  ACFT OK FOR SERVICE.  (W)


REMARKS:
CLT - FLT 1863 - ON APPROACH, THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE.  WHEN THE GEAR HANDLE WAS LOWERED THERE SEEMED TO BE A WHINING NOISE AS THE NOSE GEAR TRIED TO COME DOWN.  THE RED LIGHT DID NOT ILLUMINATE EITHER.  THE GEAR WAS RECYCLED AND OPERATIONS WERE GOOD.  MAINTENANCE JACKED THE ACFT AND CYCLED THE NOSE GEAR SEVERAL TIMES.  NO WHINING NOISEWAS NOTED.  ALL INDICATIONS CHECKED GOOD.  ACFT OK FOR SERVICE.  (W)


REMARKS:
MSP - FLT 232 - AFTER TAKEOFF, THE REDLIGHT FOR THE NOSE GEAR INDICATION DID NOT ILLUMINATE.  THE GEAR WOULD NOT RETRACT.  THE GEAR WAS RECYCLED TWICE WITH NOSE GEAR UNSAFE LIGHT STILL ON.  THE CABIN PRESSURE WAS DUMPED, AND CREW RETURNED TO MSP.  ON ARRIVAL, THE NOSE STRUT WAS FOUND TO BE FLAT.  MAINTENANCE SERVICED THE NOSE GEAR STRUT.  NO LEAKS WERE FOUND.  THE NOSE STRUT CHECKED OK.  (W)


REMARKS:
CLT - FLT 1541 - THE FWD SECTION OF THE FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED A SHORTED LIGHT AT THE FWD FLIGHT ATTENDANT SEAT.  OPERATIONAL CHECKS OK.  (W)


REMARKS:
CLT - FLT 1760 - DURING FLIGHT, THE LT CSD LOW OIL PRESSURE LIGHT ILLUMINATED.  THE CSD WAS DISCONNECTED AS PER PROCEDURES.  THE CREW RETURNED TO CLT.  MAINTENANCE FOUND THE CSD OIL TO BE LOW AND SERVICED.  ALL WIRING WAS INSPECTED.  NO DEFECTS WERE FOUND.  THE ENGINE WAS RUN AFTER RECONNECT AND FULLY  LOADED GENERATOR.  VOLTS AND FREQUENCY CHECKED GOOD.  ACFT OK FOR SERVICE.  (W)


REMARKS:
PIT - FLT 919 - THE FLOOR LEVEL LIGHTS IN THE FWD CABIN WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE FWD EMERGENCY PACK POWER SUPPLY.  LIGHT OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
PHL-MCI - FLT 65 - EN ROUTE, WHEN FUEL LEAK WAS SUSPECTED FROM LT WING.  FLIGHT DIVERTD TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE INSTALLED 6 HYLOCKS ON LT TANK.  SEALED HYLOCKS, AND LEAK CHECKED OK.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 25 INCHES BY .50 INCH CORROSION UP TO .075 INCH DEEP, BS 500 D PLUS 4 TO 525 RBL.  REPAIRED PER EA 38316.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 17R UPPER FLANGE TO BULKHEAD CLIPSTA 980.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND A 2.25 INCH CRACK LT SIDE HORIZONTAL STAB LOWER SPAR CAP AT STA XHS-193.  FABRICATED AND INSTALLED ANGLES 3-5-7-9 PER USAIR EA 28365.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND 3 INCH CRACK LT DORSAL FIN ATTACH ANGLE.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 23 AND 23A.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND .8750 INCH CRACK RT DORSAL FIN ATTACH AT STA 1121.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 23 AND 23A.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND .3750 INCH CRACK IN RT PYLON UPPER DRAG ANGLE.  INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 6R AT LOWER ATTACH POINT STA 639. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-03 FIG 2.  (W)


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD GALLEY INTERCOSTAL BETWEEN BS 294.5 AND BS 312 CORRODED AT INBOARD FLANGE.REPAIRED PER SWA RA 1-553-227.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD GALLEY FLOOR BEAM CORRODED AT BS 344, LBL 9 AT AFT FLANGE.  REPAIRED PER SWA RA 1-553-1225.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD GALLEY FLOOR BEAM CORRODED AT BS 294.5, RBL 31 AND 39.  REPAIRED PER SWA RA1-553-1226.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT WING L/E SKIN CRACKED AT NR 4 SLAT OUTBOARD AUXILIARY TRACK CUTOUT.  REPAIREDPER SWA RA 1-257-254.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND NR 2 PYLON FIXED L/E LOWER PANEL CRACKED AT LOWER EDGE.  REPAIRED PER SWA RA 1-357-260.


REMARKS:
DURING DESCENT, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY DISPLAYED ZERO.  ENGINE TEMPERATURE REMAINED IN NORMAL RANGE.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT LANDED WITHOUT INCIDENT AT SEA.  INSPECTED AND FOUND OIL PRESSURE TRANSMITTER ELBOW FITTING CRACKED.  REPLACED FITTING, OIL SERVICED ENGINE, AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
EXPERIENCED LOUD BANG FROM NR 2 ENGINE.  EPR DROPPED SLIGHTLY WITH A SLIGHT RISE IN EGT, BUT STILL WITHIN GREEN BAND.  FUEL FLOW LESS THAN NR 1 ENGINE.  CREW DID NOT PERFORM ENGINE SHUT-DOWN.  AIRCRAFT LANDED WITHOUT INCIDENT.  INSPECTED ENGINE AND DETERMINED COMPRESSOR STALL.  REPLACED NR 2 ENGINE FOR MAINT CONVENIENCE AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND DEBONDED SKIN AT RT STUBWING I/B SKIN BETWEEN FRAMES STA 24011 AND 24611, STR 52 AND 53.  REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLERS PER USAIR EA NR 28034.  (W)


REMARKS:
DURING Q-1 CHECK INSPECTION, FOUND DEBONDED SKIN AT LT STUBWING I/B SKIN BETWEEN FRAMES STA 24011 AND 24611, STR 23 AND21A DEBOND AREA 21 INCHES BY 13.23.  REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER USAIR EA 28034.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND 40 INCH AREA OF CORROSION AT FLOOR BEAM BL 600L BETWEEN STA 3857 AND 4875.  REMOVED AND REPLACED FLOOR BEAM SECTION PER SRM 51-40-02 AND 51-41-01.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND 20 INCH SQUARE OF CORROSION IN FWD GALLEY FLOOR BEAM BLO BETWEEN STA 3845 AND 5805.  REMOVED AND REPLACED FWD SECTION IAW 51-40-02 AND 51-41-01.  (W)


REMARKS:
DURING Q-1 INSPECTION, FOUND 1 INCH BY 22 INCHES DELAMINATION, AND 2 INCH CRACK IN THE LT I/B FLAP TE.  REMOVED DAMAGEDAREA, INSTALLED NEW CORE AND DOUBLER REPAIR PER SRM 51-70-10 AND 51-70-11.  (W)


REMARKS:
MSY/ATL - FLT 160 - AFTER TAKEOFF, EXPERIENCED TWO LOUD BANGS AND VIBRATION FROM NR 1 ENGINE.  SHUT DOWN ENGINE AND RETURNED TO MSY, INSPECTION REVEALED FEATHERS AND BIRD CARCASS IN INLET.  ENGINE MUST BE REPLACED.  REMOVE AND REPLACED NR 1 ENGINE.


REMARKS:
ALT/MDW - FLT 79 - ON DESCENT TO MDW, PRECAUTIONARY SHUT-DOWN OF NR 3 ENGINE DUE TO LOW OIL PRESSURE, ZERO QUANTITY ANDRISING TEMP, MAX TEMP WAS 110 DEGREES OIL TEMPERATURE WINDMILLED 14 MINUTES,  ZERO OIL PRESSURE.  LOWER BUSHING WORN AWAY AT OIL FILTER HOUSING.  REMOVED AND REPLACED WORN BUSHING AND O-RING, REMOVED AND REPLACED OIL FILTER.  NO FOD FOUND. PER MM 72-00, PAGE 518D & MM 79-15-00, SERVICED OIL TANK.  OPS CHECK OKAY, NO LEAKS, PRESSURE AND QUANTITY OKAY.  (X)


REMARKS:
DURING Q-1 INSPECTION, FOUND STRINGER 68 RT SIDE CRACKED THROUGH AT STA 3876.  REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN NEW PER SRM 51-70-02.  (W)


REMARKS:
CMH - FLT 976 - DURING FLIGHT, THERE WAS VIBRATION FROM THE NR 2 ENGINE.  THROTTLE WAS RETARDED WITH NO CORRECTION.  THE NR 2 ENGINE WAS SHUTDOWN.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 ENGINE.  INSPECTED INSTALLATION OF NR 2 ENGINE ASSEMBLY AS PER JOB CARD J571-00-1.  (W)


REMARKS:
EXPERIENCED NUMBER 1 ENGINE FLAMEOUT.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND AFT TURBINE SECTION DAMAGE.  REPLACED ENGINE ASSEMBLY AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
DURING CLIMB AT 5000 FEET ACFT WOULD NOT PRESSURIZE.  AIRCRAFT RETURNED TO ATL SAFELY.  MAINTENANCE RESET OUTFLOW VALVE5 AMP CIRCUIT BREAKER AND PRESSURIZED ON GROUND.  OPS CHECK GOOD PER MM 21-30-00.


REMARKS:
MCI - DURING OP-17, FOUND LEFT FUSELAGE SKIN WORN, STATION 720D AND 720E, STRINGER 19L.  REPAIRED PER ARA 8966.  TOTAL CYCLES 23,610.


REMARKS:
MCI - DURING OP-17, FOUND CREASE IN SKIN BELOW STRINGER 17L, STATION 480 TO 520.  REPAIRED PER SRM 53-30-3, FIGURE 2 AND TWA STANDARD PRACTICES.  TOTAL CYCLES 23,601.


REMARKS:
MCI - DUIRNG OP-17, FOUND CORROSION ON FUSELAGE SKIN BETWEEN STRINGERS 30R AND 29R, STATION 990-1010.  REPAIRED PER SRM53-30-3, FIGURE 3A, SHEET 3.  TOTAL CYCLES 23,610.


REMARKS:
PIT - FLT 2050 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANACE FOUND RIGHT AFT SERVICE DOOR FALSE LOCKED.  RECYCLED DOOR.  OPS CHECK NORMAL.  (Z)


REMARKS:
PBI - FLT 96 - PBI TO MDW, ON TAKEOFF AFTER GEAR UP, LOUD POP FOLLOWED BY ACRID SMELL, SUSPECTED POSSIBLE FIRE AND STABCONTROL ACTUATOR CIRCUIT BREAKER TRIPPED, RETURNED TO PBI.  FOUND STAB TRIM CONTROL RELAY BAD, REMOVED AND REPLACED RELAY, OPS CHECK NORMAL PER MM 27-40, PAGE 501.  (X)


REMARKS:
STL - INVESTIGATION INTO ENGINE S/N 1501, SHUTDOWN DUE TO HIGH VIBRATION, REVEALED NR 3 BEARING, MFG P/N 804059, CAGE BREAK.  REWORKED RELATED COMPONENTS.  ENGINE S/N 1501 REPAIRED AND RETURNED TO SERVICE.


REMARKS:
LAX - FLT 816 - THE EMERGENCY LIGHTS ON ROWS 3, 4, 5, AND 6 WERE FOUND TO BE INOPERATIVE.  MAINTENANCE FOUND A WIRE PUSHED BACK ON THE EMERGENCY LIGHTS AND REPOSITIONED THE WIRE.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-2 CHECK, INSPECTION FOUND 4 INCH CRACK BETWEEN STA 598 AND 617 SIDE O/B OF SEAT TRACK IN CUSP MEMBRANE.  MANU NEW SECTION OF MEMBRANE WEB AND SPLICED IN PER SRM 53-05 FIG 96.  (W)


REMARKS:
PIT - FLT 580 - ON APPROACH, THE NOSE GEAR AND RT LANDING GEAR LIGHTS DID NOT ILLUMINATE.  THE GEAR WAS RECYCLED AND THEN THE GREEN LIGHTS ILLUMINATED NORMALLY.  MAINTENANCE ACCOMPLISHED BITE TEST ON THE PSEU.  ALL GEAR INDICATION INPUT SWITCHES AND SENSORS CHECKED NORMALLY.  ALL THREE GEAR POSITION LIGHTS CHECKED NORMAL.  THE PSEU WAS REPLACED AS A PRECAUTION.  (W)


REMARKS:
DURING SCHEDULED 1/4 D CHECK, FOUND SEVERALS CRACKS EXTENDING FROM UNDER RIVET HEADS AT FWD SIDE OF PRESSURE BULKHEAD AT BS 178, LBL 6 AND WL 183.0.  REPAIRED PER SWA RA 1-253-1236.


REMARKS:
DURING SCHEDULED QUARTER D CHECK, FOUND MANY CRACKS EXTENDING FROM THE INBOARD VERTICAL ROW OF BULKHEAD FASTENER HOLES,LBL 5.25 AND WL 185.5.  REPAIRED PER SWA RA 1-253-1236.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CORRODED AT BS 727D, RBL 16, WL 150.  REPLACED PER BOEING STRUCTURAL REPAIR MANAUL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 885, BETWEEN S19 AND 20R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANAUL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 294.5, LBL 11 TO RBL 45.  REPAIRED PER SWA RA 1-353-418.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SKATE ANGLE CRACKED AT BS 570, WL 158, LBL 50.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINTENANCE CHECK, FOUND CRACK IN WEB AT BS 726, S18A, LEFT SIDE.  REPAIRED PER SWA RA 1-553-1222.


REMARKS:
FOUND SEVERAL CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED FORWARD RIGHT BATTERY CHARGER PER BOEING M/M.


REMARKS:
DURING SCHEDULED B1 CHECK, FOUND TWO GOUGES ON FUSELAGE SKIN AT BS 380, AT WL 208 AND 216.  REPAIRED BOTH PER BOEING STRUCTURAL RPAIR MANUAL.


REMARKS:
CLT - FLT 730 - AT 33,000 FEET, THE FIRST OFFICER WINDSHIELD CRACKED.  THE CAPTAIN DESCENDED TO 10,000 FEET TO TAKE THEPRESSURE OFF.  THE ACFT REMAINED AT 10,00 FEET AND DIVERTED TO CLT WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE WINDSHIELD AND THE TEMPERATURE CONTROLLER.  OPERATIONS CHECKED GOOD.  REF USAA941374.


REMARKS:
BWI - FLT 2180 - FLIGHT EN ROUTE PBI-LGA FMC FAILED, FOLLOWED BY FAILURE OF C/O ADI THEN FAILURE OF NR 2 ADI.  FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED FMC COMPUTER.  OPS CHECK GOOD.  NO FAULTS NOTED.  (W)


REMARKS:
BWI - COCKPIT EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WHEN TESTED.  MAINTENANCE REPLACED BATTERIES.  OPS CHECKS OK.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK (VISABLE) FS 695 LOWER FRAME FITTING.  PART REPLACED 65-51657-7 AND 65-51656-7.  (W)


REMARKS:
PIT - DURING Q-3 CHECK, INSPECTION FOUND .5 INCH CRACK IN FRAME AT END OF FLOOR BEAM ABOVE CARGO DOOR OPENING AT STA 408 BETWEEN LONGERON 18R AND 19R.  REF SID PSE 53.09.001A.  REMOVED AND REPLACED FRAME PER DACO BLUEPRINT.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .4375 INCH CRACK IN FRAME AT O/B END OF FLOOR BEAM STA 389 JUST BELOW BEAM NEAR LONGERON 19R REF SID PSE 53.09.001A.  REMOVED AND REPLACED FRAME PER DACO BLUEPRINT.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .0937 CRACK IN THE LT AFT OVERWING EMERGENCY EXIT WINDOW DOOR JAMB.  INSTALLEDDOUBLER REPAIR PER SRM 53-05 FIG 32.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTIN, FOUND 8 INCH CRACK AFT PAX ENTRANCE DOOR JAMB THROUGH RADIUS NEAR TO RT SIDE.  INSTALLED SRM REPAIR 53-05 FIG 30, 53-11-3 FIG 6A, 51-60 FIG 19 AND USAIR EA NR 28827.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND CRACK RADIATING FROM LIGHTNING HOLE OF FRAME WEB AT STA 1038 AND LONGERON 11R,.5 INCH IN LENGTH.  INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2 SHT 3.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.25 INCH CRACK AT STA 1046 LT VERTICAL STAB ATTACH ANGLE.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 84. (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK IN CANTED FRAME STA 1104 AT LONGERON NR 4 AND NR 5L.  SPLICED IN NEW SECTION OF FRAME PER SRM 53-03 FIG 30.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND A CONVEXED DENT AND .125 INCH CRACK IN THE FUSELAGE SKIN STA 560 LONGERON 30.INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 38.  (W)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH LONG, .020 DEEP GOUGE IN THE FUSELAGE SKIN AT STA 832 JUST I/B OF LONGERON 29L.  INSTALLED INTERNAL DOUBLER REPAIR PER SRM 53-04 FIG 38 SHT 17.  (W)


REMARKS:
CLT - FLT 1740 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT FLT 51 - AFTER ADVANCING THE THROTTLES FROM IDLE TO APPROXIMATELY 1.6 EPR, THE LT ENGINE SHUT ITSELF DOWN.  THIS OCCURRED AT 10,000 FEET.  THE ACFT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LT ENGINE FUEL PUMP.  LEAK AND OPERATION CHECKED GOOD.  (W)


REMARKS:
PIT - THE EMERGENCY FLOOR TRACK LIGHTING FROM ROW 6 FWD WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
GS0 - FLT 881 - THE LT ENGINE WAS LOSING OIL APPROXIMATELY 1 TO 2 QUARTS PER TEN MINUTES IN FLIGHT. THE CREW DECIDED TODIVERT TO GSO AS A PRECAUTION.  MAINTENANCE FOUND THE LINE TO THE NR 1 OIL TRANSMITTER LEAKING.  THE SEAL WAS REPLACED AND THE JAMB NUT TIGHTENED.  OPERATION CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 283 - THE CREW RECEIVED A MASTER CAUTION, NO ANNUNCIATOR LIGHT AND A 'LT CSD LOW OIL LIGHT'.  THE CAPTAIN SHUT OFF THE GENERATOR/CSD AND ELECTED TO LAND AT PIT.  ON FINAL TO PIT CREW RECEIVED A 'RT CSD LOW OIL LIGHT' AND CAPTAIN SHUT OFF RT GENERATOR\CSD.  AN EMERGENCY WAS DECLARED.  THE ACFT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE RESET THELT GENERATOR CONTROL PANEL AND AC CROSSTIE.  THEY REPLACED THE RT ENGINE CSD DUE TO FAILURE.  OPERATIONS CHECKED GOOD.(W)


REMARKS:
YUL - FLT 257 - ON FINAL APPROACH, THE CREW RECEIVED AN UNSAFE NOSE GEAR INDICATION.  THEY PERFORMED A MISSED APPROACH AND WENT AROUND.  THE GEAR WAS RECYCLED TWICE BUT WAS STILL UNSAFE.  THE CREW CLIMBED OUT OF THE AREA AND PERFORMED ANOTHER GEAR RETRACTION WHICH WAS NORMAL.  THE ACFT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE INSPECTED THE NOSE GEAR AND FOUND NO FAULTS.  BOTH NOSE GEAR INDICATION SWITCHES WERE NORMAL.  (W)


REMARKS:
CHS - FLT 1178 - THE LT AND RT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
CLT - FLT 730 - AT 33,000 FEET, THE FIRST OFFICER WINDSHIELD CRACKED.  THE CAPTAIN DESCENDED TO 10,000 FEET TO TAKE THEPRESSURE OFF.  THE ACFT REMAINED AT 10,00 FEET AND DIVERTED TO CLT WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE WINDSHIELD AND THE TEMPERATURE CONTROLLER.  OPERATIONS CHECKED GOOD.  REF 95ZZZW21.


REMARKS:
PHL - FLT 1277 - THE FIRST CLASS EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERIES.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 1634 - THE EMERGENCY A/C AND D/C LIGHTS WOULD NOT TEST.  MAINTENANCE REPLACED THE OVERHEAD ANNUNCIATOR PANEL. OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
RDU - FLT 2517 - ON APPROACH, WHEN LANDING GEAR WAS LOWERED, TWO GREEN LIGHTS ILLUMINATED FOR THE MAIN GEAR, BUT NO LIGHT FOR THE NOSE GEAR.  THE CREW RECYCLED THE GEAR AND THREE GREEN LIGHTS ILLUMINATED.  NO FURTHER INCIDENTS.  MAINTENANCE CLEANED GREASE FROM THE DOWN LOCK POSITION SWITCH CONNECTOR.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLE - EMERGENCY EXIT LIGHT STRIP UNDER FIRST CLASS INOPERATIVE.  MAINTENANCE REPAIRED WIRE UNDER SEAT ROW 1A AND C.  (W)


REMARKS:
BOS - SERVICE DOOR EMERGENCY LIGHT INOPERATIVE.  MAINTENANCE RELAMPED.  (W)


REMARKS:
ORF - FLT 2292 - A NR 2 BLEED DUCT LEAK AND POSSIBLE APU FIRE.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCERAN BOTH ENGINES, FOUND NR 1 H/P VLV PRESSURE AT 60 PSI, ADJUSTED SAME.  INSPECTED APU COMPONENTS, NO EVIDENCE OF ANY FIRE DAMAGE.  REPLACED APU FIRE BOTTLE.  (W)


REMARKS:
CLT - FLT 1512 - AFTER T/O FUEL WAS VENTING OUT BOTH WINGS (MAIN PUMPS ON CTR TANK PUMPS ON AUTO).  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED MAIN FUEL PANEL (REFUEL), AND GROUND RAN ENGINES.  NO LEAKAGE FROM WING VENTS NOTED, OK FOR SERVICE.  (W)


REMARKS:
TPA - FLT 1882 - AUTO FEED FAULT ON TO.  CENTER TANK PUMPS TURNED OFF.  FUEL NOTICED BY TOWER VENTING FROM BOTH WING TIPS.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED FUELING DOOR SHUTOFF BRACKET AND RIGGED.OPERATION CHECKS OK.  (W)


REMARKS:
MSP - FLT 1847 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. CREW GOT GRND/FLT CONTROL ALERT.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE READJUSTED G/F MICRO-SW PER MM 32-63-01.  INSPECTED GEAR CYCLING AND SWITCH ADJUSTMENTS.  NORMAL OPERATION.  (W)


REMARKS:
PIT - FLT 243 - THE LT WINDOW HEAT FAILED IN FLIGHT, COULD NOT REINSTATE.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED LT WINDOW HEAT CONTROLLER.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
JAX - EMERGENCY LIGHT IN CABIN WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED NR 4 AND NR 5 BATTERY PACKS.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
PIT - FLT 324 - LIFTDUMPER UNSAFE WARNING DURING FLIGHT.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  FOUND LTLIFTDUMPER INTERLOCK PROX SWITCH NR 2 INTERMITTENT.  REMOVED AND REPLACED SWITCH, OPERATION CHECKS NORMAL.  (W)


REMARKS:
CLT - FLT 794 - AFTER TAKEOFF, CREW GOT VIBRATION FROM RT MAIN GEAR AND THEN GOT LOW EPR AND LIFTDUMPER FAULT.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND DAMAGE TO THE RT WING FLAP FAIRING, RT ENG COWLING, FIRST STAGE FAN BLADES ALL CAUSED BY THE RT MAIN I/B TIRE BLOWN.  REPAIRED AND REPLACED DAMAGED AREAS AND REPLACED RT I/B TIRE. (W)


REMARKS:
ORF - DURING UNSCHEDULED MAINTENANCE FOUND AFT CABIN EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED NR 6 AND NR 7 BATTERY PACKS, AND NR 7 INVERTER FOR AFT ACFT EMERGENCY LIGHTS.  (W)


REMARKS:
DURING SCHEDULED A-CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY CHARGER PER BOEING MM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD  EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT ASSEMBLY PER BOEING MM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD SERVICE AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOP.  REPLACED BATTERY PACK AND CHARGER PER BOEING MM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND A 3 INCH CRACK IN FUSELAGE SKIN IN LOWER SECTION 46, BS 951, FWD OF POTABLE WATER SERVICE PANEL.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND A 2 INCH CRACK IN LOWER LEFT FUSELAGE SECTION 46, BS 727E, AFT OF LOWER EMERGENCY EXIT LIGHT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING WALKAROUND CHECK, FOUND A 2 INCH FUSELAGE SKIN  CRACK AT BS 761, 1 INCH ABOVE S17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING WALKAROUND CHECK, FOUND A 2.25 INCH FUSELAGE SKIN  CRACK AT BS 814, AT S16L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING WALKAROUND CHECK, FOUND A FUSELAGE SKIN  CRACK AT BS 831, 2 INCHES ABOVE S25R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP.  REPLACED AFT BATTERY PACK PER BOEING MM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND SECTION OF CABIN EMERGENCY FLOOR LIGHTING INOP.  REPLACED AFT BATTERY PACK PER BOEING MM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EXIT SIGN LIGHT INOP.  REPLACED BATTERY PACK PER BOEING MM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY CHARGER PER BOEING MM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY DOOR EMERGENCY EXIT SIGN LIGHT INOP.  REPLACED BATTERY PACK PER BOEING MM.


REMARKS:
DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACK BETWEEN PASSENGER WINDOWS 11 AND 12.  THE CRACK MEASURED 3 INCHES IN LENGTH AND APPROX CENTERED IN THE SKIN PANEL BETWEEN WINDOWS JUST BELOW S12L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND RIGHT WING SPAR UPPER SURFACE AT WS 500 JUST AFT OF FRONT SPAR CORRODED.  REPAIRED PER TRAMCO EWO 95-0051.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL CORROSION AT BS 767-787, RBL 22, WL 150 AND AT BS 344, BL 0, WL 208.  FABRICATED AND REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
ON TAKEOFF, AIRCRAFT EXPERIENCED SLIGHT TAIL DRAG.  INSPECTED AREA PER BOEING STRUCTURAL REPAIR MANUAL.  PERFORMED MAINT FERRY FLIGHT TO DAL FOR REPAIRS.  FABRICATED DOUBLER AND REPAIRED DAMAGED AREA PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
PHL - FLT 474 - THE NR 2 ENGINE WAS UNABLE TO DEVELOP FULL POWER.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.MAINTENANCE REPLACED THE RT ENGINE FUEL FLOW REGULATOR.  TRIM RUN AND LEAK CHECK OK.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY .5 INCH AREA CORRODED ON FLOOR BEAM, BS 967, LBL 18.  REPAIRED PER EA 38318.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH AREA CORRODED (3 PLACES) ON FLOOR BEAM BS 967-RBL 18, RBL 25, AND LBL 18.  REPAIRED PER EA 38318.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-1 CHECK INSPECTION, FOUND 2 INCH BY 2 INCH AREA OF CORROSION AT SEAT RAIL ON FLOOR BEAM BL 1127R NEAR STATION 4850.  REMOVED CORRODED AREAS AND INSTALLED REPAIR ANGLES PER USAIR EA NR 28880.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-1 CHECK INSPECTION, FOUND 4 ELONGATED HOLES IN THE LEFT WING NR 4 LIFT DUMPER SPIGOT MOUNT REAR SPAR BRACKET.  OVERSIZED HOLES AND INSTALLED BUSHINGS PER USAIR EA 28886.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-1 CHECK INSPECTION, FOUND 3 INCH BY .5 INCH AREA OF CORROSION AT RT OUTBOARD SEAT TRACK (BL250R) NEAR STATION 3450.  REMOVED AND REPLACED FORWARD SECTION OF SEAT TRACK PER SRM 53-10-00.  (W)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-1 CHECK, INSPECTION FOUND A 4 INCH BY 2.5 INCH DEBONDED AREA OF THE LEFT STUBWING FUSELAGE SKIN, BETWEEN FRAMES 24011 AND 24611 AND STRINGERS 22 AND 23.  INSTALLED INSIDE DOUBLER PER USAIR EA 28877.  (W)


REMARKS:
DURING CLIMB, NUMBER 5 SLAT WOULD NOT FULLY RETRACT.  RECYCLED SLATS WITH NO HELP.  AIRCRAFT RETURNED TO ONT AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 5 SLAT ACTUATOR AND OPERATION CHECK PER BOEING MM.


REMARKS:
DURING CLIMB, NUMBER 6 L/E SLAT TRANSIT LIGHT REMAINED ILLUMINATED.  RECYCLED SLATS WITH NO HELP.  AIRCRAFT RETURNED TOHOU AND MADE AN UNEVENTFUL LANDING.  REPLACED NUMBER 6 SLAT ACTUATOR AND OPERATION CHECK PER BOEING MM.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT CARGO DOOR L ANGLE CORRODED AT BS 832 RBL 32 WL 158.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED, AND A PREVIOUS REPAIR AT BS 767, BETWEEN S20 AND 21R.  REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM STIFFENER CORRODED AT BS 294.5 AND 312, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, MAIN GEAR BRAKE ANTI-SKID INOP LIGHT FLICKERED MOMENTARILY, THEN REMAINED ILLUMINATED.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACED ANTI-SKID CONTROL UNIT PER BOEING MM.


REMARKS:
DURING WALKAROUND INSPECTION , FOUND A 4 INCH SKIN CRACK ON RIGHT SIDE FUSELAGE, JUST AFT OF T/E FLAPS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND 3 INCH SKIN CRACK AT BS 890, AT S24R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND RIGHT WING FIXED L/E CRACKS AT NUMBER 4 AND 5 AUX TRACK CUTOUTS.  REPAIRED PER SWA RA 1-257-264/65.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND PRESSURE BULKHEAD CRACKED IN RADIUS OF FWD VERTICAL FLANGE OF T-SUPPORT AT BS 178 LBL 5.5 WL 183.0.  REPAIRED PER SWA RA 1-253-1239.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND SEVERAL CRACKS UNDER VERTICAL STRAP AT BS 178, LBL 5.7.  REPAIRED PER SWA RA 1-253-1240.


REMARKS:
DURING SCHEDULED C-2 CHECK, FOUND SUPPORT ANGLE CRACKED AT WING TO FUSELAGE TRANSITION PANEL INBOARD OF GROUND SPOILER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING WALKAROUND INSPECTION, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 761, 1 INCH ABOVE S17L.  A 2.25 INCH CRACK AT BS814 S16L, AND A 2.75 INCH CRACK AT BS 831, 2 INCHES ABOVE S25R.  REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CORROSION AROUND FASTENERS AT BS 727D TO 767, S26R, AND AT BS 767 TO 807, S26R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND APU COMPARTMENT BULKHEAD AIR INLET CUTOUT WITH CORROSION ON UPPER AND LOWER STRINGERS AND STIFFENERS FROM  BS 1116 TO 1127.  REPLACED PARTS PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FORWARD GALLEY DOORWAY INNER CHORD CRACKED AT BS 294.  REPAIRED PER SWA RA 1-553-1228.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND WEB CRACKED AT BS 726 STRINGER 18A, RIGHT SIDE.  REPAIRED PER SWA RA 1-553-1233.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND WEB HOLE CRACK AT BS 1088 BULKHEAD.  REPAIRED PER SWA RA 1-553-1234.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACKED FROM BS 480 TO 500B, 808, 858, STRINGER 10R.  REPAIRED PER TRAMCO EWO 95-0058.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS  AT THE FOLLOWING LOCATIONS:  BS 380, 381, 400 TO 431, 450 TO 461, 490, 500, 500 PLUS 1, AND 500A TO 500B, STRINGER 10L.  REPAIRED PER TRAMCO EWO95-0058.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATIONS:  BS 400, 410, 420, 430, 440, 461 TO 500A, 500B, 500B PLUS 10, 586, 587, 605, 626, 705, 727A, 777, 778, 818, 838, 848,868, 878, 888, 898, 925, STRINGER 4L.  REPAIRED PER TRAMCO EWO 95-0058.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATION: BS 379 TO 399, 479 TO 500, 500 PLUS 9, 500A, 500A PLUS 9, 500A PLUS 10, 500B PLUS 1, 588, 628, 684 TO 706, 746, 747, 777, 816, 817, 846, 847, 886, 887, 916, 945, 965 TO 995, STRINGER 4R.  REPAIRED PER TRAMCO EWO 95-0058.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATION: BS 520 AND 521, STRINGER 10L.  REPAIRED PER TRAMCO EWO 95-0058.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN DENTED AT BS 413, BETWEEN S5 AND 6R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 380, S14R.  REPAIRED PER TRAMCO EWO 95-0058.


REMARKS:
N1 TURBINE SHAFT FAILED DURING TEST CELL RUN.  (X)


REMARKS:
PIT - DURING ACCOMPLISHMENT OF Q-1 CHECK INSPECTION, FOUND A 10 INCH BY 22 INCH AREA OF DEBOND AND OVERHEATED SKIN RT STUBWING FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611 AND BETWEEN STRINGERS 51 AND 53A (VISUAL INSPECTION CONFIRMED BY CONDUCTING CHECK).  REMOVED DAMAGED MATERIAL AND INSTALLED FILLERS AND DOUBLERS PER USAIR EA NR 28877.  (W)


REMARKS:
FLT 24 - DIVERTED TO ATL ON FLIGHT FROM EWR TO MCO AFTER A/C COULD NOT MAINTAIN PRESSURIZATION.  REMOVED AND REPLACED RIGHT OUTFLOW VALVE AND REMOVED AND REPLACED CABIN MANUAL PRESSURE CONTROL.  OPS CHECK OKAY PER MM 21-31-00.  REF CONTROLNR IXKA9400033.


REMARKS:
ATL/FLL - FLT 139 - DURING CLIMB, RIGHT ENGINE LOST OIL QUANTITY AND PRESSURE.  CREW SHUT DOWN ENGINE AT 4 QUARTS, APPROXIMATELY 10-15 MINUTES SINGLE ENGINE TIME.  RETURN TO ATL.  REMOVED AND REPLACED OIL PRESSURE TRANSMITTER.


REMARKS:
PHL/ATL - FLT 225 - DURING TAKEOFF ROLL, APPROXIMATELY 100 KIAS, AIRCRAFT STRUCK ONE OR MORE DEER.  ACCOMPLISHED A THOROUGH AIRCRAFT INSPECTION, THE ONLY DAMAGE WAS TO THE RIGHT NOSE GEAR DOOR.  MADE AN INTERIM REPAIR AT PHL.  THE DOOR WASREMOVED, REPAIRED AND REINSTALLED ON RETURN TO ATL.


REMARKS:
DURING SPECIAL CHECK, FOUND CORROSION ON FUSELAGE SKIN STA 700 TO STA 703, STR 29L AND STR 29R.  REMOVED CORROSION AND REPAIR PER SRM 53-30-3.  AIRCRAFT TOTAL TIME:  36,863 HOURS; 23,946 CYCLES.


REMARKS:
DURING CHECK C-2D, FOUND CRACK APPROXIMATELY TWO INCHES IN BULKHEAD BELOW APU FLOW CONTROL VALVE, IN RT MLG WHEELWELL.STOP DRILLED CRACK AND INSTALLED DOUBLER PER TWA DWG C03242 AND TWA STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  61,014 HOURS; 40,930 CYCLES.


REMARKS:
DURING SPECIAL CHECK, FOUND CORROSION ON FUSELAGE SKIN AFT OF STA 1010, OUTBOARD OF STR 29R AND STR 30R.  REMOVED CORROSION PER SRM 51-10-6 AND REPAIRED PER SRM 53-30-3, FIGURE 3A.  AIRCRAFT TOTAL TIME:  36,860 HOURS; 23,944 CYCLES.


REMARKS:
DURING OP-17, FOUND CORROSION ON RT SERVICE DOOR FRAME AT FLOOR LINE FORWARD FRAME.  REPAIRED PER SRM 51-40-3.  AIRCRAFT TOTAL TIME:  37,605 HOURS; 23,610 CYCLES.


REMARKS:
DURING OP-17, FOUND CORROSION ON AFT CARGO FUSELAGE SKIN, STA 1045, STR 28L.  REPAIRED PER SRM 53-30-03.  AIRCRAFT TOTAL TIME:  37,605 HOURS; 23,610 CYCLES.


REMARKS:
DURING SPECIAL CHECK, FOUND A FUSELAGE SKIN CRACK AND CORROSION, STA 277, STR 25R AND STR 26R.  INSTALLED DOUBLER PER SRM 53-30-3 AND TWA STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  58,949 HOURS; 39,640 CYCLES.


REMARKS:
DURING SPECIAL CHECK, FOUND CORROSION ON FUSELAGE SKIN, STA 1050 TO STA 1070, STR 29R AND STR 30R.  CUT OUT CORRODED SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 3.  AIRCRAFT TOTAL TIME:  36,863 HOURS; 23,946 CYCLES.


REMARKS:
ATL/BNA - FLT 558 - AIRCRAFT TURNED BACK TO ATL FOR A TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ON.  SWAP EQUIPMENT WITH AIRCRAFT 915VV.  FOUND LOOSE CLAMPS FORWARD AND AFT OF AUGMENTATION VALVE RT SIDE.  VERIFIED FLANGES NOT CRACKED, REINSTALLED CLAMPS, TORQUED, AND SAFETY-WIRED HIGH POWER TO 1.9 EPR.  LIGHT DID NOT COME ON.


REMARKS:
ATL/TPA - FLT 567 - AIRCRAFT RETURNED TO ATL UNABLE TO PRESSURIZE.  FOUND FORWARD CARGO DOOR AND E & E DOOR AJAR.  RESECURED BOTH DOORS AND DOOR LIGHTS OPS CHECKED GOOD.


REMARKS:
ATL/TPA - FLT 531 - RETURNED TO ATL DUE TO A NR 1 CSD OVERHEAT AND THE CSD WOULD NOT DISCONNECT.  REMOVED AND REPLACE NR 1 CSD.


REMARKS:
FLT 24 - DIVERTED TO ATL ON FLIGHT FROM EWR TO MCO AFTER A/C COULD NOT MAINTAIN PRESSURIZATION.  REMOVED AND REPLACED RIGHT OUTFLOW VALVE AND REMOVED AND REPLACED CABIN MANUAL PRESSURE CONTROL.  OPS CHECK OKAY PER MM 21-31-00.  REF CONTROLNR 95ZZZX528.  (X)


REMARKS:
EWR/MDW - FLT 15 - THIRTY MINUTES INTO FLIGHT, UNABLE TO CONTROL CABIN PRESS IN MANUAL OR AUTO AT 28,000 FEET, A/C RETURNED TO EWR.  REMOVED AND REPLACED MANUAL PRESS CONTROL AND REMOVED AND REPLACED AUTO PRESS CONTROLLER PRECAUTIONARY PERMM 21-30-01 AND MM 31-30-00.  OPS CHECK OKAY.  (X)


REMARKS:
PHL - THE AFT LT AISLE FLOOR LEVEL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKAND CHARGER.  REF USAA941434.


REMARKS:
CLT - THE EMERGENCY LIGHTING AT ROW 11 TO 20 LT SIDE WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY CHARGER.  SYSTEM OPERATIONS CHECKED GOOD.  (W)


REMARKS:
IND - THE EMERGENCY LIGHT TRACK IN THE AFT CABIN IS CRACKED.  MAINTENANCE REPLACED THE TRACK SECTION.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PHL - THE AFT LT AISLE FLOOR LEVEL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKAND CHARGER.  REF95ZZZW30.


REMARKS:
PIT - FLT 816 - RETURNED TO FIELD DUE TO E/M 'GEN OFF'.  ALSO, THE GENERATOR OFF LIGHT ILLUMINATED.  MAINTENANCE REPLACED THE RT IDG.  OPERATIONS AND LEAK CHECKED GOOD.  (W)


REMARKS:
CLT - THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
EWR - THE FLOOR LEVEL EMERGENCY LIGHTS PAST ROW 17 WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPAIRED A BAD SECTION OFWIRE AND REPLACED THE BATTERY PACK.  (W)


REMARKS:
PHL - FLT 1021 - AFTER TAKEOFF, LT GENERATOR FAILED, APU ON MEL.  FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED NR1 ENGINE AC GENERATOR.  (W)


REMARKS:
DCA - THE LEFT EMERGENCY EXIT OVERWING LIGHT INOPERATIVE.  MAINTENANCE REPLACED LIGHT ASSEMBLY AT EMERGENCY EXIT ROW.  (W)


REMARKS:
DURING SCHEDULED A3 CHECK, FOUND FWD OVERHEAD EXIT SIGN INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT NOT TESTING.  REPLACED BATTERY PER BOEING M/M.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 360, S15L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S4L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 501, S28R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S14L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 767, S11L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP BENT AND GOUGED AT BS 727B, S26R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 927, S27R, AT BS 500A, S9R, AT BS 663, S10L, AT BS 663, S10R, AND AT BS 947, S25R.  REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, BL 0 TO RBL 25.  REPLACED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM FASTENER HOLE CORRODED AT BS 947, WL 208, RBL 5.  REPAIRED PER SWA EWO 95-0086.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM SUPPORT CRACKED AT BS 540, WL 208, BL 0 TO LBL 25.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM STANCHION CRACKED AT BS 747+4, RBL 11, WL 161.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOOR BEAM NUTPLATE HOLES CORRODED AT BS 312, LBL 11 TO RBL 11, WL 208.  REPLACED DAMAGED SECTION PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND NUMBER 2 SLAT SKIN CRACKED ADJACENT TO EXISTING REPAIR.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL AND DRAWING 65C30133.


REMARKS:
DURING SCHEDULED D CHECK, FOUND 'L' ANGLE CRACKED AT BS 616, WL 200.  REPAIRED PER TRAMCO EWO 95-0066.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOOR MOP SILL CORRODED AT BS 985, WL 208, S17R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOOR UPPER FORWARD FRAME CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AC DISTRIBUTION BAY LEFT KEEL BEAM OUTBOARD FLANGE CORRODED AT BS 500D, WL 149, LBL 7.REPAIRED PER TRAMCO EWO 95-0073.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD CARGO AFT DOOR FRAME CRACKED IN FORWARD TOP RADIUS ABOVE NUMBER 5 STOP FITTING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD CARGO AFT DOOR FRAME DENTED IN TOP FLANGE OF FRAME, BS 500, RBL 45, WL 165.75.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND E/E DOOR OUTER SKIN GOUGED AND NICKED.  REPAIRED DAMGED AREAS PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKS FROM BS 727 TO 907, S20 TO 25L AND R.  REPLACED SKINS PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTS AT: BS 916.5, 2 INCH ABOVE S25L, BS 807 TO 812, S27L TO 27R, AT BS 307, BETWEEN 21 AND 22R, AT BS 500A +6, BETWEEN S24 AND 24R, AT BS 311, BETWEEN S20 AND 21R, AT BS 1064, BETWEEN S20 AND21R, AND FROM BS 849 TO 854, BL 0 TO RBL 15, WL 159.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 957, AT S19R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOORWAY UPPER FORWARD FRAME CRACKED ON INBOARD RADIUS AT LATCH FITTING.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 327, RBL 65, WL 210.  REPAIRED PER BOEING STRUCTURAL REPAIRMANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD FOUND VERTICAL SUPPORT WEB DENTED AT SIDEWALL SUPPORT PLATE ATTACH LOCATION BS 500+3, RBL 22.5, WL 156.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND KEEL BEAM STRESS PANEL DAMAGED AT BS 663-727, BL 0, WL 148.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND WEB BETWEEN VERTICAL STANCHION BEAMS CRACKED AT BS 727, LBL 12-15, WL 170.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


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


REMARKS:
DURING SCHEDULED D CHECK, FOUND PRESSURE WEB ANGLE CRACKED AT BS 663, RBL 65, WL 203.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND WING CENTER SECTION PRESSURE DECK WEB CRACKS AT BS 665.75, RBL 39.25, WL 202.5 AND AT BS 672.75, RBL 42.5, WL 202.5.  REPAIRED PER TRAMCO EWO 95-0065.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FORWARD SERVICE DOOR OUTER SKIN GOUGED ON FORWARD EDGE ABOVE LOWER HINGE.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D CHECK, FOUND LIGHTNING STRIKE DAMAGE AT THE FOLLOWING AREAS: BS 777, S9R, AT BS 727A+16 TO 18, S8R, AT BS 500D+1.5, S3R, AT BS 727E+10, S9R, AT BS 607.75, S5R, AT BS 441, S9L, AT 278.5, 3.75 INCH ABOVE S12L, AT BS 500A+11.25 AND +13.75, S6R, AT BS 748, S9R, AT BS 727E+1.25, S9R, AT BS 727C+7 TO 8, S9R, AT BS 749.5, S9R, AT BS 727A+2, S8R,AT BS 656, S5R, AT BS 582.5, S5R, AT BS 727C+1.25, S9R, AT BS 546.5, S5R, AT BS 500A+8, S8L, AT BS 540.5, S5R, AND AT BS 523.5, S5R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 391, 421, 431, 441, 461, 500A, AND 500A+1, 500B, 500B+1, 530, AT STRINGER 10R.  REPAIRED PER TRAMCO EWO 95-0115.


REMARKS:
DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 469, AND AT 500A+9, STRINGER 4L.  REPAIRED PER TRAMCO EWO 95-0115.


REMARKS:
DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178, WL 184, LBL 5.7, PRESSURE BULKHEAD, ATFASTENER HOLES.  REPAIRED PER TRAMCO EWO 95-0119.


REMARKS:
DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATION AT VERTICAL STIFFENER, BS 178, WL 181-184, LBL 8.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATION AT BS 351, AND 381, STRINGER 14R.  REPAIRED PER TRAMCO EWO 95-0115.


REMARKS:
DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS FROM BS 267 TO 328, STRINGER 24R, ON BACK SIDE OFEXISTING REPAIR.  REMOVED EXISTING REPAIR AND REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
PIT - THE FLOOR LEVEL EMERGENCY EXIT LIGHTS FROM ROW C FORWARD DO NOT TEST.  MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK AND REPAIRED A BROKEN WIRE.  OPERATIONS CHECKED GOOD.  REFERENCE NR USAA950033.


REMARKS:
INT - DURING 'Q-99' VISUAL INSPECTION, FOUND .25 INCH BY .25 INCH .020 DEEP CORRODED AREA STATION 43 LBL 48 FLOOR BEAM. REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-224-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' VISUAL INSPECTION, FOUND FLOOR BEAM 1 INCH BY .5 INCH CORRODED AREA BS 343 LBL 43.  REPAIRED PER SRM TR 53-10-03.  CORROSION TASK NR C53-224-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA ON CHANNEL AT BS 450 RBL 55 TO 70.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-224-03.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND .5 INCH BY 15 INCH TOTAL AREA CORRODED ON FLOOR BEAM AT BS 1110 AT RBL 12 INCHES THROUGH LBL 21 INCHES.  REPAIRED PER SRM 53-10-03.  CORROSION TASK NR C53-224-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 20 INCH CORRODED AREA ON AN ANGLE BS 1176 LBL 24 THROUGH RBL 2.  REPAIRED PER EA 38530.  CORROSION TASK NR C53-224-06.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 23 INCH CORRODED AREA 'Z' ANGLE CORRODED STATION 1041-1064.  REPAIRED PER SRM 51-10-01 ITEM 4.  CORROSION TASK NR C53-224-06, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND 3 INCHES BY 20 INCHES OF CORROSION STATION 1168-1176 RBL 1.5 TO RBL 19.5 ON SHEAR WEB.  REPAIRED PER BOEING DRAWING 65-19606 SH 27.  CORROSION TASK NR C53-224-06, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORRODED AREA BS 1176 RBL 19 INCHES ON FLOOR PAN.  REPAIRED PER SRM 51-40-02.  CORROSION TASK NR C53-224-06, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY .25 INCH BY 20 INCH TOTAL AREA CORRODED ON SEAT TRACK AT BS 1090 THROUGH BS 1138 AT LBL 25 INCHES.  REPAIRED PER SRM 53-10-5.  CORROSION TASK NR C53-224-06, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION,  FOUND 1 INCH BY 3 INCH AND 1 INCH BY 1 INCH CORROSION ON SEAT TRACK AT BS380 RB 55.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-224-03, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 25 INCH AREA WITH SURFACE CORROSION ON SEAT TRACK STATION 370 TO 400 AT RBL 43.  REPAIRED PER SRM 53-10-5.  CORROSION TASK NR C53-224-03.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORRODED AREA ON SEAT TRACK AT STATION 1018 LBL 23.  REPAIRED PER SRM 53-10-5 FIG 7.  CORROSION TASK NR C53-224-03, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND SEAT TRACK CORROSION 1 INCH BY 2 INCH AREA, BS 372 RBL 23.  REPAIREDPER SRM 53-10-5.  CORROSION TASK NR C53-224-03, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING 'Q-99' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED ANGLE BS 1176 AIRSTAIR ENTRY THRESHOLD ANGLE.  REPAIRED PER EA 38530.  CORROSION TASK NR C53-224-06, CORROSION LEVEL 2.  (Z)


REMARKS:
CLT - FLT NR 1095 - ON FINAL APPROACH, CREW GOT 3 GREEN LIGHTS ON THE GEAR BUT ALSO GOT A LIGHT IN THE GEAR HANDLE AND RT MLG NOT LOCKED ON MULTI FUNCTION DISPLAY UNIT.  CYCLED GEAR.  ALL INDICATIONS NORMAL.  AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE DETERMINED RT MLG PRIMARY DOWNLOCK SENSOR OVER-SENSING.  REPLACED SENSOR IAW MM 32-61-03-400-814A AND CONFIRMED CORRECT ADJ PER MM 32-61-03-820-815A.  LANDING GEAR POSITION INDICATION SYSTEM OPERATIONAL NORMAL.  (Z)


REMARKS:
SJU - FLT 0396 - DURING GEAR RETRACTION, A LOUD NOISE WAS HEARD FROM THE NOSE GEAR.  THE NOSE GEAR DOOR L/E ANNUNCIATORPANEL LIGHT REMAINED ILLUMINATED.  MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR CABLE BROKEN.  THEY REPLACED BOTH GEAR DOOR CABLES.  (Z)


REMARKS:
PHL - FLT 1735 - AFTER TAKEOFF, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED.  THE CREW DECIDED TO RETURN TO PHL.  MAINTENANCE ADJUSTED THE NOSE GEAR UPLOCK PROXIMITY SWITCH.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
LGA - FLT 2236 - THE CABIN FLOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPAIRED A BROKEN WIRE.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
PHL - FLT NR 183 - ON FINAL APPROACH, CREW COULD NOT GET 3 GREEN LIGHTS ON THE GEAR.  THE LEFT MAIN GEAR LIGHT TESTED BUT WOULD NOT ILLUMINATE.  CYCLED GEAR, THEN AN INTERMITTENT LEFT LANDING GEAR DOWNLOCK SWITCH LIGHT ON MULTIFUNCTION DISPLAY UNIT.  AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LEFT MAIN GEAR DOWNLOCK ACTUATOR AND RIGGED PER MM.  (Z)


REMARKS:
PHL - COCKPIT EMERGENCY EXIT DOES NOT LIGHT WHEN TESTED.  MAINTENANCE REPLACED CHARGER ASSEMBLY.  EMERGENCY LIGHTS CHECK GOOD.  (Z)


REMARKS:
PHL - COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE.  MAINTENANCE REPLACED LIGHT ASSEMBLY.  (Z)


REMARKS:
PHL - FLT 2338 - FLOOR EMERGENCY TRACK LIGHTING AT ROW 3 HAS LENS AND LIGHT MISSING.  MAINTENANCE REPLACED LIGHT AND LENS.  (Z)


REMARKS:
IND - FLIGHT EN ROUTE PIT TO PHX WHEN NR 1 GENERATOR DROPPED OFF LINE, FOLLOWED BY APU OPERATING INTERMITTENTLY THE SHUTTING DOWN.  FLIGHT DIVERTED TO IND WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND BENT PIN NR 2213 ON NR 1 ENGINE GCU.  REPLACED GCU.  (Z)


REMARKS:
PIT - THE FLOOR LEVEL EMERGENCY EXIT LIGHTS FROM ROW C FORWARD DO NOT TEST.  MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK AND REPAIRED A BROKEN WIRE.  OPERATIONS CHECKED GOOD.  REFERENCE NR 95ZZZZ43.


REMARKS:
PIT - THE AFT CABIN EMERGENCY LIGHTS WRE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
CLT - FLT 8028 - THE NR 1 NAV IS 45 PERCENT OFF.  IT IS TO TTHE RIGHT OF THE NR 2 NAV.  MAINTENANCE REPLACED THE VOR REC SYSTEM.  OPERATIONS CHECK GOOD.  (Z)


REMARKS:
CLT - FLT 1004 - THE EMERGENCY EXIT LOW LEVEL FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE AFT BATTERY PACK.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
SYR - FLT 1091 - AFTER GEAR RETRACTION THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NOSE GEAR DOOR SELECTOR AND SEQUENCING VALVES PER MM 32-32-06 AND 07.  LEAK AND OPERATION CHECKS NORMAL.  REF USAA950011.


REMARKS:
EWR - FLT 4001 - AFTER TAKEOFF, THE TAIL SKID LIGHT REMAINED ON.   RECYCLED GEARS, LIGHT STILL ON.  RETURNED TO EWR.  CLEANED MOISTURE, OIL AND CORROSION FROM SWITCHES.  OPERATED TAIL SKID SEVERAL TIMES AND VERTIFIED OPERATION PER MM 32-61-01, NO DEFECTS NOTED.  (W)


REMARKS:
SYR - FLT 1091 - AFTER GEAR RETRACTION THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NOSE GEAR DOOR SELECTOR AND SEQUENCING VALVES PER MM 32-32-06 AND 07.  LEAK AND OPERATION CHECKS NORMAL.  REF 95ZZZW83.


REMARKS:
PHL - FLT 2053 - ON TAKEOFF, THE GALLEY DOOR SEAL WAS LEAKING AND MAKING A RUMBLING NOISE.  MAINTENANCE REPAIRED THE FWD GALLEY DOOR TRIM.  (W)


REMARKS:
ORF - FLT 956 - ON GEAR EXTENSION AT PHF, THE RT MAIN GEAR INDICATED UNSAFE.  THE GEAR WAS RECYCLED AND THE INDICATION WAS STILL UNSAFE.  THE CAPTAIN MADE A VISUAL INSPECTION WHICH SHOWED OK.  THE FLIGHT DIVERTED TO ORF.  WHILE MAKING A LOW PASS OVER THE RUNWAY, THE GEAR WAS CONFIRMED TO BE DOWN.  MAINTENANCE REPLACED THE RT MAIN GEAR DOWNLOCK SWITCH AND CLEARED THE CONNECTOR.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
MCO - FLT 2382 - AFTER DEPARTING MCO, CREW RECEIVED AND OVERHEAT INDICATION IN THE TAIL SECTION.  THE CREW FOLLOWED EMERGENCY PROCEDURES TO ISOLATE THE PROBLEM.  THE LT PACK WAS SHUTDOWN, BUT THE CABIN PRESSURE COULD NOT BE MAINTAINED ON THE RIGHT PACK.  THE CREW DECIDED TO RETURN TO MCO.  MAINTENANCE REPLACED THE CLAMP ON RT PACK AAV INLET.  THE ACFT WAS PRESSURIZED WITH THE RT PACK.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 431 - AFTER CLIMB TO 10,000 FEET, THE ACFT WOULD NOT PRESSURIZE.  THE CREW DECIDED TO RETURN TO PIT.  MAINTENANCE PERFORMED A BITE CHECK, INSPECTED THE OUTFLOW VALVE, ACCOMPLISHED AN AUTO PRESSURE CHECK.  OPERATIONS CHECKED GOOD. (W)


REMARKS:
PIT - FLT 508 - 'THE WING ANTI-ICE CAPACITY' MESSAGE CAME ON WITH THE WING AN TAIL ANTI-ICE TURNED ON.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND THE RT HPSOV NOT OPENING COMPLETELY WHEN AIR IS ON.  REPLACED THE RT HPSOV.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
PIT - FLT 385 - FLIGHT EN ROUTE PHL TO DEN WHEN TOP LT WING OVAL PANEL, ABOVE ENGINE NACELLE SHOWED MINOR SEEPAGE.  NO FUEL IMBALANCE NOTED.  FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED FUEL TANK ACCESSPANEL AFT OF NR 1 PYLON ON TOP OF WING.  LEAK CHECK OK.  (W)


REMARKS:
BWI - FLT 1795 - FLIGHT EN ROUTE, WHEN FWD AMBER LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED.  THE NR 5 SLAT FULL EXTEND LIGHT ALSO ON.  FLIGHT DIVERTED TO BWI WHERE LANDING  WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 5 LEADING EDGE SLAT PROXIMITY SWITCH, S178.  ALL INDICATIONS CHECK NORMAL.  (W)


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


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS LEFT AND RIGHT SIDES INOP.  REPLACED BATTERY PACKAND BASE PER BOEING M/M.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 294.5 AND 312.  REPLACED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT FOLLOWING LOCATIONS: BS 1020, BETWEEN S12 AND 13L, AT BS 1000, WL 220, LEFT SIDE BEHIND AFT ENTRY DOOR, AT BS 356, BETWEEN S18 AND 19R, AT BS 193, WL 192, LEFT SIDE, AT BS 1040, LBL 188, BS 972, BETWEEN S22 AND 23L,  AND AT BS 1000, LBL 4, WL 185.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND NUMBER 6 SLAT CRACKED AT LOWER L/E OF SLAT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORROSION AT BS 1112 TO 1121, RBL 22, WL 228, AT BS 986.5, LBL 55 TO RBL 55, WL 208 AND AT BS 1016, RBL 45 TO LBL 45, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM  CORRODED BS 328, WL 208, RBL 7 TO 56, AT BS 312, WL 208, LBL 15, AND AT BS 344, WL 208, LBL 60.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM LOWER HORIZONTAL CHORD CORRODED FROM BS 1112 TO 1121, RBL 22, WL 216.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND CRACK IN COCKPIT FLOOR AT BS 248, LBL 12, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 727E+3, BETWEEN S22 AND 23L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME DAMAGE AT BS 787, RBL 22, WL 156.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND CRACK ON FWD UPPER CORNER OF FWD GALLEY DOOR AT FASTENER HOLE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
EXPERIENCED BIRDSTRIKE TO NUMBER 2 ENGINE.  AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRDSTRIKE INSPECTION AND NOTED DAMAGE TO ENGINE INLET COWL.  NO DAMAGE TO ENGINE INTERNALLY.  PERFORMED TEMP REPAIR AND MAINTENANCE FERRIED AIRCRAFT TO DAL FOR REPAIRS.  REPLACED ENGINE INLET COWL PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH CRACK IN LEFT FUSELAGE SKIN JUST AFT OF FILLET FAIRING AT BS 767.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND COMPRESSION CHORD CRACKED AT BS 727, WL 199, RBL 13 TO 15.  REPAIRED PER TRAMCO EWO 95-0076.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING FROM  BS 727D TO 747, STRINGER 22L TO 24L.  REPAIREDPER TRAMCO EWO 95-0082.


REMARKS:
EVV - FLT 689 - AT APPROXIMATELY 3,000 FEET ON APPROACH, THE LANDING GEAR WAS DEPLOYED AND AN UNAFE LIGHT FOR THE  NOSEGEAR ILLUMINATED.  THE CREW RECYCLED THE GEAR, AND THE NOSE GEAR UNSAFE LIGHT AGAIN CAME ON.  THE FLIGHT MADE A FLY-BY AND A VISUAL INSPECTION WAS MADE.  NO EMERGENCY WAS DECLARED.  MAINTENANCE RESECURED THE CONNECTOR TO THE DOWNLOCK SWITCH ON THE NOSE GEAR.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
ATL-IAD - FLT 192 - DURING CLIMB-OUT, AUTO PRESSURIZATION WENT INOP AND ACFT DEPRESSURIZED AT APPROXIMATELY 10,000 FEET.  OXYGEN MASKS IN CABIN DEPLOYED AND CREW PRESSURIZED ACFT MANUALLY.  UPON ARRIVAL IN IAD, OXYGEN MASKS WERE STOWED ANDAUTO PRESSURIZATION PLACED ON MEL.


REMARKS:
ON CLIMB-OUT, PRESSURIZATION UNCONTROLLABLE IN AUTO AND MANUAL.  AUTO PILOT PREVIOUSLY ON MEL.  FLIGHT RETURNED TO ATL. REPLACED CABIN PRESSURE DIFFERENTIAL SENSOR.


REMARKS:
ATL-MEM - FLT 520 - REPORTED NUMEROUS CIRCUIT BREAKERS WERE POPPING IN COCKPIT.  CAPTAIN DECLARED AN EMERGENCY.  FLIGHTRETURNED TO ATL.  REMOVED AND REPLACED BUS CONT PANEL, OPS CHECK GOOD PER MM 24-52.


REMARKS:
IAD-ATL - FLT 175 - FLIGHT EXPERIENCED A LT SYSTEM HYDRAULIC LOW PRESSURE LIGHT, 300 PSI AFTER PERFORMING THE GEAR UPLATCH CHECK.  FLIGHT RETURNED TO IAD FOR REPAIRS.  REMOVED AND REPLACED HYDRAULIC PUMP NR 1 ENGINE.


REMARKS:
MDW-ATL - FLT 245 - DURING CLIMB-OUT, THE LT ENGINE FIRE WARNING CAME ON, RETARDED POWER LEVER, LIGHT WENT OUT.  RETURNED TO MDW.  FOUND 13TH STAGE BLANKING CAP OFF, BROKEN CLAMP.  REPLACED CAP AND CLAMP, ENGINE OPERATIONAL CHECK NORMAL.


REMARKS:
ATL-PHL - FLT 534 - EN ROUTE, OXYGEN MASKS DEPLOYED AUTOMATICALLY DUE TO USE OF AUTO PRESSURIZATION SYSTEM PREVIOUSLY PLACED ON MEL AS INOP.  RETURNED TO MANUAL PRESSURIZATION CONTROL AND REGAINED CONTROL.  MASK PANELS AT SEAT 4 AB ROW 6 AND 7 AB AND 11 AB DID NOT DEPLOY.  PLACED ON MEL 35-2-2 PAR F, G AND H.


REMARKS:
IAD - FLT 469 - WHILE AT THE GATE, EXPERIENCED FUMES AND SMOKE TO A MARGINAL DEGREE DUE TO THE APU.  PLACED APU ON MEL 49-1.


REMARKS:
ATL-IAD - FLT 368 - FLIGHT RETURNED TO ATL DUE TO RT FUEL HEAT STAYED ON CAUSING OIL TEMP TO EXCEED LIMITS PER MM 71-00.  REMOVED AND REPLACED NR 2 FUEL ANTI-ICE VALVE.


REMARKS:
MCO - FLT 8004 - ON TAKEOFF, LIFT DUMPER FAULTED.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE L3 SENSOR ON LT GEAR MM 32-63-03 PG 401.  RAN BITE TEST. NO FAULT ON LIFT DUMPERS, OPERATIONS CHECK NORMAL.  (W)


REMARKS:
PIT - FLT 114 - RUSHNG AIR SOUND WAS HEARD COMING FROM THE MED BY F/A.  CABIN BEGAN TO CLIMB.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE MAIN ENTRANCE DOOR SEAL.  PRESSURIZED AND OPERATIONS CHECK OK.  (W)


REMARKS:
PIT - FLT 1025 - AFTER TAKEOFF, THE CREW GOT A 'HYD SYS 2 LO QTY' ALERT.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND PRESSURE LINE 'B' NUT ON UPPER PUMP LOOSE AT QUICK DISCONNECT.  MAINTENANCE TIGHTENED FITTING. SERVICED, RAN ENGINE, ALL OPERATIONS NORMAL.  (W)


REMARKS:
ORF - FLT 124 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF.  FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE SWAPPED FWD AND AFT ZONE TEMP CONTROL BOXES.  OPS CHECK NORMAL.  SWAPPED FWD AND AFT ZONE TEMP CONTROL BOXES. OPS CHECK NORMAL.  SWAPPED UNITS BACK TO ORIGNAL CONFIGURATION, BITE TEST OF TEMP CONTROL UNITS OK.  (W)


REMARKS:
MCO - FLT 682 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF.  FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND FWD ELECTRICS BY DOOR UNLATCHED.  CLOSED AND SECURED DOOR.  SYSTEM CHECKS NORMAL.  (W)


REMARKS:
MCO - FLT 350 - EN ROUTE, THE NR 2 ENGINE OIL QUANTITY WENT TO ZERO.  OIL PRESSURE BEGAN TO DROP AND OIL TEMPERATURE REMAINED NORMAL.  FLIGHT CREW IDLED ENGINE AND DIVERTED TO MCO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FOUND OIL LINE FROM GEAR BOX TO OIL PRESSURE SWITCH CRACKED.  REPLACED LINE AND ADDED 16 QUARTS OF OIL.  RAN ENGINE, CHECKED CHIP DETECTORS, ALL CLEAN.  OIL PRESSURE OPS CHECK NORMAL.  (W)


REMARKS:
PIT - FLT 977 - ON TAKEOFF, THE CREW GOT A RT MAIN LANDING GEAR WARNING ON THE MFDU.  GEAR WAS RECYCLED BUT THE WARNINGREMAINED.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REMOVED A LARGE AMOUNT OF ICE AND SAND FROMTHE MLG.  OPERATION CHECKS NORMAL.  (W)


REMARKS:
DURING SCHEDULED CHECK, FOUND CRACKS IN THE FWD PRESSURE BULKHEAD WEB BETWEEN WL 184 TO 207, BS 178.  REPAIRED PER SWA RA 1-253-1240.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND TWO CRACKS IN THE I/B AND O/B FWD TEE CHORDS AT BS 178 PRESSURE BULKHEAD, LBL 5.7.  REPAIRED PER SWA RA 1-253-1240.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED JUST ABOVE POTABLE WATER SERVICE PANEL AT S25L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AT GATE, FOUND EMERGENCY FLASHLIGHT NOT TESTING.  REPLACED FLASHLIGHT PER BOEING M/M.


REMARKS:
DURING CLIMBOUT, NOTED PRESSURIZATION LEAKAGE AT FORWARD ENTRY DOOR, LOWER HINGE SEAL.  UNABLE TO MAINTAIN PRESSURE.  AIRCRAFT RETURNED TO SJC AND MADE AN UNEVENTFUL LANDING.  FOUND LOWER HINGE SEAL NOT SEATING PROPERLY.  REPOSITIONED SEALPER BOEING M/M, NO HELP.  REPLACED UPPER AND LOWER HINGE SEAL COVERS.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND CRACK IN UPPER CORNER OF LOWER HINGE SKIN CUTOUT AT FWD SERVICE DOOR.  REPAIRED PERSWA ACO 3189-52.


REMARKS:
DURING SCHEDULED B1 CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT BS 787.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION  CHECK, FOUND FUSELAGE SKIN DENTED AT BS 328, S21R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, BETWEEN S17L AND 17R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


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


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR AND FWD ENTRY EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACKPER BOEING M/M.


REMARKS:
AT ARRIVAL IN TPA, FLT 59, UNABLE TO OPEN L1 FWD ENTRY DOOR.  FOUND RETAINER RING MISSING ON UPPER DOOR GUIDE ARM LOCK PIN REINSTALLED UPPER DOOR GUIDE ARM LOCK PIN AND RING RETAINER PER MM 52-10.  OPS CHECKED OK.  (Z)


REMARKS:
MCI - DURING CHECK 'C', FOUND .3750 INCH CRACK IN FORWARD GALLEY DOOR OUTER SKIN, FROM FASTENER TO EDGE OF DOOR CUT-OUT, LOWER AFT CORNER.  INSTALLED REPAIR PER SSRM 53-30-206, PAGE 201 AND PAGE 204.  AIRCRAFT TOTAL TIME:  66,258 HOURS; 45,561 CYCLES.


REMARKS:
MCI - DURING CHECK C-2D, FOUND .75 INCH CRACK IN TOP INBOARD CORNER OF NR 1 ENGINE AFT ENGINE MOUNT CASTING.  REPAIRED BY INSTALLING DOUBLERS PER BOEING DWG 65C34994.  AIRCRAFT TOTAL TIME:  61,014 HOURS; 40,930 CYCLES.


REMARKS:
MCI - DURING C-2D, FOUND .50 INCH CRACK AT RIVET IN NOSE LANDING GEAR WHEELWELL PRESSURE WEB CEILING, ADJACENT TO LT IN-FLIGHT BRAKE BAR, STA 262, LBL 16.  STOP DRILLED CRACK AND REPAIRED PER SRM 53-10-11, PAGE 201.  AIRCRAFT TOTAL TIME:  64,911 HOURS; 44,167 CYCLES.


REMARKS:
CVG - FLT 698 - DURING APPROACH, LT MLG UNSAFE LIGHT REMAINED ON AFTER LANDING GEAR EXTENSION.  CYCLED LANDING GEAR ANDVISUALLY CHECKED LOCK.  CLEANED ELECTRICAL CONNECTOR ON DOWNLOCK SWITCH.  LANDING GEAR INDICATION SYSTEM OPERATION CHECKED NORMAL.  CHECK OP-15 - 4-17-94 - MCI.


REMARKS:
STL - FLT 106 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LT MLG UNSAFE LIGHT REMAINED ON.  RECYCLED LANDING GEARAND VISUALLY CHECKED LOCK.  REPLACED LT MLG UPLOCK SWITCH, MFG P/N H14-6.  LANDING GEAR POSITION AND WARNING SYTEM CHECKED NORMAL.  CHECK OP-15 - 4-17-94 - MCI.


REMARKS:
STL - FLT 269 - DURING APPROACH WITH ANTI-ICE ON, A LIGHT SMOKE APPEARED IN CABIN.  TURNED ANTI-ICE OFF, SMOKE DISSIPATED.  PERFORMED ENGINE HIGH POWER RUN, NO SMOKE OR ODOR DETECTED, AND LEAK CHECKED DUCTING.  CHECK C-1D - 9-14-94 - MCI.


REMARKS:
DURING CHECK C-6C, FOUND CORROSION AT STR 44, STA 1665 TO STA 1685, LEFT SIDE FUSELAGE.  INSTALLED STRINGER SPLICE PER SRM 53-13-00, PAGE 806E, 201.  AIRCRAFT TOTAL TIME:  58,443 HOURS; 21,909 CYCLES.


REMARKS:
DURING CHECK C-6C, FOUND CORROSION CRACK ON LEFT SIDE OF FUSELAGE STA 679, BETWEEN STR 37 AND STR 38.  INSTALLED REPAIRDOUBLER PER SSRM 53-30-02, PAGE 201.  AIRCRAFT TOTAL TIME:  58,443 HOURS; 21,909 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACK IN LT LOWER LAP FUSELAGE SKIN, STA 490, LT STRINGER LAP 26L.  CUT OUT CRACK ANDCORROSION PER SRM 53-30-03 AND REPAIRED PER SRM 53-30-3 FIG 14.  TOTAL CYCLES 42,197.


REMARKS:
ATL - FLT 73 - ON TAKEOFF, SPLIT FLAP CONDITION (I/B FLAPS WOULD NOT RETRACT BEYOND 5 DEGREES) USED ALTERNATED FLAP EXTENSION TO LOWER FLAPS.  FLIGHT RETURNED TO ATL.  REMOVED AND REPLACED I/B FLAP POSITION INDICATOR PER MM 27-51-00.  OPS CHECK OK.  (W)


REMARKS:
CLT - FLT 1133 - A VIBRATION WAS REPORTED IN THE FLOOR OF THE ACFT AND AFT JUMPSEAT AREA.  THE CREW DECIDED TO DIVERT TO CLT.  FOUND SENSE LINES TO LT AUGMENTATION VALVE AND PILOT PRESSURE REGULATORS LOOSE.  TIGHTENED LINES.  (W)


REMARKS:
CLT - FLT 685 - AFTER TAKEOFF, BOTH MLG WOULD NOT RETRACT WHEN SELECTED UP.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RT GEAR SEQUENCE VALVE BRACKET LEVER ATTACH PIN.  CHECKS OK ON GEAR RETRACTION.  (W)


REMARKS:
IND - ACCOMPLISHMENT OF JOB CARD J525-60-10 CALLS FOR SLIDE DEPLOYMENT.  UPON DEPLOYMENT, SLIDE MOUNTED LIGHTS DID NOT ILLUMINATE.  MAINTENANCE REMOVED AND REPLACED SERVICE DOOR EVACUATION SLIDE.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED AREA BS 947.5 RBL 48 INCHES SEAT TRACK ATTACH ANGLE.  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 2 SPOTS OF CORROSION 6 INCH BY 6 INCH AND 2 INCHES IN DIAMETER, 6 INCH BY 6 INCH AT FWD CORNER AND 2 INCHES IN DIAMETER AT AFT CORNER OF AFT CARGO DOOR CUTOUT.  REPAIRED PER SRM 51-10-2 AND SRM 51-40-02.  CORROSION TASK NR C53-100-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL OF FLOORBEAM, INSPECTION FOUND TOTAL OF 8 INCHES IN VARIOUS LOCATIONS CORROSION BS 328 BETWEEN BL 0 AND RBL 56.  REPAIRED PER TR 53-107-12.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 80 INCH CORRODED AREA BS 947 TO BS 1016 LT SIDE 'Z' ANGLE.  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 APPROX 46 INCHES BY 2 INCHES 'Z' ANGLE I/B OF GALLEY SERVICE DOOR WL 207.5 FROM BS 294.5 TO BS 328.  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 BY 34 INCHES CORRODED AREA 'Z' ANGLE AT FWD ENTRY DOOR STA. 310 TO 344.  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 BY 1 INCH CORROSION AREA ON LT ENTRY DOOR GIRT BAR ATTACH FITTINGS BOTH FRONT AND AFT.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND THREE AREAS, 1 INCH BY .250 INCH, .500 INCH BY .250 INCH,1 INCH BY 1.25 INCH CORRODED, FWD OF GALLEY SERVICE DOOR BS 270 TO BS 294.5 - 42.0 O/B OF BBL 0.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION OF SEAT TRACKS, FOUND CORRODED AREA APPROXIMATELY 29.0 INCHES BY 1.25 INCHES, BS 328 - 10 INCHES AFT OF BS 359.96 APPROX 20 INCHES O/B OF BBL 0.  REPAIRED PER SRM 53-00-52.  CORRODED TASK NR C3-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION OF INTERCOSTAL, FOUND 1 INCH BY 6 INCH CORRODED AREA, BS 947 THROUGH BS 967 LBL 48 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 SEVERAL NUT PLATE HOLES .25 INCH BY .25 INCH AREA CORRODED, BS 986 'T' CAP CLIP NUT HOLES.  REPAIRED PER TR 53-15-01A.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
CLT - FLT 460 - DURING FLIGHT THE NR 2 PITOT HEAT FAULTED.  C/B WAS NOT POPPED.  RECYCLED AND FAULTED AGAIN.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 2 PITOT HEAD.  PITOT AND HEAT CHECK NORMAL.  (W)


REMARKS:
PIT - FLT 883 - DURING PREFLIGHT, FOUND FLT DECK EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK, OPERATION CHECKS NORMAL.  (W)


REMARKS:
PHL - FLT 2394 - ON TAXI IN, LT NOSE WHEEL SHEARED OFF.  MAINTENANCE PINNED GEAR AND TOWED ACFT TO GATE.  MAINTENANCE REPLACED NOSE LANDING GEAR LOWER LEG ASSEMBLY.  (W)


REMARKS:
JFK - DURING CHECK C-3B, FOUND SKIN CRACK ON LEFT SIDE OF FUSELAGE BETWEEN STR 39 AND STR 40, STA 760.  INSTALLED DOUBLER REPAIR PER SRM 53-30-02, FIGURE 201.  AIRCRAFT TOTAL TIME:  63,846 HOURS; 17,917 CYCLES.


REMARKS:
JFK - DURING CHECK C-3B, FOUND A ONE INCH CRACK IN AFT PRESSURE BULKHEAD WEB.  INSTALLED REPAIR PER SRM 53-11-00, PAGE 808, FIGURE 805.  AIRCRAFT TOTAL TIME:  63,846 HOURS; 17,917 CYCLES.


REMARKS:
JFK - DURING CHECK C-3B, FOUND TWO RIVETS MISSING FROM AFTER PRESSURE BULKHEAD AND AREA BULGE AT SIX O'CLOCK POSITION.REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-11-00, PAGE 808.  AIRCRAFT TOTAL TIME:  63,846 HOURS; 17,917 CYCLES.


REMARKS:
JFK - DURING CHECK C-3B, FOUND SKIN CRACK ON RIGHT SIDE OF FUSELAGE OUT OF RIVET HOLE, STA 585, STR 30.  REPAIRED BY INSTALLING DOUBLER PER SRM 53-31-00, PAGE 828.   AIRCRAFT TOTAL TIME:  63,846 HOURS; 17,917 CYCLES.


REMARKS:
JFK - DURING CHECK C-3B, FOUND CORROSION ON FORMER RING AT SIX O'CLOCK POSITION IN AREA OF DRAIN HOLES, FORWARD SIDE OFPRESSURE BULKHEAD AFT OF LAVATORY TANK.  REMOVED CORROSION SECTION OF FORMER RING AND SPLICED IN NEW SECTION PER SRM 53-11-00, PAGE 815.   AIRCRAFT TOTAL TIME:  63,846 HOURS; 17,917 CYCLES.


REMARKS:
JFK - DURING CHECK C-3B, FOUND CRUSHED TRAILING EDGE OF NR 2 TRAILING EDGE FLAP, OUTBOARD END.  REMOVED DAMAGED WEDGE AND INSTALLED NEW SECTION PER SRM 57-54-00, PAGE 12.  AIRCRAFT TOTAL TIME:  63,846 HOURS; 31,029 CYCLES.


REMARKS:
JFK - DURING CHECK C-3B, FOUND CORROSION AT SIX O'CLOCK POSITION OF DRAIN HOLES FORWARD OF PRESSURE BULKHEAD STA 1809.REMOVED DOUBLER, REPAIRED FRAME PER SRM 51-50-03, AND REINSTALLED ORIGINAL DOUBLER.  AIRCRAFT TOTAL TIME:  63,846 HOURS; 31,029 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND 1.50 INCH CRACK AT RIGHT WING F/T, STA 555 CASTELLATION, UPPER STR 14.  INSTALLED NEWCHORD ANGLE PER DWG 1647070.  AIRCRAFT TOTAL TIME:  59,628 HOURS; 23,327 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A 1 INCH CRACK IN IWS 555 RIB UPPER CAP CASTELLATION, AT 14 STRINGERS FORWARD OF REARSPAR ABOVE RIB CUT OUT, LT WING.  REPAIRED UPPER RIB CAP AT IWS 555 ST STR 18 AND STR 19, PER ARA 867.  AIRCRAFT TOTAL TIME:  59,628 HOURS; 23,327 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK - FOUND .75 INCH CRACK IN RT WING INTERNAL UPPER RIB CAP, IN AFT RADIUS, IWS 555, OUTBOARD SIDE, SIXTH STRINGER FROM AFT STR 13.  INSTALLED UPPER CHORD ANGLE PER DWG. NR. 1647070.  AIRCRAFT TOTAL TIME 59,628 HOURS; 23,327 CYCLES.


REMARKS:
MCI - DURING CHECK C-2D, FOUND A 6 INCH CRACK AT STR 29R, BS 990, OUTBOARD SIDE OF BOTTOM RADIUS.  STOP DRILLED CRACK PER SRM 51-10-1, PAGE 6A, AND REPAIRED PER SSRM 53-10-213 AND TWA DWG. C03440.   ACFT TOTAL TIME:  37,342 HOURS; 24,204 CYCLES.


REMARKS:
STL - FLT 641 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MLG UNSAFE LIGHT REMAINED ILLUMINATED; CYCLED LANDING GEAR.  REPLACED RIGHT MLG DOWNLOCK SWITCH, MFG PN H14-6.  LANDING GEAR OPERATION AND POSITION AND WARNING SYSTEM CHECKED NORMAL.  CHECK C - 1-28-94 - MCI.


REMARKS:
MCI - DURING CHECK C-2D, FOUND CORROSION AT END OF LONGERON TIE TO STR 29R.  REMOVED CORROSION PER SRM 51-10-6, AND REPAIRED PER SSRM 53-10-213 AND TWA DWG. C03440.  AIRCRAFT TOTAL TIME:  37,342 HOURS; 24,204 CYCLES.


REMARKS:
JFK - DURING CHECK C-3B, FOUND CORROSION ON INNER SKIN AT STA 1512, BETWEEN STR 32 AND STR 33 UNDER CARGO COMPARTMENT FLOOR.  REMOVED CORROSION AND INSTALLED TEAR STRAP DOUBLER AND REPAIR DOUBLER PER SRM 53-31-00, PAGE 829, FIGURE 815.  AIRCRAFT TOTAL TIME:  63,846 HOURS; 17,917 CYCLES.


REMARKS:
DURING OP-17, FOUND FUSELAGE TOP SKIN AT STA 1110 TO STA 1120 DENTED LEFT AND RIGHT OF BL 0.  REPAIRED PER SRM 53-30-3,FIGURE 3.  AIRCRAFT TOTAL TIME:  36,843 HOURS; 22,210 CYCLES.


REMARKS:
STL - FLT 409 - AFTER TAKEOFF, A NOTICEABLE SMOKE AND ODOR APPEARED IN CABIN, DISSIPATED DURING CLIMB.  FOUND APU, MFG PN 381276-1, LEAKING OIL INTO AIR CONDITIONING SYSTEM.  PLACARDED APU INOPERATIVE. PER THE MINIMUM EQUIPMENT AND DISPATCH PROCEDURES MANUAL, 49-1.  CHECK C-1D - 1-395 - MCI.


REMARKS:
STL - DURING OP-15, FOUND A ONE INCH CRACK IN RT MAIN FRAME, COMING FROM AFT LOWER HOLE ATTACHED TO TRAPEZOID PANEL.  REPAIRED PER SSRM 53-60-102.  AIRCRAFT TOTAL TIME:  70,380 HOURS: 78,720 CYCLES.


REMARKS:
STL - FLT 297 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE RIGHT MAIN WHEELWELL DOOR LIGHT REMAINED ILLUMINATED; CYCLED LANDING GEAR.  FOUND DOOR HYDRAULIC ACTUATOR, MFG 7-3141-4, BYPASSING.  REPLACED RIGHT MLG DOOR ACTUATOR.  LANDING GEAR DOOR AND DOOR INDICATION SYSTEM OPERATION CHECKED NORMAL.  CHECK C-2 - 8-19-94 - MCI.


REMARKS:
STL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 8L, STA 718.  REPAIRED PER SRM 53-02, FIGURE 2, PAGE 2A.  AIRCRAFT TOTAL TIME:  70,380 HOURS; 78,720 CYCLES.


REMARKS:
STL - DURING OP-15, FOUND .25 INCH CRACK IN FORWARD CARGO BIN LONGERON 30 AND IN LONGERON SPLICE, STA 414. INSTALLED NEW SECTION OF LONGERON AND REPLACED SPLICE PLATE.  AIRCRAFT TOTAL TIME:  70,380 HOURS; 78,720 CYCLES.


REMARKS:
STL - DURING CHECK C, FOUND A .25 INCH CRACK IN VERTICAL STABILIZER RIGHT DORSAL FIN ATTACH ANGLE, FROM FASTENER HOLE TO EDGE.  REPAIRED PER SRM 51-30 AND TWA STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  38,864 HOURS; 35,359 CYCLES.


REMARKS:
STL - DURING OP-15, FOUND CRACK IN LONGERON 6R, STA 639 AND STA 658, APPROXIMATELY .1250 INCH TO .50 INCH.  REPAIRED PER SRM 53-02 AND TWA STANDARD PRACTICES.  AIRCRAFT TOTAL TIME:  70,380 HOURS; 78,720 CYCLES.


REMARKS:
MEM/ATL - FLT 147 - AIRCRAFT RETURNED TO GATE TO GET MORE PASSENGERS.  WITH ENGINES RUNNING TOW BAR BROKE AND TUG JACKKNIFED, CAUSING DAMAGE TO BELLY SKIN FROM STA 110 TO STA 150.  REPAIR TO BE MADE BY DOUGLAS AIRCRAFT CORPORATION.


REMARKS:
ATL/MDW - FLT 240 - RETURNED TO ATL DUE TO FLIGHT CREW COULD NOT PRESSURIZE AIRCRAFT IN AUTO OR MANUAL.  REPLACED PRESSURIZED REGULATION VALVE FOR LEFT AIR CONDITIONING PACK AND SEGMENT.


REMARKS:
ATL/BNA - FLT 558 - RETURNED TO ATL DUE TO FIRST OFFICER'S ADI FAILING DURING CLIMB-OUT.  REMOVED AND REPLACED NR 2 VERTICAL GYRO.  OPS CHECK GOOD PER MM 34.


REMARKS:
ATL/MIA - FLT 595 - RETURNED TO ATL DUE TO FIRST OFFICER'S GYRO WENT INOP ON CLIMB-OUT.  REMOVE AND REPLACE NR 2 GYRO AND REMOVE AND REPLACE INSTRUMENT AMP PER MM 34-00, OPS CHECK NORMAL.


REMARKS:
AT GATE, SLIGHT SMOKE NOTED IN CABIN AREA.  INSPECTED AND DETERMINED THE SMOKE  WAS FROM APU.  APU WAS DEACTIVATED PER MEL 49-1.  OPERATED AC PACKS TO DISSAPATE SMOKE.


REMARKS:
AFTER LEVELING AT 28,000, CABIN PRESSURE WARNING HORN SOUNDED.  CABIN ALTITUDE CONTINUED TO CLIMB.  USING STANDBY OR MANUAL SYSTEM, NO HELP.  CREW INITIATED DESCENT.  OXYGEN MASKS WERE DEPLOYED.  CREW REGAINED CABIN PRESSURE USING APU AND LEFT PACK.  AIRCRAFT DIVERTED TO BNA AND MADE AN UNEVENTFUL LANDING.  REPLACED RIGHT PACK CONTROL AND SHUTOFF VALVE.  PERFORMED CABIN DEPRESSURIZATION INSPECTION PER M/M.  OPERATION TESTED BOTH AC PACKS, OK.  PERFORMED CABIN PRESSURIZATION SYSTEM TEST OK.  CLEANED AND RESTOWED CABIN OXYGEN MASKS, AND REPLACED OXYGEN BOTTLE.


REMARKS:
DURING SCHEDULED CHECK, FOUND NOSE WHEEL WELL CEILING LEFT PRESSURE ACCESS PANEL CRACKED AT AFT I/B RADIUS.  REPAIRED PER SWA RA 1-253-1249.


REMARKS:
AFTER TAKEOFF, NUMBER 6 L/E SLAT WOULD NOT PROPERLY RETRACT.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.REPLACED NUMBER 6 SLAT ACTUATOR PER BOEING M/M.


REMARKS:
ATL/DFW - FLT 231 - AIRCRAFT RETURNED TO ATL DUE TO UNABLE TO PRESSURIZE IN AUTO OR IN MANUAL.  REMOVE AND REPLACE WATER SEPARATOR BAGS AFTER T/S AND FINDING BAGS CLOGGED WITH ICE.


REMARKS:
CLT - FLT 1243 - FLIGHT EN ROUTE PHL TO ATL WHEN 'A' SYSTEM HYDRAULIC QUANTITY INDICATED ZERO.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE ABOVE LEFT MAIN GEAR AND 'A' SYSTEM PRESSURE FILTERS AND BOTH CASE DRAIN FILTERS.  CHECKED GOOD.  (Z)


REMARKS:
PIT FLT 107 - ON TAKEOFF AFTER GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON.  THE GEAR WOULD NOT PRESSURIZE AND THE STALL INDICATION FAILURE LIGHT ILLUMINATED.  FLIGHT RETURNED TO PIT.  MAINTENANCE FOUND THE NLG STRUT FLAT AND REPLACED THE STRUT.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
SWF - FLT 1522 - ON TAKEOFF, THE NLG WOULD NOT RETRACT.  FLIGHT RETURNED TO SWF.  MAINTENANCE FOUND THE NLG STRUT FLAT,AND SERVICED THE STRUT WITH NITROGEN.  THE SCHRADER VALVE WAS REPLACED.  LEAK CHECKED GOOD.  (W)


REMARKS:
PIT - FLIGHT NR 1141 - ON CLIMB-OUT FROM CVG, THE WING ANTI-ICE MODULATING VALVE WOULD NOT OPEN.  NO HEATING OBSERVED ON TEMP GAUGE.  AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE WING-ICE MODULATING VALVE PER MM30-10-02.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
IND - ACCOMPLISHED SCHEDULED SID INSPECTION PSE 53.09.001A FORWARD CARGO DOOR JAMB AREA.  FOUND 1.25 INCH CRACK IN FRAME STATION 389 LONGERON 18R (VISUAL INSPECTION).  REMOVED AND REPLACED INTERCOSTAL.  (Z)


REMARKS:
PIT - DURING SCHEDULED SIP VISIT FOUND A 2.5 INCH CRACK IN THE REAR PRESSURE BULKHEAD BEAM NR 3 AT BODY LINE 750 RT.  REF - INSPECTION SIP 53-10-03 LFEC PROCEDURE.  INSTALLED WEB REPAIR PATCH AND NEW REAR FACE DOUBLER AND TWO 92.  REPAIR ANGLES PER USAIR EA 29285A.  (Z)


REMARKS:
PIT - FLT 0521 - THE CAPTAIN REPORTED A LOUD POPPING OR SNAPPING NOISE ON CLIMB-OUT.  AT THE SAME TIME THE MAIN DOOR ANNUNCIATOR LIGHT ILLUMINATED.  CAPTAIN DECIDED TO RETURN TO PIT.  MAINTENANCE REPLACED THE FORWARD ENTRY DOOR SWITCH.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
PIT - FLT NR 231 - DURING PREFLIGHT THE FLIGHT ATTENDANT FOUND EMERGENCY EXIT OVERHEAD LIGHTS INOPERATIVE.  MAINTENANCEREPLACED LIGHT PLATE ASSEMBLY TO THE EMERGENCY EXIT LIGHTS ON CENTER CABIN PER WING EXIT.  OPERATION CHECKS NORMAL.  (Z)


REMARKS:
LAX - FLT 721 - ON DESCENT WHEN LANDING GEAR WAS EXTENDED, RT MLG GREEN LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR AND ALTERNATE LANDING GEAR EXTENSION.  FOUND A-5 CARD, MFG PN 8-351-07, IN ELECTRONIC PROXIMITY SWITCH BOX.  LANDING GEAR POSITION AND WARNING SYSTEM CHECKED AND B.I.T.E. CHECKED NORMAL.  CHECK C-4A - 1 -19-95 - JFK.


REMARKS:
JFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE.STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A.  AIRCRAFT TOTAL TIME:  37,178 HOURS; 24,066 CYCLES.


REMARKS:
MCI - DURING OP-17, FOUND CRACK IN LT WING FUEL TANK IN TOP AFT NR 3 STRINGER, WS 656.50, AT RIB NR 6 ATTACH POINT.  REPAIRED PER SSRM 57-20-201, PAGE 215, FIGURE 207.  AIRCRAFT TOTAL TIME:  36,843 HOURS; 22,210 CYCLES.


REMARKS:
JFK - DURING TAKEOFF, HAD SMOKE IN CABIN.  TURNED OFF HIGH PRESSURE BLEED AIR.  FOUND APU LEAKING OIL.  REPLACED APU, MFG PN 381276-1.  APU OPERATION AND LEAK CHECKED NORMAL.  CHECK C-1D - 1-30-95 - MCI.


REMARKS:
STL - DURING CHECK-C, FOUND CORROSION ON HORIZONTAL STABILIZER HINGE SIDE LOAD FITTING, RT INBOARD SIDE.  REMOVED AND REPLACED FITTING PER SRM 51-10-01.  AIRCRAFT TOTAL TIME:  59.360 HOURS; 77,013 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND 1.1250 INCH CRACK IN RT WING FT CASTELLATION, STA 503, FORWARD OF STR 13.  REPAIRED PER SB 093-57-207 AND REPLACED CHORD PER DWG. NR 1647070.  AIRCRAFT TOTAL TIME:  59,528 HOURS; 23,327 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK FOUND A 1.25 INCH CRACK IN RT WING INTERNAL/LOWER RIB CAP AT AFT RADIUS, IWS 555, OUTBOARD SIDE, 6TH STRINGER FROM AFT.  REMOVED AND REPLACED LOWER FORWARD RIB CHORD PER SB 093-57-207, AND DWG. NR 1647070.  AIRCRAFT TOTAL TIME:  59,528 HOURS; 23,327 CYCLES.


REMARKS:
DURING CHECK C-9B, FOUND .25 INCH CRACK IN AFT BULKHEAD SKIN, STA 1363, ON OUTBOARD RIVET HOLE BETWEEN STIFFENER 15 AND16; FOUND 4 INCH CRACK AT OUTBOARD FRAME, LT WHEELWELL, AT NR 16 STIFFENER.  STOP DRILLED CRACKS AND REPAIRED WITH DOUBLERS PER SRM 53-11-00, FIGURE 850.  AIRCRAFT TOTAL TIME:  60,716 HOURS; 22,699 CYCLES.


REMARKS:
JFK - DURING CHECK C-9B, FOUND FORWARD END OF INTERCOSTAL, AFT BULKHEAD STA 1363, BROKEN AWAY FROM BULKHEAD BETWEEN STRINGERS 41L AND 42L, WHEELWELL.  INSTALLED CLIP ANGLE PER SRM 53-12-00.  AIRCRAFT TOTAL TIME:  60,716 HOURS; 22,699 CYCLES.


REMARKS:
JFK - DURING CHECK C-9B, FOUND A 28 INCH VERTICAL CRACK IN AFT BULKHEAD, STA 1363, THROUGH 8 STIFFENERS, WITH 7 STIFFENERS SHEARED.  STOP DRILLED CRACKS AND REPAIR PER SRM 53-11-00, FIGURE 851.  AIRCRAFT TOTAL TIME 60,716 HOURS; 22,699 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN RT WING FT RADIUS, NR 3 STRINGER FROM LOWER REAR SPAR TIE CLIP, STA 555.  AIRCRAFT TOTAL TIME:  59,528 HOURS; 23,327 CYCLES.


REMARKS:
JFK - DURING CHECK C-9B, FOUND A 3 INCH CRACK IN AFT BULKHEAD OUTBOARD CORD ANGLE, THROUGH BOTH LEGS AT WL 160, STA 1363, AND FOUND EXTERIOR CORD ANGLE CRACKED.  REPAIRED PER SRM 53-11-00, FIGURE 842.  AIRCRAFT TOTAL TIME:  60,716 HOURS; 22,699 CYCLES.


REMARKS:
JFK - DURING CHECK C-9C, FOUND CRACK IN OUTBOARD AILERON DAMPER ATTACH FITTING REAR SPAR OF LT WING INBOARD EAR.  REMOVED AND REPLACED FITTING PER SRM 51-10-01, PARAGRAPH D.  AIRCRAFT TOTAL TIME:  65,236 HOURS; 17,223 CYCLES.


REMARKS:
JFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER.  STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850.  AIRCRAFT TOTAL TIME:  60,716 HOURS; 22,699 CYCLES.


REMARKS:
OMA - FLT 142 - DURING CRUISE, HAD ODOR AND SMOKE IN COCKPIT.  ELECTRICAL SYTEMS AND AIR CONDITIONING SYSTEM APPEARED NORMAL.  CHECKED ELECTRICAL PANELS IN COCKPIT AND ELECTRICAL EQUIPMENT COMPARTMENT AND NO ABNORMALITIES FOUND.  CHECK C-2D - 1-13-94 - MCI.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION OF STRINGER, FOUND WITH 7 INCH CORRODED AREA BS 353 TO BS 360 S-28 R.  REPAIRED PER DRAWING 69-48948.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 2 INCH BY 10 INCH CORRODED AREA BS 987 TO BS 1006 S-27 L.  REPAIRED PERSRM 53-10-3 FIG 1.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 30 INCH CORROSION BS 967 LBBL 18 TO RBBL 40.  REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 2 INCH BY 42 INCH CORROSION FLOORBEAM BS 986 RBL 3 TO RBL 45.  REPAIREDPER TR 53-10-05C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND .25 INCH CORROSION TOP SIDE OF SUPPORT BEAM, BS 1006 TO BS 1016 LBL 8 INCHES.  REPAIRED PER SRM 51-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURNG Q-6 CHECK VISUAL, INSPECTION FOUND 3 INCH BY 2 INCH CORRODED INTERCOSTAL BETWEEN FLOORBEAM  FS 328 AND 344 RBL 12.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 7 INCH BY 2 INCH CORROSION INTERCOSTAL BETWEEN FLOORBEAM FS 312 AND 328RBL 12.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 2 INCH BY 5 INCH CORROSION ON FLOORBEAM FS 312 RBL 45.  REPAIRED PER TR53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURNG Q-6 CHECK VISUAL, INSPECTION FOUND 4 INCH BY 2 INCH CORROSION FLOORBEAM FS 312 RBL 21.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 VISUAL, INSPECTION FOUND 5 INCH BY 3 INCH CORROSION FLOORBEAM FS 312 RBL 7.  REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 3 INCH BY 21 INCH CORROSION FLOORBEAM FS 328 RBL 29 TO RBL 50.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL , INSPECTION FOUND 1 INCH BY 6 INCH CORROSION AND 1 INCH BY 4 INCH CORROSION STA 306 LBL 12 TO 16, LBL 28 TO 34 ON HAT CHANNEL.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 2 INCH BY 40 INCH CORRODED AREA ON TOP SURFACE OF AFT SERVICE DOOR 'Z' ANGLE (BS 947 TO 1000) WL 208.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 16 INCH BY .50 INCH CORRODED AREA ON FRAME AT BS 360 RBL 10 INCHES TO LBL 6 INCHES.  REPAIRED PER SRM 53-10-04.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 2 INCH BY 30 INCH CORRODED AREA ON UPPER SURFACE OF 'Z' ANGLE AFT ENTRYDOOR THRESHOLD AREA BS 947 TO 987.  REPAIRED PER SRM 51-10-6.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
PIT - FLT 358 - ON CLIMB-OUT, THE ACFT WOULD NOT PRESSURIZE IN EITHER THE AUTO OR MANUAL MODE.  CREW DECIDED TO DIVERT TO PIT.  MAINTENANCE INSPECTED THE OUTFLOW VALVE, ALL DUCTING, DOORS, AND FRAMES.  NO ABNORMALITIES WERE FOUND.  THE ACFT WAS PRESSURIZED TO 7.5 PSI.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
DCA - FLT 545 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD HAD AN ELECTRICAL ARCING WHICH IMMEDIATELY CAUSED APPROXIMATELY TWENTY CRACKS IN THE OUTSIDE WINDOW.  THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO DCA.  MAINTENANCE REPLACED THE WINDSHIELD.  AN OPERATIONAL CHECK OF THE WINDSHIELD ANTI-ICING AND ANTI-FOGGING SYSTEMS WERE CHECKED.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 2350 - ON CLIMB-OUT, THE RT ENGINE HYDRAULIC PUMP FAILED.  CREW DECIDED TO RETURN TO CLT.  MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAULIC PUMP.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 1531 - ON CLIMB-OUT, THE CAPTAIN ADVISED THAT HE LOST ANTI-ICE CAPABILITIES.  FLIGHT DIVERTED TO CLT.  MAINTENANCE REPLACED THE ANTI-ICE TAIL VALVE.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 1005 - AFTER TAKEOFF, THE CAPTAIN RAISED THE GEAR, BUT GOT AN UNSAFE NOSE GEAR INDICATION LIGHT.  THE GEAR WAS LOWERED, BUT THE UNSAFE NOSE GEAR LIGHT REMAINED.  THE CAPTAIN THEN USED ABNORMAL PROCEDURES TO LOWER THE NOSE GEAR, AND RECEIVED A GREEN LIGHT FOR NOSE GEAR DOWN.  AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO GATE.  MX INSPECTED THE LANDING GEAR AND ALL COMPONENTS.  NO ABNORMAL CONDITIONS WERE NOTED.  A GEAR SWING WAS PERFORMED, ALL OPERATING PARAMETERS WERE WITHIN LIMITS.  NO OTHER DISCREPANCIES WERE NOTED.  (W)


REMARKS:
FLT 11, INBOUND TO ATL, NR 3 ENGINE WAS SHUTDOWN IN FLIGHT, WOULD NOT RESPOND TO THROTTLE MOVEMENT, WENT TO MAX POWER INDICATIONS.  REMOVED AND REPLACED NR 3 ENGINE FUEL CONT PER MM 73-21-2, WHEN RIGGING FOUND NUT MISSING AND CRANK OFF SHAFT AT PYLON CONNECTION POINT.  REINSTALLED CRANK AND INSTALLED NUT.  TRIMMED NR 3 ENGINE IAW 71-00.  OPS CHECKED OK.  LEAK CHECK OK.  (Z)


REMARKS:
AFTER TAKEOFF, LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED.  RECYCLED GEAR AND LIGHT EXTINGUISHED.  AIRCRAFT LANDED WITHOUT INCIDENT.  INSPECTED, TIGHTENED RED LIGHT BASE, AND OPERATION CHECKED PER BOEING M/M.  ON NEXT FLIGHT EXPERIENCEDRED LIGHT FLICKERING IN FLIGHT.  REPLACED LEFT MAIN GEAR UPLOCK SENSOR PER BOEING M/M.


REMARKS:
FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT AND BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY FLOOR TRACK LIGHTING AND RIGHT AFT EXTERIOR LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT FUSELAGE SKIN LAP, BS 480, S10L, AT BS 500B+10, S14L AND AT BS 530, S10R.  REPAIRED PER SWA RA 1-253-1251 AND SI 8615-53.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION NEAR SEVERAL FASTENERS IN PRESSURE WEB AT I/B SIDE OF STRAP, BS 178, LBL 5.7, FROM WL 205 TO 186.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT BS 178 PRESSURE BULKHEAD VERTICAL T-ANGLE AT LBL 5.7 AT WL 184,  IN THE I/B AND O/B FLANGE RADIUS.  REPAIRED PER SWA RA 1-253-1250.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FORWARD SERVICE DOOR CUTOUT CRACKED 1 INCH AT AFT LOWER RADIUS.  REPAIRED PER SWA RA 1-353-1252.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER RADIUS HINGE CUTOUT CRACKED .3750 INCH.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND TIE STRAP CRACKED AT BS 328, LOWER E & E COMPARTMENT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD PRESSURE WEB FROM BL0 TO RBL 17, WL 184 TO 230, UNDER STRAPS AND ANGLES.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 818 TO 828, AT STRINGER 4L.  REPAIRED PER TRAMCO EWO 95-0200.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 867, 860, 870, 887, 888, AT STRINGER 4L.  REPAIRED PER TRAMCO EWO 95-0200.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 767, AT STRINGER 4L.  REPAIRED PER TRAMCO EWO 95-0200.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 768, AT STRINGER 4R.  REPAIRED PER TRAMCO EWO 95-0200.


REMARKS:
DURING INSPECTION OF AD 91-07-11, FOUND LOWER ANGLE OF THRESHOLD AREA BETWEEN BS 950E AND BS 990 EXFOLIATED UNDER AND AROUND SEVERAL NUTPLATES.  BLENDED OUT CORROSION, FOUND OUT OF LIMITS, FABRICATED REPAIR FILLERS AND STRAPS, TREATED PRIMED, AND INSTALLED PER SRM 51-30-2, SRM 51-40-4, AND SRM 51-10-2.


REMARKS:
LGA - FLT 1156 - DURING FLIGHT THERE WAS DEPRESSURIZATION.  THE NR 1 PACK FAULTED.  CAPTAIN GOT THE CABIN PRESSURE UNDER CONTROL.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE OPERATED NR 1 PACK WITH ENGINE BLEED AND APU AIR.  CHECKS SATISFACTORY.  NO FAULT PRESENT.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREWHOLE 1 INCH BY 1 INCH INTERCOSTAL AT RBL 10 BETWEEN 312 AND 328.  REPAIRED PER TR 51-70-12 SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
OMA - FLT 142 - DURING CRUISE HAD ODOR AND SMOKE IN COCKPIT.  ELECTRICAL SYSTEMS AND AIR CONDITIONING SYSTEM APPEARED NORMAL.  CHECKED ELECTRICAL PANELS IN COCKPIT AND ELECTRICAL EQUIPMENT COMPARTMENT AND NO ABNORMALITIES FOUND.  CHECK C-2D - 1-13-93 - MCI.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM SUPPORT STRAPS CRACKED AT BS 312, AT CENTERLINE, AT 31.75 INCHES TO RIGHT OF CENTERLINE, AND AT 11.25 INCHES TO THE LEFT OF CENTERLINE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND BELTFRAME CRACKED AT BS 360, S26L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND A .3750 INCH CRACK AT UPPER RADIUS OF HINGE CUTOUT ON FUSELAGE AFT ENTRY DOOR CUTOUT.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT DIM.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


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


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN FLOOR TRACK LIGHTS AND RIGHT AFT EXTERIOR EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 22 INCH CORRODED AREA ON INTERCOSTAL, BS 947 TO BS 967 RBL 18TO RBL 24 TO RBL 40.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  REF USAA950126.


REMARKS:
CLT - FLT 2442 - ON CLIMB, AIRFRAME VIBRATION AT HGH POWER SETTNGS.  NO VIBRATION AT IDLE POWER DESCENT OR LOW POWER SETTING.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE PERFORMED ENGINE RUN AT ALL POWER SETTINGS.  VIBRATION INDICATION NEVER EXCEEDED .5.  PERFORMED AVM SIGNAL CHECK, BITE CHECKED OK.  FOUND WING TO BODY FAIRING SEAL LOOSE.  SEALED WING TO BODY FAIRINGS.  OK FOR SERVICE.  (W)


REMARKS:
MLB - FLT 1926 - DURING MISSED APPROACH AT MCO. FLAPS WOULD NOT RETRACT.  FLIGHT DIVERTED TO MCO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE INSPECTED ALL FLAP ASSEMBLYS, JACKSCREWS, AND CARRIAGES.  COULD NOT DUPLICATE ANY FAULTS.  FOUND RT O/B TRAILING EDGE FLAP 'A' ARM BELLCRANKS VERY WORN AT ROD END ATTACHMENT.  REPLACED SAME, OPS CHECK NORMAL.  (W)


REMARKS:
PIT - FLT 576 - ON CLIMB-OUT, CREW HAD NO CONTROL OVER RT AIR MIX VALVE.  VALVE WENT FULL COLD AND WAS NOT CONTROLLABLEIN MANUAL OR AUTO.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED RT PACK AIR MIX VALVE.   OPS CHECK, LEAK CHECK GOOD.  (W)


REMARKS:
MKE - FLT 293 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT.  FLIGHT RETURNED TO MKE WITHOUT INCIDENT.  INSPECTED NOSE GEAR RETRACT AND EXTEND MECH.  NO DEFECTS NOTED.  SERVICED NOSE GEAR STRUT, IAW DOUGLAS MM 32-21-02.  GEAR SWING CHECKS GOOD.  (W)


REMARKS:
BWI - FLT 198 - FLIGHT DIVERTED TO BWI DUE TO E/M 'R ENG TAI VALVE'.  PERFORMED MAINTENANCE PER FIMR PROCEDURES.  VALVECHECKS GOOD.  (W)


REMARKS:
PIT - THE LT EMERGENCY SLIDER SQUIB DOES NOT TEST IN NR 1 POSITION, AND THE RT SLIDER SQUIB DOES NOT TEST IN THE NR 2 POSITION.  MAINTENANCE CLEANED THE SWITCHES AND RELAYS.  (W)


REMARKS:
BWI - FLT 194 - AFTER TAKEOFF, THE CAPTAIN'S ADI DISPLAY FAILED.  FLIGHT RETURNED TO BWI.  MAINTENANCE REPLACED THE CAPTAIN'S EFIS CONTROL PANEL.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORRODED AREAS ON GIRT BRACKETS 2 PLACES.  FWD ENTRY STA 312 AND STA 244.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION OF FLOOR SUPPORT, FOUND SURFACE CORROSION AROUND NUTPLATES 1 INCH BY 1 INCH SEVERAL PLACES 20 INCHES RBL BETWEEN STA 807 AND STA 907.  REPAIRED PER SRM 53-00-53.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND .25 INCH BY .5 INCH GOUGE STA 887 LBL 25.  REPAIRED PER SRM 53-00-52 FIG 204.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION , FOUND .75 INCH BY .75 INCH 6 AREAS CORROSION 4 INCHES AFT OF BS 727 D FROM BL 0 TO S-28 L BL 0 TO S-28 R UNDERSIDE OF ANGLES WHERE NUTPLATE ATTACHES.  REPLACED PER T/R 53-10-06, SRM 53-00-53, AND BAC DRW.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND TWO CORROSION AREAS 1.0 INCH BY 1.0 INCH AND .500 BY 1.0 INCH, BETWEEN FWD GALLEY BULKHEAD AND BS 294.5, 42.0 INCHES FROM BBL 0.  REPAIRED PER BOEING DRAWING 69-40352-6.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION WIDTH OF FLOORBEAM, FLOORBEAM HOLES CORRODE AT BS 1016.  REPAIRED PER TYPICAL REPAIR 53-10-05.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 20 INCH CORROSION ON FLOORBEAM AT BS 344 FROM BL 0 TO LBL 24INCHES.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR.  C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 31.0 INCH BY 2 INCH BS 328 FLOORBEAM T-CAP.  REPAIRED PER SRM53-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 19 INCH CORRODED AREA ON INTERCOSTAL AT BS 967 TO BS 986 RBL 18 INCHES.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED AREA ON INTERCOSTAL AT BS 947 TO BS 967 RBL 40.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.   (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 22 INCH CORRODED AREA ON INTERCOSTAL, BS 947 TO BS 967 RBL 18TO RBL 24 TO RBL 40.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  REF 95ZZZW195.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 24.6 INCH BY 1.3 INCH CORROSION BS 1006 TO BS 1016 LBL 28 INCHES.  REPAIRED PER SRM 51-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 24 INCH BY 1.3 INCH CORROSION ON INTERCOSTAL BS 1006 TO BS 1016 RBL 18 INCHES.  REPAIRED PER SRM 51-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT -  DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 SQUARE INCHES CORROSION ON INTERCOSTAL AT BS 947 TO BS 967 AT LBL 30.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORROSION ON INTERCOSTAL AT BS 312 TO BS 328 AT LBL 12 INCHES.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY .500 INCH CORROSION ON INTERCOSTAL BETWEEN BS 328 AND BS 344,25 FROM BBL 0.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUMEROUS SCREW HOLES .500 INCH BY 500 INCH, INTERCOSTAL BETWEEN BS 312 AND BS 328, 11.5 INCHES FROM BBL 0.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 30 INCH CORRODED AREA LT LAVATORY AFT FWD BULKHEAD.  REPAIREDPER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 30 INCH CORRODED AREA RT AFT LAVATORY FWD BULKHEAD.  REPAIREDPER SRM 51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 VISUAL INSPECTION, FOUND 3 INCH BY 59 INCH CORRODED AREA, BS 947 TO 1006 LT SIDE.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-2.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 5 SQUARE INCHES OF CORROSION BS 947 TO BS 1006.  REPAIRED PER SRM 51-10-2 AND SRM 51-10-11.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER BENEATH PAINT 1 INCH BY 10 INCH BS 350 TO 360 S-25 R.  REPAIRED PER SRM 53-00-03.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER BENEATH PAINT 1 INCH BY 10 INCH BS 350 TO 360 S-25 L.  REPAIRED PER SRM 53-00-03.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (W)


REMARKS:
JAX - FLT 7004 - AT FL 310, THE CREW EXPERIENCED ACFT VIBRATION AND SURGE IN THE LT ENGINE EPR.  THE CREW SET THE LT ENGINE BACK TO IDLE THEN SHUTDOWN THE ENGINE.  THE ACFT WAS SLOWED DOWN TO 180 KNOTS AND HAD A SMOOTH RIDE TO JAX.  THE SINGLE ENGINE TIME WAS APPROXIMATELY 12 TO 15 MINUTES.  THE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LT ENGINE.  OPERATIONS CHECKED GOOD.  SUSPECT ICE INGESTION IN REMOVED ENGINE.  (W)


REMARKS:
LGA - FLT 488 - AT 500 FEET ON CLIMB-OUT, HAD A SUDDEN LOUD RUMBLE AND HIGH VIBRATION IN NR 2 ENGINE.  WHEN POWER HAS REDUCED AT LEVEL OFF, NOISE DECREASED AND VIBRATION DECREASED TO NORMAL LEVELS.  SUSPECTED BIRDSTRIKE.  FLIGHT RETURNED TO LGA WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED FAN BLADES NR 21, 4, 23, 5, 24, 6, 25, AND 2, DUE TO BIRD INGESTION FOD.  (W)


REMARKS:
FLT 462 - TPA-IAD - FLIGHT ATTENDANT REPORTED FAINT SMELL OF SMOKE IN CABIN ON APPROACH AT 8000 FEET.  PRESSURE DUMPED AT SAME TIME.  BOTH AIRFOIL AND ENGINE ANTI-ICE WERE ON.  DUCT TEMP AND DUCT PRESSURE WERE OK.  NO AIRFOIL TEMP HIGH LIGHTS ON.  OPERATIONS CHECKED BOTH AIR CONDITIONING SYSTEMS PER MM 21-00 AND COULD NOT DUPLICATE.  PRESSURE TO 20 IN HG.  AIR CONDITION PRESSURE OK.  CAPTAIN ON BOARD DURING OPS CHECK AND AGREED SYSTEM OK.  CAPTAIN AND FIRST OFFICER BOTH REPORTED SMELLING NO SMOKE, ONLY 1 FLT ATTENDANT REPORTED FAINT SMELL.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 1388 RT SIDE OF VERTICAL STAB ATTACH ANGLE.  STOP DRILLED AND INSTALLED REPAIR ANGLES PER SRM 53-05 FIG 84 AND USAIR EA NR 29735.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND SEVERAL CRACKS IN LONGERON 17L AT STATION 280.  REPLACED LONGERON AND SPLICED PER SRM 53-02 FIG 2 AND USAIR EA NR 2893.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .5 INCH AND .75 INCH CRACK IN STATION 1452 LONGERONS 3R AND 3L.  MANUAL NEW CLIP AND REPAIRED PER SRM 53-03.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT STRINGER 1388 AFT SIDE OF CANTED BELT FRAME RT SIDE ATTACH ANGLE.  INSTALLED ATTACH ANGLE STRAP REPAIR PER SRM 55-02 FIG 26.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION ACCOMPLISHED CORROSION TASK NR C58-53300 AND FOUND LEVEL I CORROSION AT STATION 1388 FLOOR SUPPORT RT LAV FLOOR BEAM.  REMOVED CORRODED AREA AND SPLICED IN REPAIR ANGLE PER USAIR TYPICAL REPAIR 53-10-14.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND A 3 INCH CRACK AT STATION 885 RT CUSP MEMBRANE.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 1 AND 2.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.25 INCH CRACK AT STATION 906 RT CUSP MEMBRANE.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2.  (Z)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION ACCOMPLISHED CORROSION CONTROL TASK ITEM NR C51-53300 AND FOUND LEVEL II CORROSION ATTHE FORWARD CARGO DOOR HINGE ATTACH FLANGE CLIPS.  MANU NEW CLIPS AND INSTALLED PER SRM 53-11-2.  (Z)


REMARKS:
BWI - FLT EN ROUTE DCA TO CMH WHEN CAPTAINS OUTER WINDSHIELD PANE CRACKED.  FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENACNE REPLACED CAPTAINS L1 WINDSHIELD.  (Z)


REMARKS:
CLT - FLT 1133 - THE LEFT ENGINE OIL QUANTITY DROPPED TO ZERO, AND THE OIL PRESSURE ALSO DROPPED.  THE ENGINE WAS SHUTDOWN AND FLIGHT DIVERTED TO CLT.  MAINTENANCE REPLACED THE OIL LINE TO THE OIL PRESSURE SWITCH AND THE FILTERS.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
PIT - FLT 1560 - AFTER CLIMB AND ENTERING CRUISE, THE TAIL COMPARTMENT TEMPERATURE LIGHT ILLUMINATED.  THE CREW DECIDEDTO RETURN TO PIT.  MAINTENANCE REPLACED BOTH LEFT AND RIGHT TAIL TEMPERATURE SENSORS.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
IND - DURING CX-5 CHECK INSPECTION ACCOMPLISHED SID INSPECTION PSE 53.09.001A, FOUND .5 INCH CRACK AT STATION 389 LONGERON 17R.  (VISUAL INSPECTION).  CUT OUT DAMAGED AREA, INSTALLED FILLER/DOUBLER TYPE REPAIR PER DAC SRM 53-04 FIG 35 AND USAIR EA 29574.  (Z)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND A .75 INCH CRACK AT STATION 101 BETWEEN LONGERON 27R AND 28R SKIN.  INSTALLED DOUBLER TYPE REPAIR PER SRM 53-01 FIG 2 SHEET 3.  (Z)


REMARKS:
RDU - FLT 0103 - THE RIGHT GENERATOR TRIPPED OFF LINE DURING FLIGHT.  THERE WAS NO CROSS TIE LOCKOUT.  THE FLIGHT DIVERTED TO RDU.  MAINTENANCE REPLACED THE RIGHT VOLTAGE REGULATOR.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
CLT - FLT 1857 - THE NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION.  THE CREW DECIDED TO RETURN TO CLT.  MAINTENANCE CLEANED THE NOSE GEAR UP PROXIMITY SWITCH.  THE GEAR WAS CYCLED THREE TIMES WITH NO PROBLEMS.  (Z)


REMARKS:
PIT - FLIGHT 1181 - AFTER TAKEOFF, THE RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED.  THE CREW RECYCLED THE GEAR AND GOT THREE GREEN LIGHTS.  AFTER THE SECOND RETRACTION THE UNSAFE LIGHT STILL REMAINED ILLUMINATED.  ON FINAL APPROACH JUST BEFORE GEAR EXTENSION, THE RED LIGHT WENT OUT GIVING NORMAL GEAR UP INDICATION.  MAINTENANCE REPOSITIONED THE HARNESS LANDING GEAR.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
MIA - FLT 2240 - AFT CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF.  FLIGHT RETURNED TO MIA WHERE LANDING WAS WITHOUT FURTHERINCIDENT.  MAINTENANCE FOUND CARGO STRAP WEDGED BETWEEN ROLLER AND CAM.  REMOVED STRAP AND CHECKED OPERATION OF DOOR WARNING SYSTEM.  OPS CHECK NORMAL  (Z)


REMARKS:
GSO - FLT 884 - AFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT.  RECYCLED GEAR.  ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT.  MAINTENANCE COULD NOT DUPLICATE NLG DISCREPANCY.  ALL INDICATIONS NORMAL.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 4 INCH BY 2 INCH CORRODED AREA STA 500 D STR 27 LT.  REPAIRED PER SRM 53-00-07 FIG 204.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH IN LENGTH CORROSION SEVERAL AREAS, BS 947 TO BS 1006 'Z' ANGLE RT AFT SERVICE DOOR.  REPAIRED PER SRM 51-70-11.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND CORROSION TWO AREAS 2 INCH BY 2 INCH, 54.0 INCH BY 1 INCH 'Z' ANGLE FWDGALLEY SERVICE DOOR BS 294.5 TO BS 344.  REPAIRED PER BOEING DRAWING 65-45875 AND SRM 51-10-02 PG 15.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND 8 SQUARE INCHES OF CORROSION 'Z' ANGLE FWD ENTRY DOOR.  REPAIRED PER SRM51-10-02.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
BOS - FLT 83 - UNABLE TO PRESSURIZE ACFT ON CLIMB-OUT.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND FWD OUTFLOW VALVE FOR DEFECTIVE SWITCH OPERATION.  ALL CHECKS NORMAL.  (W)


REMARKS:
PHL - FLT 1926 - UNABLE TO PRESSURIZE ACFT ON CLIMB.  FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENACNE FOUND RT PACK NOT ABLE TO SUPPLY SUFFICIENT AIRFLOW.  RELEASED ON MEL 21-1.  REPLACED AIR CONDITIONING ACCESSORY UNIT M324.  OPS CHECK NORMAL.  CLEARED MEL.  (W)


REMARKS:
FLL - FLT 44 - DURING CLIMB AT APPROX 1,000 FEET FLAPS SET, ACFT EXPERIENCED VIBRATION WHICH INCREASED WITH AIRSPEED.  FLIGHT RETURNED TO FLL WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE FERRIED ACFT TO CLT.  TIGHTENED ROLLERS ON BOTH I/B ENDS AND ON BOTH I/B FOREFLAP TOGGLES.  CYCLED FLAPS, NO FURTHER DEFECTS NOTED ON TEST.  (W)


REMARKS:
PHL - FLT 63 - AFT CARGO DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF.  FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPAIRED 3 BROKEN WIRES AT AFT CARGO DOOR SWITCH.  OPS CHECK GOOD.  (W)


REMARKS:
PIT - FLT 428 - AT FL 330 GOT EXCESSIVE CABIN ALTITUDE MESSAGE.  CABIN WAS APPROACHING 11,000 FEET.  CREW DID EMERGENCYDESCENT IAW PROCEDURES.  ALSO, TRIED MANUAL PRESSURIZATION BUT HAD NO RESPONSE.  ACFT DIVERTED AND LANDED WITHOUT INCIDENT.  MAINTENANCE PRESSURIZED ACFT.  LEAK DOWN RATE WITHIN LIMITS.  FOUND COOLING OUTFLOW VALVE STICKING.  REPLACED VALVE, TEST OK.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 541 AND 634, LT SIDE TIE DOWN TRACK.  INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-20-09A.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND TWO EACH CRACKS BOTH .5 INCH, STA 1418 LONGERON 2 LT BELTFRAME.  CUT OUT DAMAGE AREA AND INSTALLED FILLER, DOUBLERS PER SRM 53-03 FIG 32 SHT 4 PG 135.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND DENT BEYOND LIMITS .065 INCH DEEP FUSELAGE STA 345 LONGERON 20 RT.  CUT OUT DAMAGED SKIN AND INSTALLED PLUG FILLER AND INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND EA 26628 REV B.  (W)


REMARKS:
DURING Q-4 CHECK, INSPECTION FOUND DENTS BOTH .063 INCH DEEP STA 229, LONGERONS 22 TO 26 LT, IN SKIN.  CUT OUT DAMAGE SKIN AND INSTALLED FLUSH REPAIR WITH INTERNAL FINGER DOUBLER.  PER SRM 53-04 FIG 26.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 823 LONGERON 29 RT, IN SKIN.  CORROSION TASK NR C22-57301.  INSTALLED DOUBLER PER SRM 53-04 FIG 53.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 800 BETWEEN LONGERONS 28 RT AND 29 RT SKIN.  CORROSION TASK NR C22-57301.  INSTALLED DOUBLER PER SRM 53-04 FIG 53.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND 1 INCH CRACK STA 1338 CENTER TOP OF AFT PASS DOCK IN STIFFENER.  STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE DOUBLERS PER SRM 53-01 FIG 2 SHEET 4.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND .52 INCH CRACK STA 1437 BETWEEN LONGERON 2 AND 3 LT, IN SKIN.  CUT OUT DAMAGE AND INSTALLED PLUG REPAIR DOUBLER PER SRM 53-04 FIG 38.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .5 INCH STA 1418 LONGERON 2RT.  SPLICED IN NEW SECTION OF LONGERON, PER SRM 53-02 FIG 5.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACKS 2 EACH .25 INCH BY .1250 INCH RT WING FUEL PANELS ACCESS DOOR AREA, LEADING EDGE SKIN.  STOP DRILLED CRACKS, MFG DOUBLERS AND INSTALLED REPAIR PER SRM 57-06B PAGE 9 FIG 3.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION  FOUND .75 INCH CRACK STA 1309 LONGERON 12 FEET.  INSTALLED LONGERON AND SPLICE PER SRM USAIR TYPICAL REPAIR 53-10-17.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND LIGHTNING STRIKE .375 INCH BY .035 INCH DEEP STA 1172 LONGERON 30 IN SKIN.  INSTALLED EXTERNAL DOUBLER, DAMAGE WAS BLENDED.  PER SRM 53-04 FIG 38 VIEW G USAIR EA 29390.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 541 RT SIDE TIE DOWN TRACK.  REMOVED CORROSION, CLEANED, ALODINE, PRIMED, INSTALLED 'L' ANGLES, PER USAIR TYPICAL REPAIR 53-20-09A.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 693 LT SIDE TIE DOWN TRACK.  REMOVED CORROSION AND INSTALLED REPAIR STRAPS PER USAIR TYPICAL REPAIR 53-20-09A.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 332 AND 389 RT I/B SEAT TRACK.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND GOUGE .022 INCH IN FUSELAGE LT SIDE STA 229 BETWEEN LONGERON 18L AND 19L SKIN. BLENDED DAMAGED SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND COCKPIT AND CO-PILOTS AFT SEAT TRACKS WEAR BEYOND LIMITS.  REMOVED AND INSTALLED REPAIR KIT PER TYPICAL REPAIR 53-20-06.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1338 RT LAV AREA FLOORBEAM.  CORROSION TASK NR C58-53300.  REPLACED TOP ANGLE AND INSTALLED DOUBLER REPAIRS, WEB AND FITTING TYPICAL REPAIR 53-10-14 AND SRM 53-05 FIG 72.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1322 RT SIDE LAV AREA FLOORBEAM.  CORROSION TASK NR C58-53300.  CUT OUT DAMAGED AREA, INSTALLED FILLER, REPAIR ANGLES AND DOUBLER.  PE SRM 53-05 TYPICAL REPAIR 53-10-19 EA 29461.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED AFT PAC DOOR LOWER THRESHOLD ATTACHANGLE STA 1338 AT FLOOR PANEL NR 101 ATTACH ANGLE.  REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 34EA 29474.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .25 INCH STA 446 LONGERON 30 BELTFRAME.  INSTALLED REPAIR 'J' ANGLE PLATES PER SRM 53-03 FIG 2A.  (W)


REMARKS:
PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .5 INCH AT STA 1408 AND 1429 LT SIDE LONGERON 2 LT DORSAL FIN SKIN.  CUTOUT DAMAGE SKIN AND INSTALLED SKIN SPLICE REPAIR PER DACO PER SKETCH 3413J AND EA 29421 AND EO 5388X223.  (W)


REMARKS:
AT EWR, ON POST FLIGHT INSPECTION FOUND RIGHT INBOARD FLAP CABLE FOR FOLLOW UP DRUM BROKEN.  REMOVED AND REPLACED RT INBOARD AFT FLAP CABLE PER MM 27-51-05.  OPS CHECK OK.  (W)


REMARKS:
AFTER TAKEOFF, FLT NR 52, PBI TO EWR, UNABLE TO PRESSURIZE AIRCRAFT DUE TO AIR LEAK AT L2 DOOR.  SECOND OFFICERS ANNUNCIATOR SHOWED ALL DOOR CLOSED.  DIVERTED TO ATL.  FOUND L2 DOOR NOT FULLY CLOSED.  CHECKED DOOR STOPS AND HINGES, CHECKEDOK.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN RT FLAP LOWER SPAR CAP STATION XFIS 304.031.  SPLICED IN NEWSECTION OF SPAR CAP PER DAC REPAIR DWB J060179 AND USAIR EA 29245.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK AT CUSP MEMBRANE AT STATION 598 RIGHT.  SPLICED IN SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 96.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .75 INCH CRACK IN CUSP MEMBRANE AT STATION 598 LEFT.  SPLICED IN SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 96.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK NR C58-53300 ON THE RT LAV FLOOR BEAM STATION 990 GROUND LEVEL I CORROSION (PREVIOUSLY REWORKED).  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 20A.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C58-5330 ON FLOOR SUPPORT AT STATION 965 RT LAV PREVIOUSLY REWORKED, LEVEL I.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 53-10-14.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION FOUND DEEP GROOVES IN FLOOR BEAM STATION 465 CAUSED BY FLOORBOARD.  INSTALLED DOUBLERREPAIR PER SRM 53-05 FIG 20/20A.  (Z)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C46-53303 INSIDE OF SERVICE DOOR STATION 200 FOUND LEVEL I CORROSION ON SUBFLOOR.  CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SUBFLOOR PER SRM 53-01 FIG 2.  (Z)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C45-53301 AND C46-53303 FOUND LEVEL I CORROSION ON SUBFLOOR SKIN UNDER THRESHOLD AT STATION 160-200.  AREA WAS PREVIOUSLY 6 INCH BY 14 INCH.  CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SUBFLOOR PER SRM 53-01 FIG 2.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT STATION 200, LONGERON 15L INNER SKIN WEB AT RIVET.  INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND DEEP GROOVES WORN IN FLOOR BEAMS FROM CTR FLOOR BOARD NR 34 TO STA 408, 389 AND 427.  INSTALLED DOUBLER REPAIRS PER SRM 53-05 FIG 20/20A.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND CORROSION AT RT OUTBOARD SEAT TRACK STATION 200.  SPLICED IN NEW SECTION OF SEAT TRAK PER SRM 53-05 FIG 4F.  (W)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C51-53300 AND FOUND LEVEL I CORROSION FWD CARGO REAR FLOOR SUPPORT ANGLE STATION 596, LONGERON 28L-28R.  REMOVED AND REPLACED ANGLE PER DACO DRAWING.  (W)


REMARKS:
PIT - FLT 1297 - ON CLIMB-OUT, THE CAPTAIN PULLED THE GEAR HANDLE BUT IT WOULD NOT GO INTO THE 'UP' POSITION.  CREW DECIDED TO RETURN TO PIT.  MAINTENANCE DRAINED FLUID FROM THE NOSE LANDING GEAR LOWER LEG, REINSTALLED THE LOWER LEG AND SERVICED.  NUMEROUS GEAR SWINGS WERE PERFORMED.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - FLT 0881 - DURING CLIMB, BOTH PACKS FAILED.  THE RIGHT PACK RETURNED FOR 15 SECONDS THEN FAILED AGAIN.  CREW RETURNED CLT.  MAINTENANCE FOUND THE LEFT TEMPERATURE CONTROL VALVE STUCK OPEN CAUSING THERMOL TRIP ON LEFT PACK.  THE LEFT PACK TEMPERATURE CONTROL VALVE WAS REPLACED.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
SYR - FLT 0545 - AFTER TAKEOFF, CREW RECEIVED A NOSE GEAR UNSAFE LIGHT.  THE GEAR WAS CYCLED TWO MORE TIMES AND THE LIGHT REMAINED ON.  THE FLIGHT DIVERETED TO SYR AND LANDED SAFELY.  MAINTENANCE SERVICED THE NOSE STRUT.  A GEAR SWING WAS PERFORMED WITH NO DISCREPANCIES NOTED.  AIRCRAFT OK FOR SERVICE.  (W)


REMARKS:
PIT - FLIGHT 0310 - CREW COULD NOT GET A GREEN LIGHT ON THE NOSE GEAR.  THE GEAR WAS RECYCLED AND THE NOSE GEAR GREEN DOWNLOCK LIGHT CAME ON.  MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH.  (W)


REMARKS:
PIT - FLT NR 1576 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM PIT.  MAINTENANCE FOUND THE NOSE GEAR STRUT FLAT ON ARRIVAL AT THE GATE.  THE STRUT WAS SERVICED WITH NITROGEN AND THE STRUT INFLATED TO THE PROPER HEIGHT.  (W)


REMARKS:
CAE - FLT 0253 - ON LANDING IN CAE, THE GEAR DOOR OPEN LIGHT WOULD NOT GO OUT.  THE GEAR WAS RECYCLED THREE TIMES BUT THE LIGHT REMAINED ON.  MAINTENANCE SECURED A LOOSE ROLLER ON THE RIGHT MAIN LANDING GEAR UPLATCH.  CHECKED OTHER PORTIONS OF THE DOOR INDICATION SYSTEM.  NO DEFECTS WERE NOTED.  GEAR WAS SWUNG SEVERAL TIMES.  ALL INDICATIONS WERE NORMAL.  (W)


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND STRINGER CLIPS CRACKED AT BS 400, S27L, AND 28L, AT BS 747, S10R, AT BS 500D, S3R AND 19R/L, AT BS 406, S3R, AT BS 380, S7L, AT BS 500A, S1, AT BS 727B, S14L, AT BS 663, S10R AND L, AND AT BS 727A, S16R. REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, TOP AND BOTTOM OF UPPER T-CHORD FROM LBL 10 TO RBL49.  REPAIRED PER TRAMCO EWO 95-0172.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, AT BL 0 AND LBL 12, WL 208, AND AT BS 360, LBL 10 AND RBL 1, WL 208, AND AT BS 344, LBL 10 AND RBL 10.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTED AT BS 312, BETWEEN 18 AND 19R, AT BS 320, BETWEEN S20 AND 21R,FROM BS 363 TO 364, S5L, AND AT BS 1128, BETWEEN S14 AND 15R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH AT FORWARD GALLEY DOORWAY LOWER AFT CORNER, BS 328, RBL 65, WL 211.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND LEFT WING L/E DENTED 15 INCHES OUTBOARD OF NUMBER 1 ENGINE, MEASURING 1.5 INCHES BY.5 INCH BY .012 INCH DEEP.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT SERVICE DOOR EXTERNAL SKIN BENT AT UPPER OUTER EDGE LOWER HINGE CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME FLANGE CRACKED AT BS 492, S24R.  REPAIRED PER TRAMCO EWO 95-0194.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, RBL 45 TO LBL 45, AT BS 344, LBL 25 TO BL 0, WL 208.  REPAIRED PER SWA RA 1-353-542 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND L-ANGLE CRACKED AT BS 294, RBL 30, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME DENTED AND GOUGED AT UPPER FASTENER HOLE OF STRINGER CLIP BS 947, S26R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTS AT BS 314, S18R, AT BS 916, S21 TO 22L, AND AT BS 424, BETWEEN S21 AND 22R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED  AT BS 880 TO 890, BETWEEN S25 AND 26L, AT BS 990, BETWEEN S14AND 15L, AT BS 670, BETWEEN S2 AND 3R, AND AT BS 390, BETWEEN S16 AND 17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND DEEP GOUGES IN FUSELAGE SKIN  AT BS 960, BETWEEN  S20 TO 21L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO BAY SHEAR TIE CRUSHED AND SKIN DENTED AT BS 807, RBL 6 TO LBL 6, WL 151.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD SECTION OF CABIN EMERGENCY FLOOR TRACK LIGHTING INOP.  REPLACED BATTERY PACK PER BOEING MM.


REMARKS:
EWR - FLT 29 - AFTER TAKEOFF, ALL FUEL FLOW WENT TO ZERO, RETURNED TO EWR.  FOUND SHORTED NR 5 PIN ON FUEL FLOW POWER SUPPLY AND CHAFED WIRE TO POWER SUPPLY 8 TO 10 INCHES BEHIND S/O PANEL.  REPAIRED CHAFED WIRE AND REMOVED AND REPLACED FUEL FLOW POWER SUPPLY PER MM 73-30.  OPS CHECK OKAY.  (X)


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 470, 471, AND 490, STRINGER 10L.  REPAIRED PER TRAMCO EWO 95-0203.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 727+11, 757, AND 758, STRINGER 4L.  REPAIRED PER TRAMCO EWO 95-0203.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT BS 391, STRINGER 14L.  REPAIRED PER TRAMCO EWO 95-0203 AND 95-0205.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT VERTICAL STIFFENER, BS 178, LBL 6, WL 184.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD SKIN, WL 218, RBL 10-12, AT WL 187 TO 203, AND WL 202 TO 188, RBL 5.7.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT VERTICAL STIFFENER, BS 178,RBL 6, WL 184.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT AFT ENTRY DOOR UPPER AFT CORNER, BS 986.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D CHECK, FOUND BELTFRAME CRACKED AT BS 360, STRINGER 26L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D CHECK, FOUND WEB CRACKED 1 INCH AT I/B RADIUS ABOVE RAM AIR DUCT AT FWD END ATTACH POINT, LEFT AC BAY.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
MCI - DURING OP-17, FOUND FORMER RING BENT BETWEEN STRINGERS 23L AND 24L, FS 520.  REPAIRED PER ARA 9106.  TOTAL CYCLES22,210.


REMARKS:
STL - DURING OP-15, FOUND ONE INCH CRACK IN MAIN FRAME RIGHT SIDE, STATION 680, ABOVE STRINGER 15R.  REPAIRED PER EMLR 65330.  TOTAL CYCLES 78,720.


REMARKS:
MCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN EXTERIOR SKIN AT TOP AFT CORNER OF FORWARD ENTRY DOOR.  CUT OUT CRACKEDAND DAMAGED AREA, REPAIRED PER SRM 5-30-03.  TOTAL CYCLES 33,173.


REMARKS:
MCI - DURING OP-17 FOUND A 6 INCH CRACK AT AFT CARGO STRINGER 29, IN RT VERTICAL LEG INBOARD SIDE, FS 1000 TO FS 1010.REPAIRED PER ARA 8682 AND STANDARD PRACTICES.  TOTAL CYCLES 22,210.


REMARKS:
MCI - DURING CHECK C-1D, FOUND A 1.5 INCH CRACK IN FORWARD FUSELAGE, RUNNING FORWARD TO FASTENER HOLE UPPER HINGE CUTOUT, FORWARD ENTRY DOOR.  REPAIRED BY INSTALLING DOUBLER PER S/B 727-53-0198.  TOTAL CYCLES 25,548.


REMARKS:
STL - DURING DESCENT, SMOKE APPEARED IN CABIN WITH A HOT ODOR.  TURNED OFF AIRFOIL ANTI-ICE AND SMOKE AND ODOR DISSIPATED.  ACCOMPLISHED AIR CONDITIONING DUCT OIL CONTAMINATION CHECKS AND AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL.  CHECK C-2D.


REMARKS:
STL - DURING C-CHECK, FOND A .875 INCH CRACK IN UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD PASSENGER DOOR JAMB.  STOP DRILLED CRACK AND REPAIRED PER S/B 53-137.  TOTAL CYCLES 29,619.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACK IN CASTELLATION, EMANATING UNDER UPPER RIB, OUTBOARD SIDE IWS 555.00, AT STRINGER 18, 19 AND 20, RESPECTIVELY.  REPAIRED PER DRAWING 1647070 AND TWA STANDARD PRACTICES.  TOTAL CYCLES 23,012.


REMARKS:
MCI - DURING CHECK C-6C, FOUND 1.5 INCH CRACK IN FUSELAGE SKIN, WITH AREA BULGED OUTWARD AND WITH RIVET HEAD MISSING, STATION 649, STRINGER 36-37.  REPAIRED PER SRM 53-31-00, FIGURE 815.  TOTAL CYCLES 22,020.


REMARKS:
JFK - DURING SPECIAL CHECK, FOUND TWO CRACKS AT BOTTOM OF STIFFENER, STATION 1301.  REPAIRED PER SRM 53-10-09.  TOTAL CYCLES 17,680.


REMARKS:
JFK - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT.  FOUND NO ELECTRICAL POWER TO LANDING GEAR TRUCK LEVEL SENSORS. REPLACED 2F16 CIRCUIT BREAKER, MFG P/N 2T20-5.  LANDING GEAR SYSTEM CHECKED NORMAL.  CHECK C-9C.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACKS IN UPPER RIB CAP IWS 503, IN CASTELLATION AT FORWARD SIDE OF STRINGERS 13, 24 AND 25, 1.1250 INCH, 1.25 INCH AND ONE INCH, RESPECTIVELY, INTO AND THROUGH RADIUS.  REPAIRED BY INSTALLATION OF NEW SECTION OF RIB CAP PER DRAWING NR 1647070.  TOTAL CYCLES 23,342.


REMARKS:
STL - AFTER TAKEOFF VERY LOUD BANG, AND ELECTRICAL SMOKE ENTERED COCKPIT.  SHUT OFF ELECTRICAL POWER TO GALLEY.  FOUND ELECTRICAL CONNECTOR FOR NR 2 COFFEEMAKER SHORTED. REPLACED NR 2 COFFEEMAKER AND ELECTRICAL HARNESS, MFG P/N WK-236318.OPERATION OF NR 2 COFFEEMAKER CHECKED NORMAL.  CHECK OP-16.


REMARKS:
JFK - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE INTRANSIT LIGHT REMAINED ON AND NOSE LANDING GEAR DOOR LIGHT WOULD ILLUMINATE WHEN LANDING GEAR SELECTOR PLACED IN NEUTRAL.  FOUND NOSE LANDING GEAR UPLOCK SUPPORT BROKEN, MFG P/N 1506362-101.  REPLACED NOSE LANDING GEAR UPLOCK ASSEMBLY, MFG P/N 1606361-105.  NOSE LANDING GEAR OPERATION AND INDICATIONCHECKED NORMAL.  CHECK C-7C.


REMARKS:
STL - DURING CHECK-C, FOUND .25 INCH CRACK IN BELT RING, IN TAIL COMPARTMENT, STA 1212.809, LONGERON 6L, 6R, 5R, 5L, 4R, AND 4L.  REPLACED BELT RING PER SRM 51-10-4 AND SRM 51-30-0.  AIRCRAFT TOTAL TIME:  38,988 HOURS, 35,341 CYCLES.


REMARKS:
PHL - FLT 8610 - FLIGHT EN ROUTE BUT TO ACY WHEN AIRCRAFT LOST 'A' SYSTEM HYDRAULICS.  FLIGHT DIVERTED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENACNE REPLACED BROKEN FITTING AT LEFT MAIN GEAR DOWN LINE RESTRICTOR.  ALSO, REPLACED NR 1 AND NR 2 ENGINE 'A' SYSTEM HYDRAULIC PUMPS, PRECAUTIONARY.  (Z)


REMARKS:
ROC - FLT 1670 - UNABLE TO RAISE GEAR HANDLE ON TAKEOFF.  CREW PERFORMED CHECKLIST, DETERMINED THAT LANDING GEAR LEVER LATCH SOLENOID FAILED.  OVER RIDE LEVER PULLED AND GEAR RETRACTED NORMALLY PER CHECK LIST.  FLIGHT PROCEEDED ON TO PHL AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LOCK SOLENOID.  (Z)


REMARKS:
TYS - 1192 - ON CLIMB, NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED.  FLIGHT RETURNED TO TYS WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND NR 2 ENGINE OIL FILTER CONTAMINATED WITH CARBON.  REPLACED MAIN OIL FILTER.  RANENGINE, CHECKED FOR LEAKS, NO LEAKS NOTED.  OIL FILTER BYPASS LIGHT DID NOT ILLUMINATE AT RUN UP.  (Z)


REMARKS:
MCO - ON CLIMB, LEFT ENGINE OVERHEAT LIGHT ILLUMINATED.  FLIGHT RETURNED TO MCO WHERE AN OVERWEIGHT LANDING WAS MADE.  REPEAT EVENT, ON CLIMB, LEFT ENGINE OVERHEAT LIGHT ILLUMINATED.  FLIGHT RETURNED TO MCO WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND GASKET FAN TSO THERMOSTAT IN PNEUMATIC LINE RUPTURED.  REPLACED GASKET.  ACOMPLISHEDOVERWEIGH LANDING INSPECTION.  FOUND 13TH STAGE ANIT-ICE DUCT LEAKING AT EXPANSION JOINT 12 O'CLOCK POSTION UNDER ENGINE FIXED COWL.  REPLACED RIGID LINE.  (Z)


REMARKS:
PHL - 159 - FORWARD EXTERIOR EMERGENCY EXIT LIGHTS AND AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK FOR FORWARD EMERGENCY EXIT LIGHTS.  REPLACED AFT OVERHEAD EMERGENCY LIGHT POWER SUPPLY.  OPS CHECK NORMAL.  (Z)


REMARKS:
EWR - 44 - DURING APPROACH FOR LANDING LGA, TRAILING EDGE FLAP INDICATION BETWEEN 1 DEGREE AND 2 DEGREE.  FLIGHT DIVERTED TO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT FLAP POSITION.  (Z)


REMARKS:
IND - FLT 1860 - EN ROUTE TO PIT, FLIGHT LOST ELEVATOR FEEL PITOT HEAT.  FLIGHT DIVERTED TO IND, DUE TO ICING SITUATIONAT PIT.  LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPAIRED WIRE IN CONNECTOR AT RIGHT ELEVATOR PITOT PROBE.  HEAT TEST CHECKS GOOD.  (Z)


REMARKS:
JFK - FLT 2689 - ON APPROACH LGA, WHEN FLAPS WERE SET TO 5, FLAPS FROZE IN THE 1 POSITION.  FLIGHT DIVERTED TO JFK WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND INDICATOR SPLIT CAUSING FLAP SYSTEM TO BE LOCKED OUT.  REPLACED INDICATOR.  SYSTEMS OPS NORMAL.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .375 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN (BS 178) BS 178, LBL 5, WL 200.  REPAIRED PER T/R 53-10-07.  (Z)


REMARKS:
INT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND .75 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN BS 178, BS 178RBL 5, WL 200.  REPAIRED PER T/R 53-10-07.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND APPROX .5 INCH BY 4 INCH LONG CHAF WEAR DEEP INTO FUSELAGE SKIN, BETWEEN STRINGER 1 AND 2 LEFT AT STATION 867 TO 887.  REPAIRED PER SRM 53-00-01 AND TR 53-30-01 AND TR 53-30-03 AND EA 38864.(Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 31 INCH BY 2 INCH CORRODED AREA ON BEAM AT BS 986.5.  REPAIRED PER SRM 53-00-51.  CORROSION TASK NR C53-00-51.  CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON AFT CARGO FLOOR STRINGERS, BS 775 AT LBL 2, 7, AND 12 RBL 2, 7, (5 PLACES).  REPAIRED PER TR 53-10-06.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .625 INCH BY 10 INCH TOTAL CORROSION IN SEVERAL PLACES, ON FLOOR BEAM AT BS 847 THROUGH BS 787.7.  REPAIRED PER SRM 53-00-53 FIG 202.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (Z)


REMARKS:
CLT - 1838 - ON CLIMB LOW OIL PRESSURE LIGHT FOR NR 1 ENGINE ILLUMINATED ALONG WITH OIL QUANTITY INDICATING NEAR ZERO.CREW SHUT DOWN NR 1 ENGINE AND FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACEDNR 1 GARLOCK SEAL.  LEAK CHECK GOOD.  (Z)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACKS AT STA 555 UPPER RIB CAP AS FOLLOWS, .75 INCH O/B OF STRINGER 18, 1 INCH IN STRINGER 18 CASTELLATION, .6250 INCH STRINGER 19, 1 INCH I/B SIDE OF STRINGER 19, AND .0625 INCH AT STRINGER 21.  REPAIREDSECTIONS OF CAP PER DRAWING 1647070.  TOTAL CYCLES 21031.


REMARKS:
MCI - DURING OP-17, FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER SKIN FUSELAGE, STA 1333.  REPAIRED PER ARA 9113.  TOTAL CYCLES 22210.


REMARKS:
MCI - DURING OP-17, FOUND CORROSION IN AFT CARGO STRINGER/STRINGER SPLICE 29R AND 29L, FS 990.  REMOVED CORROSION PER SRM 51-10-6 AND REPAIRED PER ARA 8682 AND STANDARD PRACTICES.  TOTAL CYCLES 22210.


REMARKS:
ROC - FLT 1890 - ON TAKEOFF, CREW HEARD A BANG.  THE FIRST OFFICER CALLED FOR CONTINUOUS MAXIMUM POWER.  CREW HEARD SEVERAL MORE COMPRESSOR STALLS.  CAPTAIN NOTICED THAT THE EPR HAD ROLLED BACK TO 1.0 TO 1.2 POWR WAS PULLED BACK AND ALL ENGINE INDICATIONS APPEARED NORMAL.  CAPTAIN DECLARED AND EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
STL - FLT 223 - DURING CLIMB, HAD SMOKE IN CABIN.  SELECTED FULL RATE CABIN PRESSURE AND FULL COLD, AND CABIN CLEARED.FOUND OIL IN 8TH STAGE AIR DUCT OF LT ENGINE, SN 1215.  REPLACED LT ENGINE.  ENGINE TOTAL TIME:  18,588 HOURS; 9,630 CYCLES, CHECK C-1D - 1-30-95 - MCI.  INVESTIGATION INTO SMOKE IN THE CABIN, REVEALED OIL IN THE 8TH STAGE DUCT OF ENGINE 1215 CAME FROM THE NR 3 BEARING, MFG PN 795075, RETAINING NUT BEING LESS TIGHT THAN NORMAL.  ENGINE SN 1215 WAS REPAIRED AND RETURNED TO SERVICE.  (X)


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


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STRINGER 3R.  REPAIRED PER SWA RA 1-253-1260.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BS 178, LBL 5.7, FORWARD CHORD CRACKED.  REPAIRED PER SWA RA 1-253-1255.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BS 308, LBL 20, FLOOR BEAM CORRODED.  REPAIRED PER SWA RA 1-253-1257.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BS 360, BL 0, FLOOR BEAM CORRODED.  REPAIRED PER SWA RA 1-253-1258.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BS 328, RBL 22 TO RBL 48, FORWARD FLANGE, FLOOR BEAM CORRODED.  REPAIRED PER SWA RA1-253-1256.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BS 312, FLOOR BEAM UPPER SPLICE CORRODED.  REPAIRED PER SWA RA 1-253-420.


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 10 INCH TOTAL OF CORRODED AREA ON INTERCOSTAL AT BS 986.5 THROUGH BS 1016.  REPAIRED PER SRM 53-60-51 AND SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 200 INCH CORRODED AREA STATION 727 TO 767 AND 847 TO 947 RIGHT ANGLE IN AFT CARGO.  REPAIRED PER SRM 51-10-02 AND 51-40-02.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 36 INCH CORRODED AREA, STATION 947 BULKHEAD LOWER ATTACH ANGLE S-26 R TO S-26L.  REPAIRED PER BOEING DRAWING NR PL 65-49616 REV LTR AND SHT 13 OF 73 ID NR 12.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (Z)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH BY .028 INCH SPOT OF CORROSION BS 1006 RBL 10.  REPAIRED PER EA 38836.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (Z)


REMARKS:
PIT - DURING Q-1 CHECK, INSPECTION FOUND .3750 INCH CRACK AT STA 198 BETWEEN LONGERON 20L AND 21L IN SKIN.  INSTALLED DOUBLER TYPE REPAIR PER SRM 53-05 FIG 57A.  (W)


REMARKS:
PIT - DURING Q-1 CHECK, INSPECTION FOUND SMALL SECTION OF SKIN TORN AT STA 37 LT RADOME HINGE CUTOUT.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 77.  (W)


REMARKS:
PIT - DURING Q-1 CHECK, INSPECTION FOUND .25 INCH CRACK AT RT FWD EMERGENCY EXIT DOOR AT UPPER AFT CORNER STOP 14 PAN AREA.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03.  (W)


REMARKS:
PIT - DURING Q-1 CHECK, INSPECTION FOUND .5 INCH CRACK IN STA 980 FRAME AT LONG 17L.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-03 FIG 32.  (W)


REMARKS:
PIT - DURING Q-1 CHECK, INSPECTION FOUND 3 SMALL CRACKS BETWEEN .0625 INCH AND .25 INCH LONG AT RIVET HEAD BELOW LONGERON 15L AND JUST FWD OF STA 996.  INSTALLED DOUBLER REPAIR INTERNALLY PER SRM 53-04 FIG 49.  (W)


REMARKS:
CLT - FLT 441 - AT CRUISE, HAD LT ENGINE OVERTHRUST.  CREW SHUTDOWN LT ENGINE.  SINGLE ENGINE TIME APPROXIMATELY 20 MINUTES.  MAINTENANCE REPLACED THE LT ENGINE DUE TO OVERTEMP CONDITION.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
CLT - THE EMERGENCY LIGHT AT THE PASSENGER ENTRY DOOR IS INOPERATIVE.  MAINTENANCE REPLACED THE LIGHT ASSEMBLY.  (W)


REMARKS:
LIT - FLT 374 - ON ROTATION, THE 'CARGO DOORS' LIGHT ILLUMINATED.  CREW RETURNED TO LIT WITHOUT INCIDENT.  MAINTENANCE INSPECTED ALL DOOR LATCHES, HOOKS AND PRESSURIZED ACFT TO 3 PSI.  NO PROBLEMS FOUND.  (W)


REMARKS:
CLT - FLT 1250 - THE NR 1 HYDRAULIC SYSTEM QUANITY AND PRESSURE WENT TO ZERO IMMEDIATELY AFTER FLAP RETRACTION AFTER TAKEOFF.  CREW RETURNED TO CLT.  MAINTENANCE REPLACED THE SUPPLY LINE ON THE LANDING GEAR SELECTOR VALVE.  LEAK CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 1197 - THE RT MLG GAVE AN USAFE INDICATION UPON LOWERING.  CREW RECYCLED THE GEAR AND RECEIVED THREE GREEN LIGHTS.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED A MISSING BOLT IN THE RT FWD MAIN GEAR DOOR ACTUATOR.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
BDL - FLT 972 - THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER THE GEAR HANDLE WAS SELECTED UP AN UNLATCH CHECK PERFORMED.  THERE WAS CONTINUOUS NOISE WITH THE GEAR HANDLE UP AND THE UNSAFE LIGHT ON.  MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT.  OPERATIOINS CHECKED GOOD.  (W)


REMARKS:
CAE - FLT 849 - AFTER TAKEOFF, CREW SMELLED TOXIC FUMES THROUGHOUT THE COCKPIT AND CABIN.  FLIGHT RETURNED TO CAE WITHOUT INCIDENT.  MAINTENANCE INSPECTED THE INTAKES, FLUID QUANTITIES, CARGO BINS AND E AND E COMPARTMENT.  WATER SEPARATORSWERE DRAINED FOR CONTAMINATION.  ALL CHECKED GOOD.  (W)


REMARKS:
STL - AFTER TAKEOFF VERY LOUD BANG, AND ELECTRICAL SMOKE ENTERED COCKPIT.  SHUT-OFF ELECTRICAL POWER TO GALLEY.  FOUND ELECTRICAL CONNECTOR FOR NR 2 COFFEEMAKER SHORTED.  REPLACED NR 2 COFFEEMAKER AND ELECTRICAL HARNESS (P/N WK6-236318).  OPERATION OF NR 2 COFFEMAKER CHECKED NORMAL.  CHECK OP-16 1-12-94 - STL.


REMARKS:
JFK - DURING C-CHECK, FOUND A FUSELAGE SKIN CRACK AT STA 668, STRINGER 36L.  REPAIRED PER SRM 53-31-00 PG 828 FIG 815.TOTAL CYCLES 22734.


REMARKS:
MCI - DURING OP-17, FOUND STA 555 UPPER RIB CRACKED O/B SIDE OF STRINGER 18 AND FOUND A .5 INCH CRACK AT STRINGER 19.  INSTALLED NEW SECTION OF UPPER CAP FROM STRING 19 FWD PER DWG NR 1647070.  TOTAL CYCLES 22210.


REMARKS:
MCI - DURING OP-17, FOUND A ONE INCH CRACK IN UPPER RIB CAP I/B SIDE AT STRINGERS 21 AND 24, STA 503.76.  REPAIRED UPPER RIB CAP PER DWG. NR 1647070 AND INSTALLED NEW SPLICE PER VIEW K.  TOTAL CYCLES 22210.


REMARKS:
MCI - DURING OP-17, FOUND .75 INCH CRACK AT STRINGER 19, RT WING STA 529.40 UPPER RIB CAP O/B SIDE.  CUTOUT DAMAGED RIBCAP AND SPLICED PER DWG NR 1647070, VIEW V.  TOTAL CYCLES 22210.


REMARKS:
STL - DURING CLIMB, NR 3 ENGINE FIREWARNING SOUNDED.  REDUCED POWER ON THE NR 3 ENGINE AND FIREWARNING CEASED.  FOUND 13TH STAGE DUCT AND PERFORMED A HIGH POWER LEAK CHECK.  CHECKED NORMAL.  CHECK C-1 11-21-94 - MCI.


REMARKS:
JFK - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE INTRANSIT LIGHT REMAINED ON AND NOSE GEAR DOOR LIGHT WOULD ILLUMINATE WHEN LANDING GEAR SELECTOR PLACED IN NEUTRAL.  FOUND NOSE LANDING GEAR UPLOCK SUPPORT BROKEN, (P/N 1506362-101). REPLACED NOSE LANDING GEAR UPLOCK ASSEMBLY, (P/N1606361-105).  NOSE LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL.  CHECK C-7C - 11-21-94 - JFK.


REMARKS:
STL - FLT 658 -  DURING CLIMB, THE NR 1 ENGINE (S/N 2107) WAS SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION AND A DECREASE IN OIL QUANTITY.  FOUND NOSE COWL ANTI-ICE DUCT, (P/N 7958591-501), RUPTURED, BLOWING HOT AIR ON BYPASS LIGHTSWITCH, MELTING SOLDER JOINTS OF SWITCH BODY.  REPLACED ANTI-ICE DUCT, REPLACED BYPASS SWITCH, (P/N 42D109-1A) AND REPLENISHED OIL QUANTITY.  ENGINE OPERATION AND LEAK CHECKS NORMAL.  CHECK C-1 - 1-12-94 - STL.


REMARKS:
LAX - FLT - 210 - ON TAKEOFF, WHEN LANDING GEAR WAS RETRACTED, LT MLG RED LIGHT AND DOOR LIGHT REMAINED ILLUMINATED.  FOLLOWED FLIGHT HANDBOOK PROCEDURES AND LIGHTS REMAINED ILLUMINATED.  FOUND DEFLECTOR ASSEMBLY (P/N 5937042-501) BENT ANDCONTACTING HYDRAULIC RESERVOIR.  REPLACED DEFLECTOR ASSEMBLY AND LANDING GEAR OPERATION CHECKED NORMAL.  CHECK C-1D - 1-13-94 - MCI.


REMARKS:
LAX - FLT 721 - ON DESCENT WHEN LANDING GEAR WAS EXTENDED, RT MLG GREEN LIGHT DID NOT ILLUMINATE.  CYCLED LANDING GEAR AND ALTERNATE LANDING GEAR EXTENSION.  FOUND A-5 CARD, MFG PN 8-351-07, IN ELECTRONIC PROXIMITY SWITCH BOX.  LANDING GEAR POSITION AND WARNING SYSTEM CHECKED AND B.I.T.E. CHECKED NORMAL.  CHECK C-4A - 1-19-95 - JFK.


REMARKS:
MCI - FLT 119 - DURING CLIMB, RT ENGINE LOST POWER.  SHUT DOWN ENGINE.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE SN 3257.  ENGINE TOTAL TIME:  19,850 HOURS, 10,375 CYCLES.  CHECK C-2D - 1 13-94 - MCI.


REMARKS:
STL - FLT 223 - DURING CLIMB, HAD SMOKE IN CABIN.  SELECTED FULL RATE CABIN PRESSURE AND FULL COLD, AND CABIN CLEARED.FOUND OIL IN 8TH STAGE AIR DUCT OF LEFT ENGINE SN 1215.  REPLACED LEFT ENGINE.  ENGINE TOTAL TIME:  18,588 HOURS; 9,630CYCLES.  CHECK C-1D - 1-30-95 - MCI.


REMARKS:
IN FLIGHT, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED.  CYCLING GEAR, NO HELP.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFULL LANDING.  TROUBLESHOT AND FOUND M983 PC CARD FAULT.  REPLACED AND OPERATIONAL CHECKED PER BOEING M/M.


REMARKS:
STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED.  THEFLIGHT MADE AN UNSCHEDULED LANDING.  REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1),  AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1).  OPS CHECKS NORMAL.  CHECK C-1 - 10-18-94 - MCI.  REF 95ZZZW266, 95ZZZW267, 95ZZZW268.


REMARKS:
STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED.  THEFLIGHT MADE AN UNSCHEDULED LANDING.  REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1),  AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1).  OPS CHECKS NORMAL.  CHECK C-1 - 10-18-94 - MCI.  REF 95ZZZW265, 95ZZZW267, 95ZZZW268.


REMARKS:
STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED.  THEFLIGHT MADE AN UNSCHEDULED LANDING.  REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1),  AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1).  OPS CHECKS NORMAL.  CHECK C-1 - 10-18-94 - MCI.  REF 95ZZZW265, 95ZZZW266, 95ZZZW268.


REMARKS:
STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED.  THEFLIGHT MADE AN UNSCHEDULED LANDING.  REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1),  AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1).  OPS CHECKS NORMAL.  CHECK C-1 - 10-18-94 - MCI.  REF 95ZZZW265, 95ZZZW266, 95ZZZW267.


REMARKS:
MCI - FLT 119 - DURING CLIMB, RIGHT ENGINE LOST POWER.  SHUT DOWN ENGINE.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACEDENGINE SN 3257.  ENGINE TOTAL TIME: 19,850 HOURS; 10,375 CYCLES.  CHECK C-2D - 1-13-94 - MCI.


REMARKS:
MCI - FLT 119 - DURING CLIMB, RT ENGINE LOST POWER.  SHUT DOWN ENGINE.  FOUND METAL PARTICLES IN TAIL PIPE.  REPLACED ENGINE, SN 3257.  ENGINE TOTAL TIME:  19,850 HOURS; 10,375 CYCLES.  CHECK C-2D - 1-13-94 - MRI.  INVESTIGATION INTO ENGINE, SN 3257, LOSS OF POWER DURING CLIMB, REVEALED LOW PRESSURE TURBINE 2 VANE, MFG. PN 800892, SHIFTED AFT CONTACTING LOWPRESSURE TURBINE 2 BLADE, CAUSING BLADE FRACTURE.  ENGINE, SN 3257, WAS REPAIRED AND RETURNED TO SERVICE.  (X)


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


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


REMARKS:
DURING OVERNIGHT CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP.  REPLACED TWO FLOOR TRACK BATTERY PACKS PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LEFT AFT ENTRY DOOR EMERGENCY LIGHTING INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CABIN FORWARD SECTION OF FLOOR TRACK LIGHTING INOP.  REPLACED BATTERY CHARGER HOUSING PER BOEING M/M.


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


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 767, 11 INCHES ABOVE SKIN LAP.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
CLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING.  FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE CHANGE OVER SWITCH AND CARGO DOOR SEALS AND ADJUSTED THELEFT ENGINE CHANGE OVER SWITCH.  OPERATIONS CHECKED NORMAL.  REFERENCE NR USAA950218.


REMARKS:
PHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330.  CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED TO RIGHT PRSOV AND THE RIGHT PACK FLOW VALVE.  OPERATIONS CHECKED GOOD. REFERENCE USAA950201.


REMARKS:
SFO - THE EMERGENCY EXIT LIGHT AT DOOR 3R ILLUMINATED WITH THE EMERGENCY LIGHTS IN THE ARMED POSITION.  MAINTENANCE REPLACED THE R3 EMERGENCY EXIT SIGN ASSEMBLY.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
CLT - FLT 435 - ON CLIMB-OUT THROUGH 8000 FEET, FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE RELEASED ON MEL 52-3.  REPLACED OVERHEAD ANNUNCIATOR MODULE PRECAUTIONARY, FOUND FWD CARGO DOOR STOP PINS BACKED OUT AROUND PROX SWITCH.  ADJUSTED ALL FWD CARGO DOOR STOPS AS PER B737 MM, CLEARED MEL.  (Z)


REMARKS:
PHL - THE CROSS AISLE FLOOR LEVEL EMERGENCY LIGHTS FAILED TO TEST.  MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER.OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
PHL - FLT 0676 - THE CAPTAIN LOWERED THE LANDING GEAR AND RECEIVED ONE GREEN LIGHT ON THE LEFT MAIN GEAR ONLY.  AFTER RECYCLING THE GEAR, THE LIGHT STILL REMAINED.  THE CAPTAIN DID A FLYBY AND THE TOWER STATED THAT THE GEAR APPEARED TO BE DOWN.  THE CAPTIAN RESET THE LIGHT SOCKETS ON THE INDICATORS AND ALL THREE GREEN LIGHTS APPEARED.  THE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE CHECKED THE SECURITY OF THE INDICATOR SOCKETS AND PERFORMED A BITE CHECK OF THE PROXIMITY BOX.  ALL CHECKED NORMAL.  (Z)


REMARKS:
PHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330.  CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED TO RIGHT PRSOV AND THE RIGHT PACK FLOW VALVE.  OPERATIONS CHECKED GOOD. REFERENCE 95ZZZZ155.


REMARKS:
PIT - FLT 1842 - UPON TURNING WING ANTI-ICE ON, CREW RECEIVED A WING ANTI-ICE FAULT.  FLIGHT RETURNED TO PIT WITHOUT INCIDENT.  MAINTENANCE SEATED PIN HH IN CONNECTOR AND CHECKED LOCKING.  ALL CHECKED GOOD.  (Z)


REMARKS:
PIT - THE EMERGENCY CENTER CABIN OVERWING STANDBY LIGHT WAS INOPERATIVE.  MAINTENANCE REPAIRED A LOOSE CONNECTION ON WIRING TO THE LIGHT.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
TPA - FLT 8003 - THE GEAR WOULD NOT RETRACT AFTER TAKEOFF.  CREW TRIED TO RECYCLE GEAR.  GEAR REMAINED EXTENDED AND CREW RETURNED TO TPA.  MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOOR VALVE.  (Z)


REMARKS:
GSO - EMERGENCY LIGHT OVER DOOR 2L INOPERATIVE.  MAINTENANCE REPLACED LIGHT ASSEMBLY.  (Z)


REMARKS:
PIT - FLT 852 - FLIGHT EN ROUTE PHL TO MCI WHEN CIRCUIT BREAKER FOR NR 1 FORWARD BOOST PUMP, NR 2 AFT BOOST PUMP, AND CENTER BOOST PUMP POPPED.  RESET UNSUCCESSFUL.  FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CIRCUIT BREAKER C65 AND OVERHEAD FUEL SYSTEM MODULE.  OPERATION OF ALL BOOST PUMPS NORMAL.  (Z)


REMARKS:
IAH - FLT 1439 - FLIGHT EN ROUTE SAT TO PIT WHEN NR 2 ENGINE OIL TEMPERATURE EXCEEDED RED LINE.  CREW SHUT DOWN ENGINE AND DIVERTED TO IAH WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE OIL TEMPERATURE BULB.(Z)


REMARKS:
CLT - FLT NR 0330 - ON TAKEOFF, THE LEFT AND RIGHT WINGS WERE OBSERVED TO HAVE FUEL VENTING FROM THEM.  FLIGHT RETURNEDTO CLT WITHOUT INCIDENT.  MAINTENANCE ACCOMPLISHED AN OPERATIONAL TEST OF THE FUEL AUTO FEED SYSTEM.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
CLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING.  FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE CHANGE OVER SWITCH AND CARGO DOOR SEALS AND ADJUSTED THELEFT ENGINE CHANGE OVER SWITCH.  OPERATIONS CHECKED NORMAL.  REFERENCE NR 95ZZZZ154.


REMARKS:
BUF - FLT 0873 - AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN THE GEAR WAS RETRACTED.  THE GEAR WAS RECYCLED TWICE WITH THE SAME RESULTS.  CREW RETURNED TO BUF WITHOUT INCIDENT.  MAINTENANCE INSPECTED THE GEAR AND FOUND HEAVY ICE.  THE GEAR WAS DE-ICED.  BITE CHECK OF THE PROX BOX WAS ACCOMPLISHED.  ALL CHECKED GOOD.  (Z)


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZING STRAP CRACKED AT E/E COMPARTMENT, BS 312, BOTTOM OF FLOOR BEAM BL 0.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE BULKHEAD WEB CRACKS AT BS 178, WL 184 TO 207, RBL 5.7.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE BULKHEAD WEB CRACKS AT BS 178, WL 209, AND 218, RBL 11.7 TO 13.7.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND LIGHTNING STRIKE DAMAGE AT BS 361, BETWEEN S2R AND 3R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND SKIN CRACK AT BS 987, AT STRINGER 4L.  REPAIRED PER TRAMCO EWO 95-0241 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 7, WL 203.  REPAIREDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 5.7, WL 201.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 5.7, WL 184 TO 207.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 7.7 TO 14.7, WL 218.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 10.5 TO 12.7, WL 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT POWER SUPPLY PER BOEING M/M.


REMARKS:
CLT - FLT 0791 - JUST AFTER TAKEOFF CREW RECEIVED A RIGHT GEAR UNSAFE LIGHT FOR THE SECOND TIME REQUIRING FLIGHT TO RETURN TO CLT.  MAINTENANCE CLEANED THE RIGHT GEAR UPLOCK SENSOR.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
LGA - EMERGENCY EXIT LIGHTING AT SEATS REMAIN ON WHENEVER SWITCH IS PLACED IN ARM POSITION.  MAINTENANCE FOUND CHARGE/ON WIRE BROKEN.  SPLICED IN NEW WIRE.  OPS CHECKS OK.  (Z)


REMARKS:
HTS - FLT 1028 - ON TOUCHDOWN, AIRCRAFT VEERED TO THE LEFT AND BOTH LEFT MAIN TIRES CAME OFF.  AN EMEGENCY EVACUATION WAS NOT NECESSARY.  NO INJURIES WERE REPORTED.  MAINTENANCE REPLACED THE LEFT UPPER TORQUE LINE.  (Z)


REMARKS:
PIT - DURING SCHEDULED STRUCTURES VISIT FOUND MULTIPLE SMALL CRACKS TOTALING 3 INCHES IN THE NOSE GEAR BAY TOP COVER STATION 2422 TO 2650.  REF SIP 53-10-10 (EDDY CURRENT).  STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-02-18.  (Z)


REMARKS:
PIT - DURING SCHEDULED STRUCTURES VISIT (SIP), FOUND 2 INCH CRACK IN AFT PRESSURE BULKHEAD HORIZONTAL BEAM III LOWER RADIUS AT CENTER OF BEAM.  EDDY CURRENT REF SIP 53-10-03.  STOP DRILLED CRACK ENDS AND INSTALLED REPAIR PATCH, REPAIR ANGLES (2EACH) AND REAR FACE STRIP PER USAIR EA 29615.  (Z)


REMARKS:
PIT - DURING SCHEDULED STRUCTURES VISIT (SIP), FOUND A 5 INCH CRACK IN THE FWD PRESSURE BULKHEAD LOWER CONNECTION ANGLEAT FRAME 1550 BETWEEN STA 72 AND 73.  (REF SIP 53-10-06).  STOP DRILLED CRACKS AND INSTALLED DOUBLERS PER SRM 53-11-00 AND USAIR EA 29585.  (Z)


REMARKS:
PIT - DURING RESCHEDULED STRUCTURES VISIT (SIP), FOUND A .375 INCH CRACK IN THE SE DOOR OPERATURE IN THE UPPER FWD CORNER.  (REF SIP 53-10-20) EDDY CURRENT INSPECTION.  CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-02-16AND USAIR EA NR 29601.  (Z)


REMARKS:
PIT - DURING FC-5 CHECK INSPECTION ACCOMPLISHED SIP 55-30-01 AND FOUND 2 .5 INCH CRACKS IN RT SIDE CONNECTION ANGLE AT VERTICAL STABILIZER TO FUSELAGE AT 50 PERCENT SPAR.  CUT OUT CRACK SECTION OF ANGLE AND ACCOMPLISHED SPLICE REPAIR PER SRM 55-31-00.  (Z)


REMARKS:
PIT - DURING FC-5 CHECK INSPECTION ACCOMPLISHED SIP 53-10-09 AND FOUND ONE .5 INCH CRACK RT AISLE OF MAIN FRAME CLIP 3450 40 INCHES ABOVE FLOOR LEVEL.  REMOVED AND REPLACED CLIP PER SRM 53-02-12 FIG 6 AND USAIR EO 5391L681.  (Z)


REMARKS:
PIT - FLT 0680 - THE EMERGENCY STRIP LIGHTS AT ROWS 1, 2 AND 3 WAS INTERMITTENT.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
LAX - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, UNSAFE LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR AND INDICATION WAS NORMAL.  FOUND LANDING GEAR MODULE, MFG P/N 257T1103-15, EXTEND/RETRACT LEVER STICKING.  CLEANED AND LUBRICATED LANDING GEAR MODULE EXTEND/RETRACT LEVER.  LANDING GEAR OPERATION AND INDICATION SYSTEM CHECKED NORMAL.  CHECK C-4A.


REMARKS:
STL - AFTER TAKEOFF LEFT MAIN LANDING GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS REMAINED ILLUMINATED WITH GEAR HANDLE IN THE UP POSITION.  FOUND LEFT MAIN LANDING GEAR BUNGEE CYLINDER, MFG P/N 3914016-5503 CRACKED.  REPLACED LEFT MAIN LANDING GEAR BUNGEE CYLINDER.  LANDING GEAR OPERATION AND LIGHT SYSTEMS CHECKED NORMAL.


REMARKS:
BOS - AFTER TAKEOFF NOSE LANDING GEAR DID NOT RETRACT.  CYCLED LANDING GEAR, AND NOSE LANDING GEAR RETRACTED.  INSPECTED NOSE LANDING GEAR AND LUBRICATED.  JACKED NOSE LANDING GEAR AND OPERATED NOSE LANDING GEAR SEVERAL TIMES AND ALL OPERATIONS WERE NORMAL.


REMARKS:
CLT - FLT 0845 - THE FLOOR TRACK LIGHTING MALFUNCTION AT DEPARTURE TIME.  (W)


REMARKS:
ATL/TPA - FLT 101 - RETURNED TO ATL DUE TO UPON RAISING LANDING GEAR, NOSE GEAR UNSAFE LIGHT REMAINED ON.  RIGHT GEAR UNSAFE LIGHT REMAINED ON ALSO.  REMOVED AND REPLACED PROXIMITY SWITCH BOX, PN 008-0004-004, SN OFF 254, SN ON 263.  OPERATION SELF-TEST IAW VALUEJET MM 32-00.  AIRCRAFT WAS TEST FLOWN, OPS CHECK OKAY.


REMARKS:
AIRCRAFT WAS PORTED ON THE RAMP, CUSTOMERS WERE LOADING ONTO THE AIRCRAFT WHEN THE RIGHT TRAILING EDGE OF THE FLAP WAS STRUCK BY A BAGGAGE CART.  APPROXIMATELY 20 INCHES OF THE TRAILING EDGE WAS BROKEN OFF.


REMARKS:
IAD/PBI - FLIGHT 477 - RUNWAY CONDITIONS, STANDING SLUSH.  DURING TAKEOFF, NR 2 ENGINE EXPERIENCED A LOUD BANG ACCOMPANIED BY DECAYING OF THE NR 2 ENGINE INSTRUMENTS.  INITIATED A REJECTED TAKEOFF AT 110 KNOTS.  ACCOMPLISHED A VISUAL INSPECTION OF NR 2 ENGINE INLET AND EXHAUST, THEN PERFORMED A POWER ASSURANCE RUN TO TAKEOFF POWER.  ALSO, PERFORMED REJECTEDTAKEOFF WORK CARDS NR 0027.  OPS CHECKED GOOD PER MM 71-00, PAGE 537.


REMARKS:
ATL - FLT 134 - DURING APPROACH, LEFT GEAR UNSAFE LIGHT INITIATED A GO-AROUND.  LANDED IN ATL, NO TROUBLE REPORTED.  REMOVED AND REPLACED THE LEFT GEAR DOWNLOCK SWITCH AND CONNECTOR.


REMARKS:
ATL/IAD - FLT 368 - AIRCRAFT RETURNED TO ATL DUE TO RIGHT FUEL HEAT STAYED ON CAUSING OIL TEMP TO EXCEED 120 DEGREES CENTIGRADE.  REMOVED AND REPLACED NR 2 ANTI-ICE VALVE.


REMARKS:
IAD/ATL - FLT 173 - EXPERIENCED NR 2 ENGINE CSD OVERTEMP AND FOUND THE CSD WOULD NOT DISCONNECT.  CREW WAS INFORMED TO SHUT DOWN NR 2 ENGINE AND AIR TURNED BACK TO IAD.  CREW DECLARED AN EMERGENCY AND LANDED WITH NO OTHER PROBLEMS.


REMARKS:
DTW/ATL - FLT 441 - RETURNED TO DTW DUE TO A VIBRATION FROM NOSE GEAR WHEELWELL AREA AFTER GEAR RETRACTION.  FOUND NOSEGEAR DOORS OPEN.  CLOSED DOORS AND INSPECTED NOSE GEAR AREA PER MM 32.


REMARKS:
ATL/PBI - FLT 501 - RETURNED TO ATL BECAUSE ON CLIMB-OUT CAPTAIN REPORTED SMOKE IN THE COCKPIT COMING FROM THE GALLEY AREA BEHIND THE FIRST OFFICER'S SEAT, AND DECLARED AN IN-FLIGHT EMERGENCY.  ON FINAL APPROACH, CAPTAIN PULLED FORWARD GALLEY CIRCUIT BREAKER AND SMOKE STOPPED.  AN OVERWEIGHT LANDING WAS MADE AT 101,000 POUNDS.  PERFORMED OVERWEIGHT LANDING INSPECTION.  REMOVED COFFEEMAKER AND PLACED ON MEL.


REMARKS:
STL - FLT 246 - RT MAIN GEAR UNSAFE WARNING LIGHT REMAINED ON WHEN LANDING GEAR WAS EXTENDED.  CYCLED LANDING GEAR WITHSAME RESULTS.  FOUND BROKEN WIRE APPROXIMATELY TWELVE INCHES FROM THE DOWNLOCK PROXIMITY SENSOR.  SPLICED BROKEN WIRE.OP CHECKS NORMAL.  CHECK C-2 - 3-22-94 - MCI.


REMARKS:
JFK - FLT 885 - DURING CRUISE, SINGLE SERVICE CART POSITION D5A, OVERHEATED AND EMITTED SMOKE.  CIRCUIT BREAKER TRIPPED.  DISCONNECTED SERVING CART.  REPLACED SINGLE SERVICE CART, SN 1374.  SINGLE SERVICE CART POSITION OPERTION CHECKED NORMAL.  CHECK C-2 - 4-3-94 - MCI.


REMARKS:
PHL - EMERGENCY EXIT LIGHTS ILLUMINATE ABOUT EVERY 45 MINUTES, THEN SLOWLY FADE BACK TO OFF.  MAINTENANCE FOUND FLOOR LIGHTS ON CONSTANTLY IN ARM.  DISCONNECTED PLUG D4049F TO CHECK POWER.  POWER CHECKED GOOD.  WHEN RECONNECTED, PROBLEM DID NOT OCCUR.  OPS CHECK NORMAL. (X)


REMARKS:
CLT - EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE RPELACED FUSE ON M1479 EMERGENCY LIGHT BATTERY PACK AND RESAFTIED AFT FLIGHT ATTENDANT EMERGENCY EXIT LIGHT SWITCH.  (X)


REMARKS:
LGA - EMERGENCY EXIT LIGHTS FLASHING ROWS 8 THROUGH 15.  MAINTENANCE REPLACED BATTERY PACK AT POWER SUPPLY ON SEAT 11A. (X)


REMARKS:
CLT - FLT 1112 - FLIGHT RETURNED TO GATE WITH A COMPASS PROBLEM WHICH MAINTENANCE FIXED.  FLIGHT PROCEEDED AGAIN AND AFTER TAKEOFF, THE NR 1 UNIT FAILED AGAIN.  CREW DECIDED TO RETURN TO CLT.  MAINTENANCE REPLACED THE NR 1 IRU.  OPERATIONSCHECKED GOOD.  (X)


REMARKS:
CLT - FLT 0366 - AFTER TAKEOFF, THE GEAR WOULD NOT RETRACT.  CAPTAIN WENT THROUGH PROPER PROCEDURES AND RECEIVED THREE GREEN DOWNLOCK LIGHTS.  CREW DECIDED TO RETURN TO CLT.  MAINTENANCE RECHARGED THE HYDRAULIC RESERVOIR PRESSURE.  HYDRAULIC SYSTEM AND LANDING GEAR OPERATIONS CHECKED GOOD.  (X)


REMARKS:
PIT - DURING SCHEDULED STRUCTURES VISIT, FOUND 7.5 INCH CRACK IN AFT SIDE OF FORWARD PRESSURE BULKHEAD BETWEEN STA 72 AND STA 73.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PLATE PER SRM 53-11-00, PAGE 2.  (X)


REMARKS:
PIT - FLT 0141 - THE R1 FUEL BOOST PUMP FAULT LIGHT ILLUMINATED IN-FLIGHT.  FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT.  MAINTEANCE REPLACED THE R1 AND R2 BOOST PUMPS AND COCKPIT OVERHEAD PANEL.  OPERATIONS CHECKED GOOD.  (X)


REMARKS:
PIT - FLT 0590 - UPON GEAR RETRACTION, CREW HEARD A LOUD BANG FROM THE NOSE GEAR.  THE RED UNSAFE LIGHT ILLUMINATED.  THE GEAR WAS PUT DOWN, BUT THE LIGHT REMAINED.  FLIGHT RETURNED TO PIT WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LEFT NOSE GEAR FORWARD LINK DUE TO DAMAGE.  THE EXTENSION/RETRACTION AND FREE FALL ALL GOOD.  (X)


REMARKS:
CLT - FLT 8027 - AFTER TAKEOFF, THE STALL INDICATION FAIL AND WINDSHEAR WARNING LIGHTS ILLUMINATED.  FLIGHT RETURNED TOCLT WITHOUT INCIDENT.  MAINTENANCE REPLACED RIGHT FLAP TRANSMITTER.  OPERATIONS CHECKED GOOD.  (X)


REMARKS:
DTW - FLT 1698 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF.  CREW RETURNED TO DTW WITHOUT INCIDENT.  MAINTENANCE FOUND LANDING GEAR CONTROL CABLE IN THE RIGHT WHEELWELL FROZEN.  THE OBSTRUCTION WAS CLEANED.  AIRCRAFT OKAY FOR SERVICE.  (X)


REMARKS:
STL - FLT 447 - AFTER TAKEOFF, RT MLG RED LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION.  CYCLED LANDING GEAR.  REPLACED LANDING GEAR POSITION AND WARNING ACCESSORY UNIT MFG PN 65-60211-95.  LANDING GEAR POSITION AND WARNING LIGHT SYSTEM CHECKED NORMAL.


REMARKS:
PHL/ATL - FLT 225 - EXPERIENCED A LOSS OF HYDRAULIC PUMP PRESSURE ON THE RIGHT ENGINE.  CREW TURNED ON THE AUXILIARY HYDRAULIC PUMP AND HAD SUFFICIENT PUMP PRESSURE AND NO LOSS OF HYDRAULIC FLUID.  PLACED RIGHT HYDRAULIC PUMP ON MEL 29-5.


REMARKS:
ATL/DFW - FLT 231 - RETURNED TO ATL DUE TO RT AND LT AIR CONDITIONING PACKS AIRFLOW WENT TO ZERO.  RESET CIRCUIT BREAKER FOR GROUND COOLING FAN FOR RT AIR CONDITION PACK.  ON LT AIR CONDITION PACK, FOUND DUCT TEMP INDICATOR STUCK AND PACK THERMAL TRIPPED.  PACK COOLED AND RE-STARTED INBOUND TO ATL.  GROUND CHECK OKAY.


REMARKS:
BOS - THE EMERGENCY LIGHTS POP CIRCUIT BREAKER.  MAINTENANCE REPLACED THE LIGHT SWITCH IN THE COCKPIT OVERHEAD PANEL.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT 0757 - FLIGHT DIVERTED TO PIT DUE TO A PRESSURIZATION PROBLEM.  MAINTENANCE REPLACED THE OUTFLOW DOOR AFT MOTOR AND GEAR BOX.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
LAS - FLT 414 - EN ROUTE LAX TO MCI, CABIN PRESSURE BEGAN CLIMBING.  DROPPED TO FL 290 AND CREW WAS ABLE TO CONTROL PRESSURE ON MANUAL.  BOTH GENERATORS THEN DROPPED OFF LINE.  CREW GOT THEM BAC ON LINE AND DIVERTED FLIGHT TO LAS WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER.  OPS CHECKED ENGINE GENERATORS, NO PROBLEMS NOTED.  REFERENCE NR USAA950241.


REMARKS:
PIT - FLT 670 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  RIGHT PACK ON MEL AND LEFT PACK VERY WEAK.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED RIGHT TURBO FAN VALVE AND FLOW CONTROL VALVE.  REFERENCE USAA950247.


REMARKS:
PIT - FLT 1406 - FLIGHT EN ROUTE CMH TO TPA WHEN CREW REPORTED A PRESSURIZATION PROBLEM.  AIR LEAK AND LOUD AIR NOISE HEARD FROM FORWARD ENTRY DOOR.  FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPOSITIONED HINGE PIN IN UPPER HINGE COVER.  FOUND AFT OUTFLOW VALVE NOT COMPLETELY CLOSING.  REPLACED OUTFLOW VALVE AND CONTROLLER.  RESEALED INNER AREA AROUND EXTERNAL POWER RECEPTACLE.  REFERENCE USAA950248 .


REMARKS:
BGM - FLT 0746 - THE RED LANDING GEAR DOOR LIGHT REMAINED ON AFTER TAKEOFF FROM BFM.  THE GEAR WAS RECYCLED BUT THE LIGHT REMAINED ILLUMINATED.  FLIGHT CONTINUED TO PIT WITH GEAR DOWN.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE INSTALLED THREE RIVETS, ADJUSTED STOPS AND REPLACED THE RIGHT MAIN LANDING GEAR DOOR SADDLE BRACKET.  THE DOOR WAS RIGGED AND GEAR SWING PERFORMED.  ALL INDICATIONS WERE NORMAL.  (W)


REMARKS:
LAS - FLT 414 - EN ROUTE LAX TO MCI, CABIN PRESSURE BEGAN CLIMBING.  DROPPED TO FL 290 AND CREW WAS ABLE TO CONTROL PRESSURE ON MANUAL.  BOTH GENERATORS THEN DROPPED OFF LINE.  CREW GOT THEM BAC ON LINE AND DIVERTED FLIGHT TO LAS WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER.  OPS CHECKED ENGINE GENERATORS, NO PROBLEMS NOTED.  REFERENCE NR 95ZZZW420.


REMARKS:
DCA - LEFT SEAT EMERGENCY LIGHT ON ROW 10 INOPERATIVE.  MAINTENANCE REPLACED LIGHT ASSEMBLY.  (W)


REMARKS:
PIT - FLT 0541 - THE COCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - THE FLOOR LEVEL LIGHTING WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPAIRED A BROKEN WIRE IN THE FIRST SEGMENT OFFLOOR TRACK LIGHTING.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
TPA - FLT 60 - ON CLIMB-OUT FROM TPA, LEFT ENGINE PYLON PANEL CAME OFF.  FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE PLACED PANEL ON CDL 54-20-1 AND RELEASED AIRCRAFT.  REPLACED NACELLE STRUT ACCESS DOORON LEFT ENGINE PYLON.  (W)


REMARKS:
PIT - FLT 670 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  RIGHT PACK ON MEL AND LEFT PACK VERY WEAK.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED RIGHT TURBO FAN VALVE AND FLOW CONTROL VALVE.  REFERENCE 95ZZZW421.


REMARKS:
PIT - FLT 1406 - FLIGHT EN ROUTE CMH TO TPA WHEN CREW REPORTED A PRESSURIZATION PROBLEM.  AIR LEAK AND LOUD AIR NOISE HEARD FROM FORWARD ENTRY DOOR.  FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPOSITIONED HINGE PIN IN UPPER HINGE COVER.  FOUND AFT OUTFLOW VALVE NOT COMPLETELY CLOSING.  REPLACED OUTFLOW VALVE AND CONTROLLER.  RESEALED INNER AREA AROUND EXTERNAL POWER RECEPTACLE.  REFERENCE 95ZZZW422.


REMARKS:
PIT - FLT 1797 - FLIGHT EN ROUTE MCI TO LGA WITH NR 2 ENGINE OIL QUANTITY DECREASING.  FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE BAGGED DRAINS AND RAN ENGINE AT TAKEOFF POWER.  NO LEAKS FOUND, NO OIL IN INLET OR TAILPIPE.  FERRIED AIRCRAFT TO GSO.  FOUND CSD DRIVE PAD LEAK.  REPLACED ENGINE.  (W)


REMARKS:
JFK - FLT 253 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT AND LANDING GEAR UNSAFE LIGHTS ILLUMINATED.  PLACED LANDING GEAR SELECTOR TO DOWN AND ALL DOWN, AND LOCKED INDICATION ILLUMINATED.  VERIFIED LANDING GEAR DOWN.  FOUND LANDING GEAR BYPASS VALVE IN THE BYPASS POSITION.  STOWED AND LATCHED LANDING GEAR BYPASS VALVE.  GROUND CHECKS OF LANDING GEAR CHECKED NORMAL.  CHECK C-1D - 11-14-94 - MCI.


REMARKS:
STL - DURING CHECK-C, FOUND A .50 INCH AND A .25 INCH LONG SKIN CRACK AT TWO FASTENERS, STA 68.5.  REPAIRED PER ARA 8823, USING SRO 9530239. AIRCRAFT TOTAL TIME:  60,099 HOURS; 71,912 CYCLES.


REMARKS:
ON TAKEOFF, FIRST OFFICER'S AIRSPEED AND ALTIMETER INDICATORS BECAME INOPERATIVE.  BUFFET ALERT ON CDU, AND SPEED TRIM FAIL LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACED FIRST OFFICER'S AIR DATA COMPUTER PER BOEING MM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 480, S2L, S3L, AT BS 500D, S3L, AT BS 616, S3L, AND AT BS 440, S16L.  REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTS AT BS 1012, AT S14-15L, AT BS 927 AND 947.5, BETWEEN S18 AND 19L, AT BS 887 AND 907, BETWEEN S17 AND 18L, AT BS 310 AND 326, S21 TO 22R, AT BS 1006, S12 TO 13L, AT 1004, S11 TO 12L, AT BS351, BETWEEN S25 AND 26L, AT BS 366, AT S5L, AND AT BS 950,  BL 0.  REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 1 SPOILER SKIN DENTED 2 PLACES ON UPPER SURFACE.  REPAIRED PER BOEING STRUCTURALREPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 3 SLAT SKIN CRACKED AT T/E.  REPAIRED PER BOEING DRAWING BAC 65C30133.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CREASED AT BS 1100, AT S16L AND AT BS 1112, S17L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND NUMBER 5 GROUND SPOILER DENTED 2 PLACES ON LOWER SURFACE.  REPAIRED PER TRAMCO EWO 95-0222.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.7, WL 184.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SUPPORT ANGLE CORRODED AT BS 1121, RT SIDE, 10 INCHES ABOVE APU AIR INLET OPENING.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME TO INTERCOSTAL STRAP AT BS 993, WL 247 DAMAGED.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED ON RIGHT SIDE OF APU TORQUE BOX FROM BS 1088 TO 1138, WL 230.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR WEB CRACKED AT BS 312, BL 0, WL 207.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR UPPER FRAME CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 294, CRACKED AT RBL 54, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD UPPER FRAME OF AFT ENTRY DOOR CRACKED.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT UPPER FLANGE, BS 947, BL 0 TO LBL 10.  REPAIRED PER TRAMCO EWO 95-0231 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 18.5 TO 23.5, WL 208.  REPAIRED PER TRAMCO EWO 95-0231 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 1 TO RBL7, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD GALLEY DOOR LOWER HINGE CUTOUT CRACKED 2 PLACES.  REPAIRED PER SWA ACO 3189-52.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 500A PLUS 8, BETWEEN S21 AND 22L, AT BS 500, BETWEEN 23 AND 24L, AND AT BS 460, BETWEEN S23 AND 24L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
IN FLIGHT, NUMBER 1 AND 2 ENGINE HYDRAULIC PUMPS INDICATED LOW PRESSURE, 'A' SYSTEM QUANTITY DISPLAYED ZERO.  AIRCRAFT RETURNED TO SAT AND MADE AN UNEVENTFUL LANDING.  AFTER LANDING, SYSTEM 'A' INDICATED 1.5 GAL AND BEFORE REACHING GATE, INDICATED 2.5 GAL.  FOUND O-RING RUPTURED ON NR 2 'A' SYSTEM PRESSURE SWITCH.  REMOVED AND REPLACED BOTH ENGINE DRIVEN PUMPS, LOW PRESSURE SWITCH, CASE DRAIN FILTERS, AND SYSTEM 'A' FILTER.  OP/PRESSURE CHECKED SYSTEM PER BOEING MM, NR 1 PUMP S/N MX398721 AND NR 2, MX369280.


REMARKS:
AFTER DEPARTURE, THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  REPLACED BOTH ISOLATION PRESSURE SWITCHES AND T/R ISOLATION MODULE.  LEAK AND OPS CHECKED NORMAL PER BOEING MM.


REMARKS:
DURING CLIMBOUT, NUMBER 1 ENGINE OIL TEMP INDICATOR ENTERED YELLOW RANGE FOR 14 MINUTES.  AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND NR 1 ENGINE OIL TEMP SENSOR CANNON PLUG PIN B BROKEN.  REPLACED PIN ANDPERFORMED ENGINE POWER ASSURANCE RUN PER BOEING MM.


REMARKS:
FIFTEEN MINUTES BEFORE PUSHBACK, EMERGENCY LIGHTS ILLUMINATED WITH NORMAL AIRCRAFT POWER APPLIED AND SWITCH IN ARMED POSITION.  INSPECTED AND REPAIRED WIRE ON AFT GALLEY EMERGENCY LIGHT SWITCH PER BOEING MM.


REMARKS:
DURING SCHEDULED B/C CHECK, FOUND FWD SERVICE DOOR UPPER HINGE CUTOUT CRACKED IN UPPER CORNER.  REPAIRED PER SWA RA 1-252-207.


REMARKS:
DURING SCHEDULED B/C CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED IN LOWER CORNER.  REPAIRED PER SWA RA 1-352-206.


REMARKS:
DURING SCHEDULED QUARTER D-CHECK, FOUND STABILIZING STRAP IN E/E COMPT CRACKED AT BS 312, AT BOTTOM OF FLOORBEAM, BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED .75 INCH AT BS 767 AND STRINGER 19R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED QUARTER D-CHECK, FOUND NUMBER 2 ENGINE STRUT INNER SKIN CRACKED AT O/B EDGE OF PANEL 5827R OPENING.  CRACK RUNS BEYOND STOP DRILL AND UNDER CROWN SKIN.  INSTALLED DOUBLER PER ACO 6135-54.


REMARKS:
DURING SCHEDULED QUARTER D-CHECK, FOUND FUSELAGE SKIN CRACKED 1.2 INCH AT AC GROUND SERVICING CUTOUT, RBL 5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
JFK - FLT 481 - DURING CLIMB, SHUT DOWN LEFT ENGINE DUE TO LOUD BANG AND INCREASING EGT.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE, SN 3218.  GROUND RUN-UP AND OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  27,663 HOURS; 14,695 CYCLES.  CHECK OP-16 - 8-17-94 - MCI.


REMARKS:
BOS - FLT 184 - DURING CRUISE ONE HOUR AFTER TAKEOFF, NLG RED UNSAFE LIGHT ILLUMINATED.  DURING APPROACH, RED UNSAFE LIGHT REMAINED ON.  CYCLED LANDING GEAR AND LIGHT WENT OUT.  FOUND NLG PROXIMITY SENSOR MFG PN 8-337-03 BAD.  REPLACED NLGPROXMITY SENSOR.  NOSE LANDING GEAR POSITION AND WARNING SYSTEM CHECKED NORMAL.  CHECK C2D 9-14-94 MCI.


REMARKS:
JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED.  USED MECHANICAL LANDING GEAR EXTENSION.  REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100-109, AND LANDING GEAR CONTROL VALVE, MFG P/N 2680262M6.  LANDING GEAR SYSTEMOPERATION CHECKED NORMAL.  REFERENCE 95ZZZW441.


REMARKS:
JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED.  USED MECHANICAL LANDING GEAR EXTENSION.  REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100-109, AND LANDING GEAR CONTROL VALVE, MFG P/N 2680262M6.  LANDING GEAR SYSTEMOPERATION CHECKED NORMAL.  REFERENCE 95ZZZW440.


REMARKS:
BWI - FLT 2476 - ON CLIMB-OUT OF BWI, LOUD WHISTLING NOISE HEARD COMING FROM FORWARD ENTRY DOOR, FOLLOWED BY A LOUD BOOM.  FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED UPPER HINGE SEAL AND SEAL BRACKET.  REFERENCE USAA950240.


REMARKS:
BWI - FLT 2476 - ON CLIMB-OUT OF BWI, LOUD WHISTLING NOISE HEARD COMING FROM FORWARD ENTRY DOOR, FOLLOWED BY A LOUD BOOM.  FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED UPPER HINGE SEAL AND SEAL BRACKET.  REFERENCE 95ZZZW459.


REMARKS:
CLT - FLT 2188 - EN ROUTE TPA TO LGA, LOST 'A' SYSTEM HYDRUALIC QUANTITY, FOLLOWED BY LOW 'A' PRESSURE LIGHTS.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND NOSE GEAR ACTUATOR LINE LEAKING AT 'B' NUT.  REPLACED LINE, BOTH 'A' SYSTEM PRESSURE FILTERS, AND BOTH ENGINE DRIVEN PUMPS CASE DRAIN FILTERS.  (W)


REMARKS:
PIT - FLT 0239 - AIRCRAFT RETURNED TO PIT DUE TO A GENERATOR PROBLEM.  MAINTENANCE REPLACED THE RIGHT ENGINE CSD AND THE RIGHT ENGINE GENERATOR FOR TROUBLESHOOTING.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK IN STRINGER S-16 R BS 500 C PLUS 4 INCHES.  REPAIRED PEREO 5393X228.  (W)


REMARKS:
IND - DURING SCHEDULED CX-2 INSPECTION, FOUND A 1 INCH CRACK EXTENDING FROM VERTICAL LEG INTO HORIZONTAL LEG OF STABILIZER TO FUSELAGE ATTACH ANGLE.  CUT OUT DAMAGED SECTION AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-05 FIG NR 23A. (W)


REMARKS:
IND - DURING SCHEDULED CX-5 INSPECTION, FOUND .5 INCH CRACK IN FRAME AT STATION 389 AT LONGERON 17R.  CUT OUT DAMAGED AREA, INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-04 FIG 35 AND USAIR EA 29574.  (W)


REMARKS:
PIT - DURING MAINTENANCE WALK AROUND CHECK, FOUND .5 INCH CRACK IN INNER AND OUTER SKIN AT AFT CORNER OF AIR STAIR LOWER CORNER STATION 200.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-05 FIG 57A.  (W)


REMARKS:
CLT - FLT 2195 - FLIGHT EN ROUTE DCA TO MSY WITH NR 2 LEADING EDGE FLAP INTRANSIT LIGHT ILLUMINATED.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 LEADING EDGE FLAP DOWN SENSOR AND FLAP/SLATPOSITION MODULEIN E/E COMPARTMENT.  OPS CHECK NORMAL (W)


REMARKS:
PIT - FLT NR 497 - LOUD VIBRATION ON FORWARD RIGHT PART OF AIRCRAFT.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE CLOSE FORWARD LAV SERVICE LATCH.  NO OTHER FAULTS FOUND ON FORWARD FUSELAGE OF AIRCRAFT, OK FOR SERVICE.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM CORRODED 2 INCH BY 72 INCH AREA (CLIP NUT HOLES) BS 328.  REPAIRED PER SRM 51-70-12 AND TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM CORROSION AT CHIP NUT HOLES BS 312 RBBL 24 TO LBBL 30.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION ,FOUND SEAT TRACK 1 INCH BY 8 INCH CORRODED AREA BS 340 RBL 44.  REPAIRED PER SRM 52-00-52 FIG 201.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEAT TRACK 2 INCH BY 24 INCH CORRODED AREA BS 340-364 RBL 24.  REPAIREDPER SRM 53-00-52 FIG 201.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEAT TRACK 2 INCH BY 12 INCH CORRODED AREA BS 277-294 RBL 24 INBOARD SIDE OF NR 1 GALLEY.  REPAIRED PER SRM 53-00-52 FIG 202.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 60 INCH STATION 986.5 ENTIRE LENGTH.  REPAIRED PER TR 53-10-5.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM (2) 1 INCH BY 1 INCH CORRODED AREAS (ABOUT .060 INCH DEEP), LBL 6 AND RBL 6 AT BS 947.  REPAIRED PER SRM 53-00-51 FIG 202.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 .5 INCH BY 1 INCH CORRODED AREAS (ABOUT .050 INCH DEEP), BS 328-344 RBBL 12 (CABIN FLOOR SUPPORT).  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES, BS 312-328 LBBL 12.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION 1 INCH BY 15 INCH AND 1 INCH BY 3 INCH FOR TOTAL OF 1 INCH BY 18 INCH, BS 300 THROUGH BS 344 AT FORWARD CABIN (LEFT SIDE) ENTRY DOOR.  REPAIRED PER SRM 51-10-4.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCH BY 1 INCH BY 6 INCH EQUALS 1 INCH BY 36 T, BS 277-BS 328 FORWARD SERVICE DOOR ANGLE.  REPAIRED PER SRM 51-10-4.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.(W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION AT CLIP NUT HOLES BS 320-344 LBBL 12.  REPAIRED PER SRM51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH BY 1 INCH CORRODED AREA (ABOUT .050 INCH DEEP), BS 312-328RBBL 12 (CABIN FLOOR SUPPORT).  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORRODED SEVERAL NUT PLATES BS 947 BS 1006.  REPAIRED PER SRM 51-10-02 PG 16.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
CLT - FLT 731 - FLIGHT EN ROUTE PHL TO MSY WHEN FORWARD NR 2 MAIN TANK FUEL BOOST PUMP LOW PRESSURE LIGHT CAME ON.  FLIGHT DIVERETED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 FORWARD BOOST PUMP PER MM 28-22-41.  NO LEAKS NOTED, OPS CHECK GOOD.  (W)


REMARKS:
STL - DURING CRUISE, SINGLE SERVE CART S/N 0458 OVERHEATED CAUSING SMOKE IN LOWER GALLEY.  DISCONNECTED ELECTRICAL CABLE.  REPLACED SINGLE SERVE CART MFG P/N 888011 AND OPERATION CHECKED NORMAL.


REMARKS:
PIT - FLT 0233 - LOW POWER ON THE RIGHT ENGINE ON CLIMB-OUT.  FLIGHT RETURNED TO PIT.  SINGLE ENGINE TIME WAS TWELVE MINUTES.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP.  THE RIGHT ENGINE FUELCONTROL UNIT WAS ALSO REPLACED AS A PRECAUTION.  OPERATIONS CHECKED GOOD.  REFERENCE CONTROL USAA950304.  (X)


REMARKS:
PIT - FLT 0233 - LOW POWER ON THE RIGHT ENGINE ON CLIMB-OUT.  FLIGHT RETURNED TO PIT.  SINGLE ENGINE TIME WAS TWELVE MINUTES.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP.  THE RIGHT ENGINE FUELCONTROL UNIT WAS ALSO REPLACED AS A PRECAUTION.  OPERATIONS CHECKED GOOD.  REFERENCE CONTROL 95ZZZX1856.  (X)


REMARKS:
CLT - THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND BATTERY PACK.  OPERATIONS CHECKED GOOD.  REFERENCE USAA950307.


REMARKS:
PIT - DURING SCHEDULED SIP INSPECTION, FOUND CRACK IN THE FORWARD PRESSURE BULKHEAD LOWER CONNECTION ANGLE AT FRAME 1550 BETWEEN STATION 72 AND 3.  STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-11-00.  (W)


REMARKS:
PIT - DURING SCHEDULED SIP INSPECTION, FOUND .1250 INCH CRACK IN MID CARGO DOOR HINGE FWD END.  EDDY CURRENT INSPECTIONREF SIP 52-30-09 PG 2.  REMOVED AND REPLACED CARGO DOOR PER F28 MM 52-30-01.  (W)


REMARKS:
PIT - DURING SCHEDULED STRUCTURES VISIT (SIP) FOUND A .375 INCH CRACK IN AFT CARGO DOOR HINGE LUG (AFT END).  REMOVED AND REPLACED HINGE LUGS WITH NEW MODIFIED HINGE P/N D28410-409 PER USAIR EO NR 5294X201.  (W)


REMARKS:
PIT - DURING SCHEDULED STRUCTURES VISIT (SIP) FOUND .1250 INCH CRACK IN MID CARGO DOOR HINGE LUG.  EDDY CURRENT INSPECTION REF SIP 52-31-09.  REMOVED AND REPLACED HINGE LUG WITH NEW MODIFIED HINGE P/N D28410-409 PER USAIR EA NR 5294X201.  (W)


REMARKS:
PIT - THE EMERGENCY LIGHTS AT ROW 15ABC WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND BATTERY PACK.  OPERATIONS CHECKED GOOD.  REFERENCE 95ZZZW525.


REMARKS:
INT - DURING Q-4 CHECK VISUAL EDDY CURRENT INSPECTION, FOUND 27 INCH CHAFED AREA BY .25 INCH WIDE BS 860 TO BS 887 S-2 LEFT TO S-2 RIGHT.  REPAIRED PER SRM 53-00-01 AND TR 53-30-03.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION UNDER FWD BELLY AT MARKER BEACON ANTENNA.  INSTALLED DOUBLERREPAIR PER USAIR EA 29959.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION LONGERON NR 1 AND SKIN LAP JOINT STATION 263-275 NR ADF LOOPAND STATION 300-308 NR 2 ADF LOOP ANTENNA.  CLEANED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 29 AND USAIR EA 29614A.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND CRACK .75 INCH LONG AT STATION 1463 CANTED FRAME WEB.  CUT OUT DAMAGED SECTION OF WEB AND MANUFACTURED NEW WEB PER USAIR EA 27544.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND .1250 INCH CRACK AT STATION 1437 LONGERON 3L IN SKIN.  CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-04 FIG 38 FIG 38 VIEW L.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND A 1.75 INCH CRACK BETWEEN STATION 1287 AND STATION 1309 LEFT SIDE CUSP MEMBRANE.  MANUFACTURED NEW SECTION OF CUSP MEMBRANE AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-05 FIG 97.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION BETWEEN STATION 180 AND 203 FORWARD GALLEY AREA AND SERVICE DOOR THRESHOLD JAMB PAN, CUSP ANGLE LOWER CORNER OF SERVICE DOOR OPENING.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT FORWARD CARGO DOOR JAMB BETWEEN STATION 370 AND 427.  REPLACED PAN AND SPLICED WITH REPAIR DOUBLERS PER SRM 53-05 FIG 44.  (W)


REMARKS:
BOS - THE EMERGENCY EXIT LIGHT ON THE LOWER RIGHT WING EXIT WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE OVERWING EMERGENCY BATTERY PACK AND BATTERY.  (W)


REMARKS:
PIT - THE RIGHT EMERGENCY EXIT LIGHTS WERE INTERMITTENT.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
CLT - THE EMERGENCY EVACUATION LIGHTS WILL NOT ILLUMINATE WHEN THE COCKPIT SWITCH IS USED.  MAINTENANCE REPLACED THE DIODE (LV96) FOR THE EMERGENCY LIGHTS.  OPERATIONS CHECKED NORMAL.  (W)


REMARKS:
JAX - FLT 1606 - ON CLIMB NR 2 OIL FILTER BYPASS LIGHT ILLUMINATED.  RETARDED THROTTLE AND LIGHT WENT OUT.  FLIGHT DIVERTED TO JAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  REPLACED RIGHT MAIN OIL FILTER BYPASS SWITCH AND RIGHT MAIN OILSCREEN.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK IN VERTICAL STAB STATION ZFS 52.3 5TH RIB, CRACK AT SIDE END. INSTALLED DOUBLER REPAIR PER SRM 55-02 FIG 27.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH SKIN CRACK AT CUSP MEMBRANE AT STATION 604 LONGERON 18R STATION 59818L.  INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 96.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND LEVEL I CORROSION AT CUSP MEMBRANE AT STATION 945 RT SIDE.  REMOVED CORRODED SECTION OF MEMBRANE AND INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 96.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND .035 GAUGE 7 INCH LONG IN VERTICAL STAB AT STA ZV133 LT SIDE.  INSTALLED DOUBLER REPAIR PER SRM 35-01 FIG 2.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND .25 INCH CRACK IN KEEL FITTING BELOW CENTER TANK REAR SPAR FWD OF MLG DOOR.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK RIGHT UPPER PYLON ATTACH ANGLE STATION 1019.  INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND .25 INCH SKIN CRACK IN FUSELAGE SKIN WITHIN PYLON LEFT SIDE AT STATION 996LONGERON 16L.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 17A.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND TEMPORARY CLASS II REPAIR INSTALLED AT STATION 503 LONGERON 25L AND 24L.  REMOVED TEMPORARY REPAIR AND INSTALLED FLUSH REPAIR PER USAIR TYPICAL REPAIR 53-30-08.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK LEFT FLAP UPPER STRINGER UPPER SPAR CAP AT XFIS-244.  INSTALLED DOUBLER REPAIR PER DACO DWG 995750 AND USAIR EA 29548.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND CORROSION LEFT WING AFT LOWER SPAR, LOWER FLANGE STATION XRS 546.  REMOVEDCORROSION AND INSTALLED DOUBLER REPAIR PER SRM 57-09 FIG 11.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND A .75 INCH CRACK ON EACH SIDE OF RIVET HEAD AT STATION 996 ABOVE RT PYLON LAWN ATTACH ANGLE, IN SKIN.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 17A.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND CORROSION .033 DEEP AT NR 2 ADF LOOP ANTENNA IN SKIN.  REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 29.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND LEVEL I CORROSION REF C57-5330 FUSELAGE SKIN AFT SIDE OF FRAME STATION 945BETWEEN LONGERON 28R AND 29R.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B.  (W)


REMARKS:
PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND SMALL DENT AND CRACK .1250 INCH AT 5910158-35 WEB AT FUSELAGE STATION 900 LONGERON 25R SID PSE 53.09.035A.  INSTALLED DOUBLER REPAIR PER DACO 5910158 AND USAIR EA NR 29704.  (W)


REMARKS:
GSO - DURING UNSCHEDULED MAINTENANCE VISUAL INSPECTION, FOUND 1.5 INCH CRACK, FORWARD END OF WEB AT THE NLG ACTUATOR SUPPORT FITTING BEAM AT STATION 227.  REPAIRED PER EA 30088, SRM 51-40-2 FIG 1.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND .1250 INCH CRACK STATION 160 LONGERON 4 LEFT.  CUT OUT DAMAGED SECTION AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 FIG 02.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND .25 INCH CRACK STATION 160 LONGERON 3 LEFT.  CUT OUT DAMAGED SECTION OF LONGERON ANDSPLICED IN NEW SECTION PER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND .3125 INCH CRACK STATION 160 LONGERON 2 LEFT.  CUT OUT DAMAGE SECTION OF LONGERON AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND GOUGE JUST AFT OF SERVICE DOOR CUSP MEMBRANE STATION 200 LONG 18R.  CUT OUT CUSP MEMBRANE SECTION AND INSTALLED REPAIR SECTION PER SRM 53-05 FIG 9.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND A 1 INCH BY 100 INCH DEEP DENT AT STATION 408 LONGERON 17 LEFT.  INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW G.  (W)


REMARKS:
PIT - DURING Q2 INSPECTION, FOUND CRACK .5 INCH LONG STATION 160 FORWARD AIR STAIR CUT OUT UPPER FWD CORNER SKIN.  CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-05 FIG 57A VIEW G.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND GOUGE RT VERTICAL STAB SKIN PANEL.  BURNISHED GOUGES AREA AND INSTALLED INTERNAL DOUBLER PER USAIR EA 29729 AND SRM 55-01 FIG 2 SHEET 2.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND .25 INCH CRACK AT STATION 256 LONGERON 17 LEFT.  CUT OUT DAMAGED SECTION AND SPLICEDIN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1338 AFT CARGO AREA BETWEEN LONGERONS 28L AND 28R.  REMOVED CORROSION, CLEANED AND TREATED.  INSTALLED REPAIR DOUBLERS PER SRM 53-03 FIG 3 PER USAIR TYPICAL REPAIR 53-30-10.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AFT CARGO DOOR THRESHOLD AT STATION 1155-1220 WEB AND STRAP.  REMOVED AND REPLACED WEB AND STRAP PER DACO DWG NR 5936442.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION ON FUSELAGE LOWER SKIN BETWEEN 1155 AND 1174.  CUT OUT DAMAGED SKIN AND INSTALLED REPAIR WITH EXTERNAL DOUBLER PER SRM 53-04 FIG 12B AND USAIR EA NR 29833.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1309 BETWEEN LONGERON 28L AND 29R ON BELTFRAME 'J'.  CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-03 FIG 7.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1322 BETWEEN AFT GALLEY AND AFT LAV CENTER AISLE.  REMOVED CORRODED AREA AND INSTALLED FILLER AND REPAIR ANGLE PER USAIR TYPICAL REPAIR 53-10-19.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION SKIN AT STATION 769 LONGERON 28 RT.  CLEANED AND TREATED CORRODEDAREA AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 53.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 807 LONGERON 29 LEFT SKIN.  CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 53.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193-1212 LONGERON 28L.  REMOVED REPLACED SPLICE PER SRM 53-02 FIG 16.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193 AND 1212 LONGERON 29 LEFT.  REMOVED AND REPLACED CORRODED SPLICE PER SRM 53-00 FIG 16.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1322 FLOOR BEAM AFT RT LAV.  CUT OUT DAMAGED AREA AND INSTALLED FILLER AND REPAIR ANGLE DOUBLERS PER SRM 53-10-19.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1338 RT SIDE UPPER TO LOWER FRAME ATTACH LONGERON 18R CUSP.  REMOVED CORROSION, TREATED AND REPLACED FITTING PER DACO PRINT REF NR 5913700.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION STATION 1338 RT SIDE UNDER LAV THRESHOLD FLOOR BEAM AREA.  CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-05 FIG 72.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION REF C58-53301 AT STATION 1344 AFT LEFT GALLEY ATTACHMENT AT FLOORBEAM 1338 TO AFT PRESSURE BULKHEAD AT FLOOR LEVEL.  MANUFACTURED INTERCOSTAL AND REPLACED PER SRM 53-14.  (W)


REMARKS:
PIT - DURING Q-2 INSPECTION, FOUND DENT 1 INCH BY 1.75 INCH BY .75 INCH DEEP BETWEEN STATION 275 AND 294 LONGERON 23L AND 27L IN SKIN AREA.  INSTALLED DOUBLER REPAIR PER SRM 53-04 SH 17 FIG 38.  (W)


REMARKS:
ORF - FLT 2323 - ON TAKEOFF AT V2, CREW HEARD A LOUD BANG.  FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  BIRD STRIKE ON RT ENGINE.  INSPECTED PER MM 5-51-201, PAGE 201.  RAN ENGINE AND ALL PARAMETERS NORMAL.  (W)


REMARKS:
PBI/ATL - FLT 502 - RIGHT GEAR UNSAFE LIGHT ON AFTER GEAR RETRACTION, RIGHT GEAR FAILED UPLOCK CHECK; CYCLED GEAR, OPS CHECK OKAY, ALL GEAR INDICATION NORMAL.  REMOVED AND REPLACED RIGHT MLG UPLOCK SWITCH PER MM 32-00.


REMARKS:
MSY/ATL - FLT 160 - RIGHT GEAR UNSAFE LIGHT ON WITH GEAR HANDLE UP.  FOUND DEFECTIVE LAMP.  RELAMPED, JACKED AND SWUNG GEAR.  ALL OPERATIONS NORMAL PER MM 32-60.


REMARKS:
DFW/ATL - FLT 234 - HAD TO DIVERT TO MEM DUE TO CABIN DE-RESSURIZATION.  AUTOPRESSURIZATION FAILED AND OXYGEN MASKS DEPLOYED, EXCEPT 4 AT ROWS 5C, D, AND E.  REMOVED AND REPLACED OYGEN BOTTLE AND DROP-CHECKED OXYGEN MASKS.  OPS CHECK OKAY,PLACED AUTOPRESS ON MEL.


REMARKS:
RDU/ATL - FLT 299 - AIR RETURNED TO RDU DUE TO LANDING GEAR HANDLE WOULD NOT RETRACT, CABIN WOULD NOT PRESSURIZE AND NOSE WHEEL STEERING STILL WORKED.  CYCLED GROUND CONTROL CIRCUIT BREAKERS, NO HELP.  FOUND FLAT NOSE STRUT SERVICED PER MM12.  LANDING GEAR HANDLE OPS CHECK OKAY.


REMARKS:
ATL/TPA - FLT 537 - FLIGHT CREW UPON STARTING APU, NOTICED A FUEL SMELL.  PLACED APU ON MEL 49-1 SEQUENCY NR 1331 DUE TO INOPERATIVE FUEL CONTROL DIAPHRAGM.


REMARKS:
ATL/SDF - FLT 350 - RETURNED TO THE GATE FOR A SLAT DISAGREEMENT LIGHT.  REMOVED AND REPLACED LT AND RT SLAT DISAGREEMENT WITH, PN H20-21B-N5N.


REMARKS:
EWR - AFTER AN OVERNIGHT SERVICE, AIRCRAFT WAS TAXIING FROM HARD STAND TO GATE, SMOKE WAS COMING FROM LEFT AFT LAV.  FOUND AFT LAV FLUSH MOTOR EMITTING SMOKE.  REPLACED LAV FLUSH MOTOR, TIMER AND CIRCUIT BREAKER.  TIMER, PN 2123M100, BREAKER, PN BACC18W5.  (X)


REMARKS:
PBI - FLT 54 - ON TAKEOFF, WHEELWELL LIGHT AND BELL CAME ON.  RETURNED TO PBI.  REMOVED AND REPLACED NOSE WHEELWELL FIRE LOOP AND AURAL WARNING CONTROL UNIT.  FIRE WARNING TEST PERFORMED ON ALL ENGINES, WHEELWELL, FIRE WALL AND APU.  ALL CHECKED GOOD.  NLG WHEELWELL LOOP, PN 356802255.  (X)


REMARKS:
MCO - FLT 74 - AFTER TAKEOFF ON RETRACTION TO 2 DEGREES, NR 8 LEADING EDGE SLAT INDICATED IN-TRANSIT, THE FLAP POSITIONINDICATOR WAS YELLOW.  NR 8 LEADING EDGE DID NOT RETRACT.  RETURNED TO MCO.  REMOVED AND REPLACED NR 8 SLAT ACTUATOR PER MM 27-81-20.  OPS CHECKED ACTUATOR PER MM 27-81-02.  OPS CHECKED GOOD.  LEAK CHECKED GOOD.  (X)


REMARKS:
FLT 9719 - AFTER TAKEOFF, LEFT GEAR AND DOOR LIGHT ON.  RETURNED TO EWR.  REMOVED AND REPLACED LEFT MLG WALKING BEAM ASSY IAW MM 32-32-2.  PERFORMED MULTIPLE GEAR SWINGS IAW MM 32-10-0.  ALL INDICATIONS SATISFACTORY.  (X)


REMARKS:
CLT - FLT 0741 - ON CLIMB-OUT, THE RED GEAR UNSAFE LIGHT AND YELLOW GEAR DOOR OPEN LIGHT ILLUMINATED.  CAPTAIN DECLAREDAND EMERGENCY AND FLIGHT RETURNED TO CLT.  MAINTENANCE REPLACED THE LEFT MAIN GEAR ACTUATING CYCLINDER.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION STATION 912-996 SKIN PANEL 5919707 LONGERON 26R TO 26L SKIN PANEL 5911424 LONGERON 18R-26R.  SPLICED IN 2 EACH SKIN PANELS PER USAIR EA 29955.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND PREVIOUS INTERNAL DOUBLER LOWER AFT CORNER OF FORWARD CARGO DOOR SURROUND OPENING STATION 427.  INSTALLED DOUBLER REPAIR PER DACO DWG SRO 9530117 AND USAIR EA 29648.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR INSTALLED STATION 313-332 LONGERON 22-24 RIGHT.  INSTALLED CLASS I REPAIR PER SRM 53-04 FIG 12B.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION RT INBOARD SEAT TRACK STATION 897 AND 965.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4E.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 30 AT SPLICE BETWEEN BELTFRAMES AT STATION 465 AND 484.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 14.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 14 LEFT STATION 1038.  SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND ONE .5 INCH CRACK IN STATION 980 TOP PYLON TO FUSELAGE ATTACH ANGLE RT.  INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 200 LONGERON 3 LEFT.  SPLICED IN SECTION OF LONGERON PER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION STATION 896-965 LEFT OUTBOARD SEAT TRACK.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION RT LAV STATION 996 WEB.  CLEANED CORROSION AND INSTALLED DOUBLER PER SRM 53-05 FIG 72.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION,  FOUND LEVEL I CORROSION FORWARD END OF LEFT OUTBOARD SEAT TRACK STATION 200.  SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE EXT PYLON ATTACH ANGLE TOP RT PYLON STATION 1019.  INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10.  (W)


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK LEFT FORWARD OVERWING EMERGENCY EXIT UPPER FORWARD CORNER DOOR STOP.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03.  (W)


REMARKS:
ATL/PBI - FLT 501 - STARTED DESCENT WHEN CREW NOTICED STABILIZER TRIM NOT FUNCTIONING.  AIRCRAFT LANDED WITHOUT INCIDENT IN PBI.  REPLACED PRIMARY TRIM MOTOR, PN 9590-6, SN ON 441, SN OFF 819.


REMARKS:
FLL/ATL - FLT 128 - ON FINAL APPROACH, LEFT THRUST REVERSER UNLOCK LIGHT ILLUMINATED AND CREW FELT HEAVY VIBRATION FROMTHE TAIL OF THE AIRCRAFT.  REMOVED AND REPLACED NR 1 ENGINE.


REMARKS:
FLL/ATL - FLT 128 - AFTER LANDING, AIRCRAFT TAXIED OFF OF ACTIVE RUNWAY WHERE THE NR 1 BRAKE LOCKED UP.  REMOVED AND REPLACED THE NR 1 AND NR 2 BRAKE ASSEMBLIES.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LWR SIDE NEXT TO RELEASE UPLOCK HOOK.  REPAIREDPER SWA ACO 3194-52.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT FUSELAGE SKIN CRACKED AT STRINGER S16R AT WING SCANNING LIGHT CUTOUT, AT AFT END OF FWD SECTION.  REPAIRED PER SWA ACO 6405-53.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND BELTFRAME CRACKED .125 INCHES AT RIVET HOLE, BS 482, RBL 1.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD CARGO DOOR CUTOUT WEB CRACKED AT BS 460, LWR AFT CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD CARGO FLOOR BEAM CRACKED AT BS 400, LBL 21.0.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
AFTER TAKEOFF, FLT NR 9003 RETURNED TO EWR AFTER ALL F/F INDICATORS FAILED.  REMOVED AND REPLACED FUEL FLOW POWER SUPPLY PER MM 73-31-12.  OPS OK.  FURTHER INVESTIGATION DETERMINED WIRE NR 198-14 SHORTED TO LFT ANTI-ICE VALVE C/P.  REPAIRED WIRE AND REPLACED P90 PLUG OF NR 1 F/F TRANSMITTER DUE SATURATION, PER 73-30.  OP CHECK OK.  AFTER BENCH CHECK OF F/F POWER SUPPLY BY AMETEK THERE WAS NO FAULT FOUND WITH UNIT.  (W)


REMARKS:
AFTER TAKEOFF EWR, FLT NR 9003, RETURNED TO EWR FOR SECOND TIME.  AFTER ALL FUEL FLOW INDICATORS FAILED.  FOUND WIRE NR198-014-18 SHORTED TO LEFT ANTI-ICE VALVE C/P.  REPAIRED WIRE AND REPLACED P90 PLUG OF NR 1 FUEL FLOW TRANSMITTER DUE SATURATION.  (W)


REMARKS:
PIT - FLT 0992 - ON TAKEOFF, THE RIGHT GENERATOR OFF LIGHT ILLUMINATED FOLLOWED BY AC CROSSTIE LOCKOUT.  CREW DECIDED TO RETURN TO PIT.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND STOWED LAV DUMP CABLE CHAFING ON GEN FEEDER CABLE.ACCOMPLISHED REPAIRS TO THE RIGHT ENGINE GENERATOR FEEDER CABLES.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
EN ROUTE PHX TO AUS, CREW EXPERIENCED NR 1 ENGINE COMPRESSOR STALL.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING.  BORESCOPED INSPECTED AND DETERMINED ENGINE CHANGE REQUIRED.  REPLACEDENGINE ASSEMBLY AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS: BS 910, WL 185, ABOVE STRINGER 19R, AT BS 932, AT S24L, AND AT BS 324, BETWEEN S22 AND 23R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED AT BS 306, WL 255, 3 INCHES BELOW FWD ENTRY DOOR ATHINGE UPPER HINGE CUTOUT.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN NICKED AND SCRATCHED AT BS 305 AND 320, BETWEEN S3 AND 4L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR SKIN DENTED AT BS 990-1016, BETWEEN S8 AND 10L.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FLOOR BEAM CORROSION  AT BS 986.5, RBL 45, WL 208, AT BS 294.5, LBL 19, WL 208,  AND AT BS 328, RBL 34 AND 48, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND LEFT AND RIGHT SKATE ANGLES CRACKED AT BS 570, WL 167.5, RBL 59.  REPLACED PER BOEING M/M.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO FRAME DENTED AT 727B, S24R, RBL 32.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND DEEP GOUGE AT FRAME AT BS 1104, AT S14R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FWD FRAME TO SIDEWALL SUPPORT DENTED AND GOUGED AT BS 439, WL 158, RBL 27.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 178, WL 195, ACCESS PLATE CUTOUT.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND SHEAR TIE CORRODED AT BS 927, LBL 22, WL 164.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN FROM BS 520 TO 578, BETWEEN S1 AND 3R, ANDAT BS 500D TO 520, BETWEEN S2 AND 3R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
EWR - A/C INBOARD LOG ITEM OMEGA UNABLE TO RECEIVE ANY STATION.  ON INSPECTION, FOUND OMEGA ANTENNA MISSING, MOUNTING RECEPTACLE AND CONNECTOR RIPPED OUT OF HORIZONTAL STABILIZER TAIL CONE.  REPAIRED MOUNTING RECEPTACLES FOR OMEGA ANTENNA PER SRM 51-40-9 AND REPLACED CONNECTOR AND OMEGA ANTENNA PER MM 34-68-11, OPS CHECK OKAY.  (X)


REMARKS:
MCO - FLT 1203 - FLIGHT RETURNED TO MCO DUE TO GEAR DOOR RETRACT PROBLEM.  FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE ADJUSTED THE CONTROL ROD.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
CLT - THE EMERGENCY LIGHT AT ROW 7 WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPAIRED THE EMERGENCY FLOOR TRACK LIGHT AT ROW 7.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
PIT - FLT NR 1206 - UPON GEAR RETRACTION, FLIGHT EXPERIENCED A LOUD NOISE AS THE NOSE GEAR WAS RETRACTED.  CREW EXTENDED THE LANDING GEAR AND RETRACTED AGAIN AND RECEIVED AN UNSAFE NOSE GEAR LIGHT.  FLIGHT RETURNED TO PIT.  MAINTENANCE REPLACED THE LEFT NOSE GEAR DOOR RETRACT CABLE AND HINGE.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
IND - FLT 1741 - FLIGHT ATTENDANT NOTICED A NOISE DURING FLIGHT WHICH WAS THE R4 DOOR SAFETY STRAP HITTING AGAINST THE SIDE OF THE AIRCRAFT.  FLIGHT DIVERTED TO IND FOR INSPECTION.  MAINTENANCE INSPECTED THE R4 DOOR FOR DAMAGE.  FOUND TO BE WITHIN LIMITS.  OK FOR SERVICE.  (W)


REMARKS:
CLT - FLT 0346 - FLIGHT EXPERIENCED SLAT EXTENSION PROBLEMS.  THE FLAPS/SLATS EXTEND LIGHT WOULD NOT STAY ON.  FLIGHT RETURNED TO CLT WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND THE LEFT LEADING EDGE ADVISORY SWITCH STICKING.  THE SWITCH WAS REPLACED AND THE FLAPS ALL CHECKED NORMAL.  (W)


REMARKS:
FLT NR 523 - ATL-MCO - BURNED SMELL IN COCKPIT, SMELL DISSIPATED AND DID NOT RETURN.  REPLACED BALLAST TRANSFORMER, P/NNR BA1701.


REMARKS:
STL - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BIN LOWER DOOR JAMB INNER PANEL, FROM FORWARD LOWER CORNER TO AFT SIDE.  REPAIRED PER SRM 53-05, FIGURE 14.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND CRACKS 1.75 INCHES LONG ON BOTH SIDES OF SPLICE, LONGERON 30, STATION 446.  REPAIRED PER SRM 53-02, FIGURE 14, SHEETS 1 AND 2, AND STANDARD PRACTICES.


REMARKS:
MCI - DURING OP-17, FOUND CORROSION IN AFT CARGO BIN, ON LEG OF STRINGER 29L, AROUND TWO HI-LOCKS, FS 990.  REPAIRED PER ARA 9054.


REMARKS:
MCI - DURING C-CHECK, FOUND A .25 INCH CRACK IN PRESSURE DECK OUTBOARD END, STATION 940.  STOP DRILLED CRACK AND REPAIRED PER ARA 9117A.


REMARKS:
MADE UNSCHEDULED LANDING ACCOUNT NR 1 ENGINE 'A' FIREWARNING ILLUMINATED.  SHUT DOWN ENGINE AND DISCHARGED EXTINGUISHERBOTTLES.  'B' LOOP PREVIOUSLY PLACARDED ON MEL.  RESTORED 'B' LOOP BY REPLACEMENT OF LOWER AFT WARNING LOOP, MFG P/N 895398.  REPLACED EXPENDED BOTTLES AND PLACARDED 'A' LOOP PER MEL.  OPS CHECKS NORMAL.


REMARKS:
MCI - DURING OP-17 FOUND A SIX INCH LONG CRACK IN AFT CARGO BIN, STRINGER 29L, FS 1000.  REPAIRED PER ARA 9054.


REMARKS:
MCI - DURING C-CHECK, FOUND A ONE INCH LONG CRACK IN STRINGER 16, STATION 656.5.  REPAIRED PER SRM 57-20-201, FIGURE 207.


REMARKS:
MCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN FUSELAGE FRAME, FS 783.95.  REPAIRED PER SERVICE BULLETIN 727-53-0197, DRAWING NR 65C36280 AND EMLR 65639.


REMARKS:
FCO - DURING PERIODIC SERVICE CHECK, FOUND A NINE INCH CRACK IN RIGHT WING FRONT WING FRONT SPAR AT FSSI 675.5.  REPAIRED CRACK PER BOEING REPAIR DRAWING 691U0103 AND TWA ARA 9122.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STATION 832.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 4L, STATION 832.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
STL - DURING OP-15, FOUND A GOUGE IN LONGERON 6R, STATION 1000.  REPAIRED BY INSTALLING LONGERON SPLICE PER SRM 53-02.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN LONGERON 3R, STATION 734.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN LONGERON 3L, STATION 794 AND STA 832.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
STL - AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE ABOVE OFF POSITION.  ACCOMPLISHED LANDING GEAR HANDLE LOCK CHECKLIST AND RETRACTED LANDING GEAR.  FOUND NOSE LANDING GEAR TORQUE LINK PIN MISSING, MFG P/N 53173.  INSTALLED NEW NOSE GEAR TORQUE LINK PIN.  LANDING GEAR CHECKS NORMAL.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A 1.5 INCH CRACK IN LONGERON 4L, STA 794.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
SJU - DURING CRUISE, WINDSHIELD HEAT WIRE HARNESS SHORTED AT R-2 WINDOW CAUSING ARCING AND SMOKE IN COCKPIT.  TURNED OFF WINDSHIELD HEAT AND DISCHARGED HAND EXTINGUISHER.  REPLACED WINDSHIELD WIRING HARNESS AND WINDSHIELD HEAT CONTROLLER, MFG P/N 27261298-02.  WINDSHIELD HEAT OPERATION CHECKED NORMAL.


REMARKS:
JFK - DURING CRUISE, NR 1 NACELLE FIRE DETECTOR FAULT LIGHT ILLUMINATED WITH TEMPERATURES IN THE FAULT RANGE.  THEN NR 1 ENGINE FIREWARNING SOUNDED.  SHUTDOWN NR 1 ENGINE AND DISCHARGED BOTH EXTINGUISHER BOTTLES.  FOUND BOTH DETECTORS SHORTED.  REPLACED BOTH DETECTORS, MFG P/N 60B00023163 AND P/N 60B00023166.  PERFORMED POWER RUNUP AND NACELLE DETECTOR FAULT AND FIREWARNING SYSTEMS CHECKED NORMAL.


REMARKS:
MCI - DURING C-CHECK, FOUND TWO INCH CRACK IN INBOARD AFT SIDE OF FRAME, BELOW FLOOR LEVEL, FS 783.95.  STOP DRILLED CRACK AND INSTALLED REPAIR PER EMLR 65661.


REMARKS:
MCI - DURING C-CHECK, FOUND .5 INCH CRACK IN PRESSURE DECK EIGHT INCHES INBOARD OF 940 CASTING.  STOP DRILLED AND INSTALLED DOUBLER PER ARA 9130.


REMARKS:
MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 250, LOWER AFT RADIUS OF R3 COCKPIT WINDOW.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132.


REMARKS:
MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 252, AFT RADIUS OF R3 COCKPIT WINDOW.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132.


REMARKS:
MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STA 249, AFT RADIUS OF R3 COCKPIT WINDOW.  STOP DRILLED CRACKED AND INSTALLED DOUBLER PER ARA 9132.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN FROM BS 380 TO 440, BETWEEN S2 AND 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 952, 6 INCHES BELOW S17L.  REPAIRED PER TRAMCO EWO 95-0031.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND E AND E DOOR, LT FWD AND AFT O/B CORNERS DENTED AND GOUGED.  INSTALLED NEW SKIN PERBOEING SRM.


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178, LBL 57 AND WL 201.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


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


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT FLIGHT ATTENDANT PANEL EMERGENCY LIGHT SWITCH INOP.  REPLACED SWITCH PER BOEING M/M.


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


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


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


REMARKS:
AT GATE, FOUND AFT EMERGENCY FLASHLIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND SPAR WEB PUNCTURED AT BS 616, 4 INCHES FROM BOTTOM NEXT TO O/B SIDE OF O/B AUX TRACK OF NUMBER 1 SLAT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND WEB CRACKED AT FLOOR LEVEL FWD OF BELT FRAME AT BS 639.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED ON INNER RADIUS OF FWD SIDE, JUST UNDER LOCK HOOK ASSY.  REPAIRED PER SWA RA 1-A52-198.


REMARKS:
LAS - FLT 90 - EN ROUTE LAX TO PHL, THE RIGHT ENGINE BEGAN TO STEADILY LOSE OIL.  THE CREW DECIDED TO DIVERT TO LAS.  FLIGHT LANDED WITHOUT INCIDENT.  ENGINE WAS NOT  SHUTDOWN.  MAINTENANCE FOUND A PIN HOLE IN THE CHIP DETECTOR OIL SCAVENGE TUBE NEAR THE FUEL/OIL COOLER.  THE TUBE WAS REPLACED.  LEAK CHECKED GOOD.  (Z)


REMARKS:
PHL - THE EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY PACK.  OPERATIONS CHECKED NORMAL.  (Z)


REMARKS:
PIT - THE PORTABLE EMERGENCY LIGHT AT THE MAIN ENTRANCE DOOR WAS BROKEN.  MAINTENANCE REPLACED THE PORTABLE EMERGENCY LIGHT FWD GALLEY.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
CLT - THE COCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE.  MAINTENANCE REPLACED THE BATTERIES ON THE COCKPIT EMERGENCY LIGHT POWER SUPPLY.  OPERATIONS CHECKED GOOD.  (Z)


REMARKS:
PIT - THE CENTER WINDSHIELD CENTER PANE CRACKED EN ROUTE TO DTW.  FLIGHT DIVERTED TO PIT.  MAINTENANCE REPLACED THE CENTER WINDOW.  (Z)


REMARKS:
MCI - DURING OP-17, FOUND CORROSION AND 20 INCH CRACK IN STRINGER 29R, STATION 950 TO 960F.  REPAIRED PER ARA 9145.  TOTAL CYCLES 24,387.


REMARKS:
MCI - DURING OP-17, FOUND CORROSION ON FUSELAGE SKIN, STATION 720 TO STATION 724, FROM FOUR INCHES LBL TO FOUR INCHES RBL.  INSTALLED SKIN DOUBLER PER SRM 53-30-3, FIGURE 1.  TOTAL CYCLES 24,387.


REMARKS:
SJU - DURING CRUISE, WINDSHIELD HEAT WIRE HARNESS SHORTED AT R-2 WINDOW CAUSING ARCING AND SMOKE IN COCKPIT.  TURNED OFF WINDSHIELD HEAT AND DISCHARGED HAND EXTINGUISHER.  REPLACED WINDSHIELD WIRING HARNESS AND WINDSHIELD HEAT CONTROLLER MFG, P/N 27261298-02.  WINDSHIELD HEAT OPERATION CHECKED NORMAL.


REMARKS:
JFK - DURING CRUISE, NR 1 NACELLE FIRE DETECTOR FAULT LIGHT ILLUMINATED WITH TEMPERATURES IN THE FAULT RANGE.  THE NR 1ENGINE FIREWARNING SOUNDED.  SHUT DOWN NR 1 ENGINE AND DISCHARGED BOTH EXTINGUISHER BOTTLES.  FOUND BOTH DETECTORS SHORTED.  REPLACED BOTH DETECTORS, MFG P/N 60B00023-163 AND P/N 60B00023-166.  PERFORMED POWER RUNUP AND NACELLED DETECTOR FAULT AND FIREWARNING SYSTEMS CHECKED NORMAL.


REMARKS:
MCI - DURING C-CHECK, FOUND TWO INCH CRACK IN INBOARD AFT SIDE OF FRAME, BELOW FLOOR LEVEL, FS 783.95.  STOP DRILLED CRACK AND INSTALLED REPAIR PER EMLR 65661.  TOTAL CYCLES 42,060.


REMARKS:
MCI - DURING C-CHECK, FOUND .5 INCH CRACK IN PRESSURE DECK EIGHT INCHES INBOARD OF 940 CASTING.  STOP DRILLED AND INSTALLED DOUBLER PER ARA 9130.  TOTAL CYCLES 42,060.


REMARKS:
MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 250, LOWER AFT RADIUS OF R3 COCKPIT WINDOW.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132.  TOTAL CYCLES 42,060.


REMARKS:
MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 252, AFT RADIUS OF R3 COCKPIT WINDOW.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132.  TOTAL CYCLES 42,060.


REMARKS:
SNN - MADE UNSCHEDULED LANDING ACCOUNT NR 1 ENGINE 'A' FIREWARNING ILLUMINATED.  SHUT DOWN ENGINE AND DISCHARGED EXTINGUISHER BOTTLERS.  'B' LOOP PREVIOUSLY PLACARDED ON MEL.  RESTORED 'B' LOOP BY REPLACEMENT OF LOWER AFT WARNING LOOP, MFGP/N 895398.  REPLACED EXPENDED BOTTLES AND PLACARDED 'A' LOOP PER MEL.  OPS CHECKS NORMAL.


REMARKS:
MCI - DURING OP-17 FOUND A SIX INCH LONG CRACK IN AFT CARGO BIN, STRINGER 29L, FS 1000.  REPAIRED PER ARA 9054.  TOTAL CYCLES 22,210.


REMARKS:
MCI - DURING OP-17, FOUND CORROSION IN AFT CARGO BIN, ON LEG OF STRINGER 29L, AROUND TWO HI-LOCKS, FS 990.  REPAIRED PER ARA 9054.  TOTAL CYCLES 22,210.


REMARKS:
AFTER TAKEOFF, EXPERIENCED NR 2 ENGINE POWER FLUCTUATION AT ALL SETTINGS.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  REPLACED NR 2 ENGINE FUEL CONTROL UNIT PER BOEING M/M.


REMARKS:
AT GATE, FOUND EMERGENCY LIGHT STRIP LOOSE AT ROW 8 AND LIGHTS DIM DURING TESTING.  REPLACED BATTERY PACK AT FWD CABIN AREA PER BOEING M/M.


REMARKS:
MCI - MADE UNSCHEDULED LANDING ON ACCOUNT THAT THE LEFT ENGINE SHUT DOWN DUE TO POWER LOSS.  FOUND METAL IN TAIL PIPE.REPLACED ENGINE S/N 3214.  INVESTIGATION INTO LEFT ENGINE SHUT DOWN DUE TO LOSS OF POWER REVEALED NR 3 BEARING MFG P/N 739483 FAILED, DISENGAGING ACCESSORY GEARBOX DRIVE.  ENGINE S/N 3214 WAS REPAIRED AND RETURNED TO SERVICE.  ENGINE TOTALTIME 32,672.  ENGINE TOTAL TIME 17,193.  (W)


REMARKS:
FLL/ATL - FLT 128 - EXPERIENCED AN ELECTRICAL MALFUNCTION WHEN THE RIGHT GENERATOR DROPPED OFF-LINE AFTER THE AIRCRAFT STARTED ITS ROLL FOR TAKEOFF.  PILOT POWERED BACK AND PROCEEDED BACK TO THE GATE.  CREW RESET CIRCUIT BREAKERS AND GENERATOR RESET TO NORMAL OPERATING LEVELS.


REMARKS:
STL - DURING C-CHECK, CORROSION ON AFT CARGO BIN LOWER DOOR JAMB INNER PANEL, FROM FORWARD LOWER CORNER TO AFT SIDE.  REPAIRED PER SRM 53-05, FIGURE 14.


REMARKS:
MCI - DURING C-CHECK, FOUND A .25 INCH CRACK IN PRESSURE DECK OUTBOARD END, STATION 940.  STOP DRILLED CRACK AND REPAIRED PER ARA 9117A.  TOTAL CYCLES 45,150.


REMARKS:
MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 249, AFT RADIUS OF R3 COCKPIT WINDOW.  STOP DRILLED CRACKED AND INSTALLED DOUBLER PER ARA 9132.  TOTAL CYCLES 42,060.


REMARKS:
CLT - FIRST CLASS LOW LEVEL LIGHTING STRIP CRACKED.  MAINTENANCE REPLACED LIGHTING TRACK.  (W)


REMARKS:
CLT - FLT 2126 - FLIGHT EN ROUTE BWI TO ATL WHEN 'A' SYSTEM HYDRAULICS FAILED.  CREW DIVERTED FLIGHT TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 ENGNE HYDRAULIC PUMP.  REPLACED 'A' SYSTEM RETURN AND BOTH CASE DRAIN FILTERS.  NO LEAKS NOTED.  (W)


REMARKS:
BOS - FLT 2176 - NR 2 ENGINE OVERHEAT CAME ON DURING CLIMB-OUT.  RETARDED THROTTLE, LIGHT WENT OUT.  FLIGHT RETURNED TOBOS WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND RIGHT ENGINE COWL ANTI-ICE SUPPLY DUCT BLOWN BETWEENCROSS OVER DUCT AND COWL ANTI-ICE VALVE.  REPLACED ANTI-ICE DUCT.  RUN UP AND LEAK CHECK OK.  (W)


REMARKS:
PIT - FLT 1669 - AFTER TAKEOFF FROM PHL EN ROUTE TO LAS, NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY NR 1 ENGINE GENERATOR DROPPING OFF LINE.  CREW DISCONNECTED NR 1 CSD AND DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT ENGINE CSD.  GROUND OPS CHECKS NORMAL.


REMARKS:
CLT - COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE.  MAINTENANCE RELEASED ON MEL 33-15A.  REPLACED BATTERY PACK AND REMOVEDMEL.  OPS CHECKED OK.  (W)


REMARKS:
PIT - EMERGENCY EXIT LIGHT AT EXIT ROW INOPERATIVE.  MAINTENANCE REPLACED EMERGENCY EXIT LIGHT AT EXIT ROW.  OPS CHECKSNORMAL.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 34 INCHES CORROSION AREA AT NUT PLATE HOLES ON BS 328 FLOORBEAM CAP, BS 328 RBL 2 TO RBL 36.  REPAIRED PER TR 53-10-3.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 524, BETWEEN S15 AND 16L, AT BS 360 TO 420, BETWEEN S21 AND 22R, AT BS 998, BETWEEN S22 AND 23L, AT BS 931, BELOW S21R, AT BS 346, S24R, AT BS 345-360, BETWEEN S21 AND 22R, AT BS 877, S26R, AT BS 260 TO 280, BETWEEN S23 AND 24R, AT BS 967, AT S20L, AND AT BS 184, AT WL 182, RBL 22.  REPAIRED ALL PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 380, S22L AND 21L, AT BS 787, S24R, AT BS 616, S5R AND L, AT BS 360, AT S4 AND 5L, AT BS 807, S15L, AT BS 787, S15L, AT BS 887, S15L, AT BS 520, S19L, AT BS 706, S11R,  AT BS 500B, S19L, AND AT BS 807, S16L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND OUTBOARD FLANGE OF SHEAR TIE ABOVE S16R CRACKED AT LOWER FASTENER AND IN RADIUS.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR REPAIR DOUBLER NEEDING REWORK.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND RIB UPPER FLANGE CRACKED AT LEFT WING STA 453 AT FWD STRINGER ATTACH.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND TOOLING MARKS ON STRINGER AND SKIN DOUBLER AT BS 727B AND S7R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, S16L AND FRAME SHEAR TIE CRACKED AT BS 460, RBL 6.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 295-311, S4L, AND AT BS 178 TO 188, LBL 26, WL 195.  REPLACEDPER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER GOUGED AT BS 864,  S15L, AND AT BS 928 TO 935, S14R, STRINGER CRACKED AT BS 1140, 12L, AT BS 787, S10R, AT BS 1016, S7L, AT BS 907, AT S4R AND L, AT BS 467, AT S22L, STRINGER CORRODED AT BS 1138, S13L, AND AT BS 520 TO 528, WL 216, LBL 65, AT BS 897-907, S20R, AND STRINGER CHANNEL CRACKED AT BS 360, S11L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND Z-ANGLE CORRODED AT BS  270, WL 208, LBL 10 RBL 10.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 312 TO 344, LBL 60, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FAILSAFE CHORD CRACKED AT BS 947, WL 175, LBL 4.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY MOPSILL CORRODED AT BS 312 TO 344, LBL 61, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY VERTICAL FLANGE ON MOPSILL CORRODED AT BS 312, LBL 61, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME LOWER CHORD CRACKED AT BS 202, RBL 2 TO 6, WL 165.  ALS, FRAME CRACKED AT BS 1104, 1 INCH ABOVE S5L.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 5, RBL 14.5, RBL 20.5, RBL 26, RBL 31, WL 207 AND 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 45 TO 63, WL 208.  REPAIRED PER TRAMCO EWO 95-0258.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 987.5, WL 208 AND WL 207, RBL 44.5 AND LBL 43.5.  REPAIRED PERSWA RA 1-253-465.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 616, LBL 65, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME DOUBLER STRAP CRACKED AT BS 1155, WL 303, RBL 24.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT FASTENER HOLES AT S3L, 2L, 1L, 2R AND 3R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 1138, S13L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED BETWEEN S13 AND 14L, BS 727.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, S14L.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR WEB CRACKED AT L/E STA 128.  REPAIRED PER BOEINGSTRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CRACKS AND HOLES AT BS 727 PLUS 18, LBL 6.5 AND 7.7, WL 149, I/B AND O/BFLANGES.  REPAIRED PER TRAMCO EWO 95-0274 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CORRODED UNDER SKIN AT BS 727 PLUS 7, WL 149, RBL 7.  REPAIRED PER TRAMCO EWO 95-0260 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND RIGHT KEEL BEAM INBOARD FLANGE CORRODED AT BS 727 PLUS 13.3, AND OUTBOARD FLANGE AT BS 727 PLUS 17.2, RBL 7.5.  REPAIRED PER TRAMCO EWO 95-0260 AND BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LAVATORY WALL SUPPORTS CORRODED AT BS 992.5, LBL 15, 20, 27, AND 43, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN LIGHTNING STRIKE DAMAGE FROM BS 440 TO 500, BETWEEN S2 AND  4R.REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LAVATORY WALL SUPPORTS CORRODED AT BS 956, LBL 27 AND 38, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 806, BETWEEN S25 AND 26R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663.7, S10L AND R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR SUPPORT CORRODED FROM BS 1007 TO 1016, LBL 0, WL 208.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CHORD CORROSION AT BS 1006, LBL 12, WL 208.  REPAIRED PER TRAMCO EWO95-0327.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM HAS A HOLE IN RADIUS AFT SIDE, BS 807, LBL 47.5, WL 208.  REPAIRED PER TRAMCO EWO 95-0318.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FWD CARGO DOOR SILL WEB CORRODED AT NUTPLATE HOLES AT BS 440 TO 490, WL 156, RBL 29.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM NUTPLATE HOLES CORRODED AT BS 344, BL 0, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND UPPER DRAG ANGLE CRACKED AT BS 536, WL 172, BETWEEN S21 AND 22R.  REPAIRED  PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION ON FLOOR BEAM AT SCREW HOLES 30 PERCENT LOSS, BS 727 TO BS 740 RBL 13.  REPAIRED PER SRM 53-00-53 FIG 202.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 3 INCH CORROSION 30 PERCENT LOSS, BS 986.5 TO BS 1006, ANGLE AT LEFT AFT BLUE ROOM 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 2 INCH BY 4 INCH SPOT, 3 INCH BY 6 INCH SPOT, 10 INCHES BY 12 INCHES SPOTS OF CORROSION TASK NR C53-107-02, CORRSOSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, ON T-CAP AT BS 986.5.  REPAIRED PER TR 53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON HAT CHANNEL BS 996 RBL 18 INCHES TO DOOR FRAME.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-0, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORRODED AREA ON INTERCOSTAL AT BS 957 RBL 18 INCHESTO RBL 45 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 2 INCHES BY 40 INCHES CORRODED AREA, AFT SERVICE DOOR.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT BS 947 TO BS 967 RBL 45 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 SEVERAL 1 INCH BY 1 INCH NUTPLATE HOLES CORRODED, BS 967 RBL 0 TO RBL 50 INCHES.  REPAIRED PER SRM 53-00-51, FIG 202.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND 16 INCH BY 8 INCH AREA OF SPOTS CORROSION ON DOOR SILL WEB SKIN, BS 804 AT AFT CARGO DOOR SILL AREA.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION THE ENTIRE LENGTH OF BEAM 25 PERCENT TO 40 PERCENT LOSS, BS 1016 LEFT END TO RIGHT END.  REPAIRED PER SRM 53-00-51 FIG 202.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL, BS 967 - BS 987 RBL 22 INCH.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-0.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH BY 30 PERCENT LOSS OF METAL, BS 947 TO 967 RBL 24.  REPAIRED PER SRM 51-10-2.  CORRSOSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (W)


REMARKS:
FCO - DURING PERIODIC CHECK, FOUND A NINE INCH CRACK IN RT WING FRONT SPAR AT FSSI 675.5.  REPAIRED CRACK PER BOEING REPAIR DRAWING 691U0103 AND TWA ARA 9122.  TOTAL CYCLES 17,425.  (Z)


REMARKS:
MCI - DURING CHECK-C, FOUND A ONE-INCH LONG CRACK IN STRINGER 16, STA 656.5.  REPAIRED PER SRM 57-20-201 FIG 207.  TOTAL CYCLES 45,150.  (Z)


REMARKS:
MCI - DURING CHECK-C, FOUND A ONE INCH CRACK IN FUSELAGE FRAME, FS 783.95.  REPAIRED PER SERVICE BULLETIN 727-53-0197, DRAWING NR 65C36280 AND EMLR 65639.  TOTAL CYCLES 45,150.  (Z)


REMARKS:
CLT - FLT 1175 - FLIGHT DEVELOPED LEADING EDGE SLAT ASYMMETRY PROBELMS AFTER TAKEOFF AND RETURNED TO CLT.  A SECOND ATTEMPT WAS MADE TO DEPART CLT AND THE FLIGHT AGAIN EXPERIENCED SLAT ASYMMETRY PROBLEMS.  FLIGHT RETURNED TO CLT AGAIN.  MAINTENANCE PERFORMED BITE TEST AND RESET THE PROXIMITY SENSOR AFTER THE FIRST RETURN TO FIELD.  ALL BITES AND RESETS CHECKED GOOD.  AFTER THE SECOND RETURN TO FIELD, MAINTENANCE FOUND THE OUTBOARD LEADING EDGE ACTIVATING ROD ON THE NR 7 SLATFAILED.  THE ROD WAS REPLACED.  OPERATIONS CHECKED GOOD.  NO DEFECTS NOTED.  (W)


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOORWAY LOWER MOP SILL CORRODED FROM BS 942 TO 986.5, WL 208, LBL 60.  REPLACED PER BOEING SRM.


REMARKS:
CLT - FLT NR 0275 - CREW REPORTED FUMES IN COCKPIT.  OXYGEN MASKS WERE USED AND AN EMERGENCY WAS DECLARED.  MAINTENANCECLEANED THE ANTI-ICE FLUID LINE AND ELBOW AT SOLENOID, FIRST OFFICERS SIDES.  OPERATIONS CHECKED GOOD.  (W)


REMARKS:
RIC - FLT 0739 - AT FL 350, THE CABIN PRESSURE RED LIGHT AND MASTER WARNING LIGHT ILLUMINATED.  CREW DECLARED AN EMERGENCY AND DIVERTED TO TIC.  MAINTENANCE INSTALLED THE OUTFLOW ACTUATOR AND PRESSURE AMPLIFIER.  OPERATIONS CHECKED NORMAL. REF CONTROL NR. 95ZZZX2328.  (X)


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND 14 LIGHTNING STRIKE DAMAGE AREAS TO FUSELAGE SKIN FROM BS 747 TO 827, BETWEEN S2 AND 3R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND AFT GALLEY DOORWAY UPPER FORWARD FRAME SECTION CRACKED AT BS957, WL 260, RBL 60.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED FROM BS 947 TO 967, LBL 41, WL 208.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND THRESHOLD TIE STRAP CORRODED FROM BS 787 TO 847, RBL 21, WL 154.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL WEB CORROSION FROM BS 328 TO 344, RBL 27, WL 208.1.  REPAIRED  PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND 11 LIGHTNING STRIKE DAMAGE AREAS TO FUSELAGE SKIN AT BS 500 TO 500D, BETWEEN S2 AND 4R.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
RIC - FLT 0739 - AT FL 350, THE CABIN PRESSURE RED LIGHT AND MASTER WARNING LIGHT ILLUMINATED.  CREW DECLARED AN EMERGENCY AND DIVERTED TO TIC.  MAINTENANCE INSTALLED THE OUTFLOW ACTUATOR AND PRESSURE AMPLIFIER.  OPERATIONS CHECKED NORMAL. REF CONTROL NR. USAA950369.


REMARKS:
CLT - THE EMERGENCY EXIT LIGHTS REMAIN ON WITH ALL POWER REMOVED FROM THE AIRCRAFT AND THE EMERGENCY EXIT LIGHT SWITCH 'OFF'.  MAINTENANCE RPELACED BATTERY POWER SUPPLY.  OPERATIONS CHECK GOOD.  (X)


REMARKS:
CLT - FLT 0052 - FLIGHT RETURNED TO CLT DUE TO A FUEL IMBALANCE.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPAIREDA CONNECTOR IN THE WHEELWELL AND SEVERAL FLAG TERMINALS ON THE PROBES.  (X)


REMARKS:
CLE - MAIN ENTRANCE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE.  MAINTENANCE REPLACED BATTERY PACK.  OPS CHECKS GOOD.  (X)


REMARKS:
PIT - RIGHT OVERWING EMERGENCY LIGHT LENS MISSING AND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE.  MAINTENANCE REPLACED LENS ON RIGHT SIDE AND REPLAMPED LEFT SIDE.  BOTH OPS CHECK OKAY.  (X)


REMARKS:
CLT - FLT 993 - AFTER TAKEOFF FROM TYS, RIGHT MLG RED LIGHT REMAINED ON AFTER GEAR RETRACTION.  CREW RECYCLED GEAR AND LIGHT WENT OUT.  FLIGHT CONTINUED WITHOUT INCIDENT TO CLT.  MAINTENANCE FOUND RIGHT MAIN GEAR HARNESS CONTACTING AFT DOOR HOOK BEFORE DOOR COULD LOCK.  RESECURED LOWER HARNESS TO STRUT.  (X)


REMARKS:
MCI - DURING C-CHECK, FOUND FORMER FRAME CRACKED 2 INCHES AROUND RADIUS, 3 INCHES ABOVE FLOOR BEAM CAP, STA 783.  STOP DRILLED CRACK PER SRM 51-10-4, PAGE 6A, AND INSTALLED DOUBLER REPAIR PER ARA 65686 AND DWG. NR 65C36280.  AIRCRAFT TT:  61,023 HOURS; 41,008 CYCLES.


REMARKS:
STL - FLT 572 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR SHOWED AN UNSAFE INDICATION.  VISUALLY CHECKED NLG FOR BEING DOWN AND LOCKED.  FOUND BROKEN WIRE AT NLG DOWLOCK SWITCH CONNECTOR, D298.  REPLACED D298 DOWNLOCK SWITCH CONNECTOR.  NLG OPERATION AND INDICATION CHECKED NORMAL.  CHECK C-2 - 9-7-94 - MCI.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A .50 INCH CRACK IN LONGERON 3L, STA 794 AND STA 832.  REPAIRED PER SRM 53-02, FIGURE2.  AIRCRAFT TOTAL TIME:  39,023 HOURS; 48,633 CYCLES.


REMARKS:
STL - DURING OP-15, FOUND A GOUGE IN LONGERON 6R, STA 1000.  REPAIRED BY INSTALLING LONGERON SPLICE PER SRM 53-02.  AIRCRAFT TOTAL TIME:  62,133 HOURS; 75,010 CYCLES.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND .50 INCH CRACK IN LONGERON 3R, STA 734.  REPAIRED PER SRM 53-02, FIGURE 2.  AIRCRAFT TOTAL TIME:  39,023 HOURS; 48,633 CYCLES.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STA 832.  REPAIRED PER SRM 53-02, FIGURE 2.  AIRCRAFT TOTAL TIME:  39,023 HOURS; 48,633 CYCLES.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND CRACK IN LONGERON 4L, STA 832.  REPAIRED PER SRM 53-02, FIGURE 2.  AIRCRAFT TOTAL TIME:  39,023 HOURS; 48,633 CYCLES.


REMARKS:
STL - FLT 10 - AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE ABOVE OFF POSITION.  ACCOMPLISHED LANDING GEAR HANDLELOCK CHECKLIST AND RETRACTED LANDING GEAR.  FOUND NLG TORQUE LINK PIN MISSING, MFG. PN 53173.  INSTALLED NEW NOSE GEAR TORQUE LINK PIN.  LANDING GEAR CHECKS NORMAL.  CHECK C-3 - 3-24-95 - MCI.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN LONGERON 4L, STA 794.  REPAIRED PER SRM 53-02, FIGURE 2.  AIRCRAFT TOTAL TIME:  39,023 HOURS; 48,633 CYCLES.


REMARKS:
LAX - FLT 841 - ON APPROACH, NR 1 ENGINE SHUT DOWN ON OWN ACCORD.  REPLACED FUEL PUMP, MFG PN 373401-26 AND JFC, MFG PN747999-5.  OP CHECKS NORMAL.  CHECK C-2 - 1-29-95 - MCI.


REMARKS:
STL - FLT 147 - AFTER LANDING GEAR RETRACTION, RIGHT DOOR AND GEAR UNSAFE LIGHT ILLUMINATED DURING UPLATCH CHECK.  RECYCLED GEAR WITH SAME RESULTS.  REPLACED DOOR LATCH BRACKET, MFG PN 4956737-1, AND SPRINGS, MFG PN 2923594-1.  OP CHECKS NORMAL.  CHECK C - 5-2-94 - STL.


REMARKS:
LAX - FLT 841 - DURING APPROACH, NR 1 ENGINE, SN 4162, SPUN DOWN.  SHUT DOWN ENGINE.  REPLACED NR 1 ENGINE FUEL PUMP, MFG PN 373401-26, AND FUEL CONTROL, MFG PN 747999-5.  ENGINE GROUND RUN UP OPERATION CHECKED NORMAL.  CHECK C-2 - 1-29-95- MCI.


REMARKS:
PHX - FLT 730 - ON TAKEOFF FOLLOWING A SHARP IMPACT ON FUSELAGE FROM RIGHT NOSE TIRE TREAD FAILURE, BOTH COMPASSES, FLIGHT DIRECTORS, AND ATTITUDE DIRECTOR INDICATORS FAILED.  AFTER LANDING, REMOVED AND RE-ESTABLISHED POWER TO ATTITUDE ANDHEADING REFERENCE SYSTEMS.  ALIGNMENT OF BOTH SYSTEMS WAS NORMAL AND SYSTEMS OPERATIONAL CHECK WAS NORMAL.  CHECK C-1D - 4-6-95 - MCI.


REMARKS:
MCO - FLT NR 74, AFTER TAKEOFF, NR 1 GEN UNDEREXCITED, ISOLATED GEN LEFT FWD BOOST PUMP CIRCUIT BREAKER POP IN NR 2 TANK, RESET, FORWARD RT BOOST PUMP CIRCUIT BREAKER POPPED, LEFT NR 2 CIRCUIT BREAKER POPPED AGAIN, NR 1 CIRCUIT BREAKER LEFT TANK BOOST PUMP POPPED.  AIRCRAFT RETURNED TO MCO.  FOUND T1 WIRE BROKEN AT NR 1 GEN, REPAIRED T1 WIRE PER 24-50, OPS CHECK OK.  (W)


REMARKS:
DURING C-CHECK AND C.P.C.P. INPSECTION, FOUND FLOOR BEAM AT BS 1070 BESIDE R2 DOOR CORRODED.  REMOVED CORRODED SECTION OF UPPER CHORD.  FABRIATED REPAIR SECTIONS IAW SRM 53-10-8 USING PN BAC 1490-2785, BAC 1490-2831, AND BAC 1505-100617 MATERIAL.  TREATED AND PRIMED IAW SRM 51-10-2.  INSTALLED REPAIR SECTION IAW SRM 53-10-8 AND SRM 51-30-2.


REMARKS:
DURING C-CHECK AN C.P.C.P. INSPECTION, FOUND BS 1323 SKIN CRACKED AT LOWER FORWARD CORNER OF CUT-OUT FOR THE LT NEG. RELIEF DOOR.  (1.33 INCH IN LENGTH.)  STOP DRILLED IAW SRM 51-10-1, PAGE 65, PARAGRAPH C.  FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIGURE 1, SHEET NR 4, TREATED AND PRIMED IAW SRM 51-10-2.  INSTALLED DOUBLER IAW SRM 51-30-2, FIGURE NR 1.  SEALED PER SRM 51-20-4, (DOUBLER MATERIAL, 7075-T6, .063 INCH, LOT NR 393421).


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND VERTICAL STIFFENER ON FORWARD SIDE OF BS 1183 BULKHEAD AT RBL 24 HAS CRACKED WEBBING APPROXIMATELY 5 FEET ABOVE FLOOR LEVEL.  FABRICATED REPAIR SECTIONS IAW SB 727-53-0182.  TREATED AND PRIMED PER SRM 51-10-2.  INSTALLED REPAIR CHANNEL PN 65-33556-48 IAW DWG 69-33556 (BOEING) AND SB 727-53-0182, TUP II.


REMARKS:
DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK CORRODED AT RBL 42 FROM FS 1010 TO BS 1030.  REMOVED CORRODED SECTION.  ALSO, NR 4 SEAT TRACK AT BS 480 CORRODED.  CUT OUT DAMAGED SECTION.  FABRICATED REPLACEMENT TRACK SECTIONS OUTOF BAC 1520-1430 7178-76511 EXTRUSTION IAW SRM 51-30-2.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND UPPER FLANGE OF VERTICAL SUPPORT WEB CORRODED AT BS 822 AND AT 860, RBL22, WL 154.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FAILSAFE CHORD CORRODED AT BS 847, BL 0, WL 148.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND 12 FUSELAGE SKIN DENT AT BS 300 TO 312, S20R.  INSTALLED REPAIR PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE GOUGED AT BS 727D, BETWEEN S19 TO 20R.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING CLIMBOUT, FLAPS REMAINED AT FIVE DEGREES.  AIRCRAFT RETURNED TO SLC AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND RIGHT FLAP POSITION TRANSMITTER CANNON PLUG CORRODED.  CLEANED PLUG AND OPERATED FLAPS THROUGH ALL SETTINGS, OKPER BOEING MAINTENANCE MANUAL.


REMARKS:
AFTER TAKEOFF, FLAPS WOULD NOT RETRACT PAST 5 DEGREES, EXTENDED FLAPS NORMALLY.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACED FLAP POSITION INDICATOR PER BOEING MAINTENANCE MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER END AT BS 294.5.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED IN FWD FLANGE RADIUS, BS 520, LBL 45.5.  REPAIRED PERBOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY DOORWAY WEB CRACKED BELOW DOOR ASSIST HANDLE.  REPAIRED PER SWA ACO 471-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT SCANNING LIGHT CUTOUT, BS 500B AT S16L AND AT BS 500B PLUS13.5.  REPAIRED PER SWA ACO 6405-53.


REMARKS:
FOUND PRESSURE BULKHEAD CRACKED AT BS 727, AFT WALL OF WHEEL WELL.  REPAIRED PER SWA RA 253-1194.


REMARKS:
DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, WL 160, RBL 24.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
YOW - FLT 0810 - CREW COULD NOT GET THE GREEN LIGHTS FOR THE RIGHT MAIN GEAR.  THE CREW HAD TO RECYCLE THE GEAR SEVERALTIMES TO GET THE GREEN LIGHTS.  FLIGHT MADE A NORMAL LANDING.  MAINTENANCE REPLACED THE RIGHT DOWNLOCK ACTUATOR.  LANDING CHECKS NORMAL.  (M)


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN AT AFT GALLEY DOOR HINGE CUTOUT, CRACKED .375 AT TOP CORNER.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY DOORWAY WEB FWD OF DOOR CRACKED BELOW DOOR ASSIST HANDLE.  REPAIRED PER SWA ACO 471-53.


REMARKS:
AT 17,000, NUMBER 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED.  CREW PERFORMED NUMBER 1 ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT LANDED AT IND WITHOUT INCIDENT.  REPLACED ENGINE STARTER, START VALVE, STARTER CUTOUT PRESSURE SWITCH AND COCKPIT START SWITCH PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND LEFT FWD FUSELAGE SKIN CRACKED AT AIRSTAIR DOOR HANDLE CUTOUT, AFT END.  REPAIRED PER SWA ACO 485-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY WEB CORRODED BETWEEN BS 986 AND 1006, RBL 46, LOWER SURFACE.  REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOORWAY WEB CRACKED AT LOWER AFT END.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT S20L, BETWEEN BS 178 AND 188, AT FWD END OF 178 BULKHEAD.  REPAIRED PER TYPICAL REPAIR BULLETIN T1-A53-025.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT S20R, BETWEEN BS 178 AND 188, AT FWD END OF 178 BULKHEAD.  REPAIRED PER TYPICAL REPAIR BULLETIN T1-A53-025.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR  SUPPORT HAT SECTION CRACKED AT BS 540, LBL 46.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND S27L CORRODED FROM BS 947.5 TO 970.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT LOWER LOBE AT BS 1006 BELTFRAME SHEAR TIE AFT LEG CORRODED FROM BL 0 TO LBL 3.REPLACED SHEAR TIE PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT UPPER CHORD FWD FLANGE RADIUS.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT CENTER CABIN STRINGER S16R END FWD OF SCANNING LIGHT CUTOUT CRACKED AT BS 500B PLUS 2.5 AND AT 13.5.  REPAIRED PER SWA ACO 6405-53.


REMARKS:
IND - DURING CD-2 INSPECTION, FOUND CORROSION ON AFT SIDE OF FORWARD DOOR STOP FITTING IN LOWER SILL PAN.  CUT OUT CORRODED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 44 AND USAIR EA 29986.  (M)


REMARKS:
PIT - DURING SCHEDULED SIP VISIT, FOUND 1.5 INCH CRACK IN REAR PRESSURE BULKHEAD STATION 17065 HORIZONTAL BEAM NR 3 AT BL 425 RT HIGH FREQUENCY EDDY CURRENT INSPECTION SIP REF 53-10-03.  STOP DRILLED CRACK AND INSTALLED ANGLE AND DOUBLER REPAIR PER USAIR EA 30104.


REMARKS:
PIT - DURING SCHEDULED SIP VISIT, FOUND .5 INCH CRACK SERVICE EMERGENCY DOOR APERTURE AFT LOWER CORNER EDDY CURRENT INSPECTION REF SIP 53-10-20.  ACCOMPLISHED SHEET METAL REPAIR PER SRM 53-02-16 PG 7, 8 AND 11.  (M)


REMARKS:
PIT - DURING SCHEDULED SIP VISIT, FOUND .25 INCH CRACK 2 EACH FUSELAGE SKIN JUST FORWARD OF RT CORNER NOSE WHEEL WELL CUTOUT, EDDY CURRENT INSPECTION SIP REF 53-10-24.  INSTALLED REPAIR PER SRM 53-02-18 FIG 10.  (M)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED LEFT INBOARD SEAT TRACK STATION 197-237. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F.  (M)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH SKIN CRACK AT RIVET HEAD STATION 347 BETWEEN LONGERON 23L AND 24L.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND DENT OUT OF LIMITS JUST AFT OF NOSE JACK PAD STATION 218 LONGERON 30.  INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 EFG.  (M)


REMARKS:
PIT - DURING Q-3 INSPECTION, FOUND TEMPORARY REPAIR INSTALLED RT AFT NOSE GEAR DOOR HINGE.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-09.  (M)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT BOLT HOLE AT REAR SPAR KEEP FITTING STATION 691 LEFT WHEEL WELL.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11.  (M)


REMARKS:
PIT - DURING Q-3 CHECK INSPECTION, FOUND TEMPORARY REPAIR INSTALLED STATION 229 LONGERON 17L TO LONGERON 18L.  INSTALLED FLUSH REPAIR PER SRM 53-04 FIG 47.  (M)


REMARKS:
MIA - FLT 1798 - AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR RED LIGHT ILLUMINATED AFTER GEAR RETRACTION.  THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED.  MAINTENANCE LUBRICATED THE LINKAGES AT THE LEFT DOOR LOCK MECHANISM AND ADJUSTEDTHE RIGHT GEAR DOOR LOCK MECHANISM AND SWITCHES.  GEAR INDICATION SYSTEM CHECKS NORMAL.  (M)


REMARKS:
CLT - FLT 1727 - THE FORWARD ENTRY DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY LIGHT ASSEMBLY.  (M)


REMARKS:
BOS - FLT 2493 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.  MAINTENANCE REPLACED THE FORWARD EMERGENCYLIGHT BATTERY PACK.  LIGHTS OPERATED NORMALLY.  (M)


REMARKS:
BDL - FLT 2074 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF.  CREW RECYCLED GEAR AND NOSE GEAR STILL WOULD NOT RETRACT.FLIGHT RETURNED TO BDL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND NOSE GEAR RETRACT PIN INSTALLED.REMOVED AND INSTALLED IN FLIGHT DECK.  OK FOR SERVICE.  (M)


REMARKS:
MCO - FLT 0244 - AFTER TAKEOFF, THE CAPTAIN RECEIVED A FLAP DISAGREEMENT LIGHT.  THE FLAPS WERE RECYCLED BUT THE INDICATAION STILL REMAINED.  MAINTENANCE REPLACED THE FLAP LEVER RVDT.  ALL TEST CHECKED GOOD.  (M)


REMARKS:
PIT - FLIGHT NR 0403 - ON CLIMB-OUT, A CRACK DEVELOPED  IN THE CAPTAINS WINDSHIELD.  FLIGHT RETURNED TO PIT WITHOUT INCIDENT.  (M)


REMARKS:
CLT - FLT 1810 - ON CLIMB-OUT, NR 2 GENERATOR TRIPPED.  APU WAS ON MEL.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE GENERATOR AND NR 2 ENGINE CSD.  OPS CHECK NORMAL.  REFERENCE USAA950457.


REMARKS:
EVV - FLT 1547 - RIGHT FRONT EMERGENCY DOOR EXIT WINDOW NOISY ON CLIMBOUT.  FLIGHT RETURNED TO EVV WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE RESEALED THE WINDOW.  (Z)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION STATION 965-996 ON RT LAV THRESHOLD BEAM REF C58-53300.  MFGTHRESHOLD SKIN AND INSTALLED PER DAC DRAWING 9915532-235.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND TEMP REPAIR STATION 110 JUST ABOVE AFT RT MLG DOOR.  INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .125 INCH CRACK FWD STOP AND .25 INCH CRACK AFT STOP LEFT AFT EMERGENCY EXIT WINDOW.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-20-03.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND GOUGE IN STATION 1076 BELTFRAME LONGERON 20R.  SPLICED IN SECTION OF BELTFRAMEPER SRM 53-03 FIG 32.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND TEMP REPAIR STATION 1096 LONGERON 42.  INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-01 FIG 2.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 16R AT STATION 965 RT LAV.  ACCOMPLISHED LONGERON SPLICE REPAIR PER SRM 53-02 FIG 4.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND A DENT .075 INCH DEEP .75 INCH LONG AT STATION 983 LONGERON 25L AND 24L.  INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-04 FIG 38.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED FINGER DOUBLER FROM STATION 965 TO 996 LONG 26R.  REMOVED AND REPLACED FINGER DOUBLER PER DACO DWG.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL II CORROSION STATION 996 RT LAV FLOORBEAM TOP SIDE, REF C58-53300.  MFG FLOORBEAM AND CAP ANGLE 7075-TL AND INSTALLED PER SRM 53-05 FIG 72.


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL II CORROSION AT STATION 980 LEFT LAV FLOORBEAM, REF C58-53300.  REMOVED CORROSION AND INSTALLED FILLER TYPE REPAIR PER USAIR TYPICAL REPAIR 53-10-19 AND SRM 53-05 FIG 20.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH SKIN CRACK LOWER AFT CORNER FORWARD AIRSTAIR DOOR AREA STATION 200.  INSTALLED EXTERNAL DOUBLER PER SRM 53-05 FIG 57A.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT STATION 980 BELTFRAME LONGERON 17R.  SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-13.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED, REF C46-53302 AT RT OUTBOARD SEAT TRACKSTATION 200 TO 236.  SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT REAR PRESSURE BULKHEAD STATION 996 TOP RIGHT DOOR FRAME AREA.  INSTALLED DOUBLER REPAIR DACO DWG J060088-507.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK AT SUPPORT FITTING AFT SPAR 7 INCHES OUTBOARD OF KEEL BEAM LEFT WHEEL WELL.  INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN STATION 980 BELTFRAME AT HI-LOCK FASTENER LONGERON 16L LEFT LAV AREA.  SPLICED IN NEW SECTION OF BELTFRAME PER SRM 53-03 FIG 32 SHT 2.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND A 2 INCH CRACK AT VERTICAL STAB ATTACH ANGLE RT SIDE AFT END OF DRAG ANGLE.  INSTALLED EXTERNAL DOUBLER PER SRM 53-05 FIG 23 AND 23A.  (M)


REMARKS:
PIT - SCHEDULED PRODUCTION CONTROL ITEM.  FOUND .75 INCH CRACK STATION 995 BETWEEN LONGERSON 15 AND 16 RIGHT SKIN CLIP. SPLICED NEW SECTION OF SKIN CLIP PER SRM 53-03 FIG 6.  (M)


REMARKS:
MCI - FLT NR 1481 - EN ROUTE TO MCI, CAPTAIN RECEIVED A NR 1 SYSTEM LOW PRESSURE WARNING LIGHT.  THE CAPTAIN CONTINUED TO MCI BUT DECLARED AN EMERGENCY.  THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.  (M)


REMARKS:
CLT - FLT NR 2461 - DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT AND THE AIRCRAFT WOULD NOT PRESSURIZE.  THE FLIGHTRETURNED TO CLT.  MAINTENANCE SERVICED THE STRUT, CLEANED THE TARGET AND TIGHTENED THE CANNON PLUG.  THE NOSE GEAR WAS THEN CYCLED.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
PHL - FLT NR 0298 - ON APPROACH, CREW RECEIVED AND APU FIRE INDICATION.  THE APU AUTOMATICALLY SHUTDOWN AND THE BOTTLE FIRED, P/N 33100007.  THERE WERE NO OTHER INDICATIONS OF A FIRE.  MAINTENANCE INSPECTED THE APU FIRE EXIT SYSTEM.  THE FIRE EXTINGUISHER BOTTLE WAS REPLACED.  OPERATIONS CHECKED GOOD.  (M)


REMARKS:
BHM - FLT 1423 - AFTER TAKEOFF, THE CREW HAD NO FEEL ON THE LEFT RUDDER INPUTS.  CAPTAIN DECIDED TO RETURN TO BHM.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND A BROKEN CABLE ON THE TRIM BUNGEE.  THE CABLE WAS REPLACED.  (M)


REMARKS:
CLT - FLT 1810 - ON CLIMB-OUT, NR 2 GENERATOR TRIPPED.  APU WAS ON MEL.  FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 2 ENGINE GENERATOR AND NR 2 ENGINE CSD.  OPS CHECK NORMAL.  REFERENCE 95ZZZM54.


REMARKS:
PHL - FLT 139 - RETURNED FROM FLIGHT ACCOUNT WHEN LANDING GEAR WAS RAISED, NOSE GEAR DOOR DID NOT CLOSE.  FOUND NOSE GEAR STRUT LOW ON NITROGEN CHARGE.  SERVICE TO NORMAL CHARGE.  CHECK C-2D - 3-9-95 - MCI.


REMARKS:
CDG - DURING SECOND SEGMENT CLIMB, WHEN CROSSFEED FROM NR 2 AND NR 3 MAIN FUEL TANKS WAS INITIATED, NR 1 ENGINE SPUN DOWN.  TURN ON ALL BOOST PUMPS.  ENGINE RESTART WAS NORMAL.  NR 2 CROSSFEED VALVE HAD BEEN PREVIOUSLY PLACARDED PER MEDP.USED ALTERNATE CROSSFEED PROCEDURES.  OPERATION WAS NORMAL.


REMARKS:
STL - DURING LANDING, SMOKE AND ELECTRICAL ODOR EMITTED FROM CENTER INSTRUMENT PANEL.  FOUND LEFT ENGINE OIL QUANTITY INDICATOR CONNECTOR SHORTED, MFG P/N 8DJ130KWA1.  REPLACED OIL QUANTITY INDICATOR AND OPERATION CHECKED NORMAL.


REMARKS:
MCI - DURING SHOP TEST, FOUND EVACUATION SLIDE, MFG P/N 7A127512, WOULD NOT MAINTAIN AIR PRESSURE.  FOUND ASPIRATOR VALVE NOT PROPERLY CLOSING.  REPAIRED ASPIRATOR VALVE.  RETEST OF EVACUATION SLIDE OPERATION CHECKED NORMAL.  (W)


REMARKS:
STL - DURING C-CHECK, FOUND .375 INCH CRACK AT TOP PYLON ATTACH ANGLE, STATION 978, LEFT PYLON.  REPAIRED PER SRM 54-04, FIGURE 10, SHEET 2.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND ONE .1875 INCH CRACK IN -85 LOWER LEFT CORNER, STATION 1167.  STOP DRILLED CRACK AND REPAIRED PER SERVICE BULLETIN 137 AND EMLR 65694.  (W)


REMARKS:
DURING SPECIAL CHECK, FOUND A TWO INCH CRACK IN LONGERON 19L, STATION 218.  REPAIRED PER SRM 53-02.


REMARKS:
STL - DURING OP-15, FOUND 12 INCH CRACK IN LEFT PORK CHOP FITTING HORIZONTAL LEG.  REPLACED LEFT PORK CHOP FITTING PER DOUGLAS MM 20-10, 20-14, 20-16 AND PER TWA STANDARD PRACTICES.  (W)


REMARKS:
STL - DURING C-CHECK, FOUND FUSELAGE SKIN BULGE AT STATION 985, LONGERON 24R.  REMOVED LONGERON, CLEANED AREA, REPLACEDLONGERON SERCTION AND END CAP PER SRM 53-02, FIGURE 4.  (W)


REMARKS:
PIT - FLT 19 - AFTER TAKEOFF, AC CABIN PRESSURIZATION BEGAN TO CLIMB.  AUTO CABIN PRESSURE SYSTEM WAS ON MEL, ACFT WAS IN STANDBY MODE.  UNABLE TO CONTROL PRESSURIZATION IN STANDBY AC AND DC MODE.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER.  REF USAA950402.


REMARKS:
PIT - FLT 19 - UNABLE TO CONTROL PRESSURIZATION AFTER TAKEOFF.  FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND MANUAL DC CIRCUIT BREAKER POPPED, RESET C/B.  REPLACED OVERHEAD CONTROL PANEL.  ALL CHECKS NORMAL.  REF USAA950403.


REMARKS:
PBI - FLT 188 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF.  FLIGHT RETURNED TO PBI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND DUCT CLAMP AND SEAL LOOSE ON AFT SIDE OF AFT PRESSURE BULKHEAD.  REINSTALLED CLAMP AND SEAL.  FOUND PACK VALVE ON LEFT PACK NOT OPENING.  REPLACED LEFT PACK VALVE.  REF USAA950404.


REMARKS:
PIT - FLT 19 - AFTER TAKEOFF, AC CABIN PRESSURIZATION BEGAN TO CLIMB.  AUTO CABIN PRESSURE SYSTEM WAS ON MEL, ACFT WAS IN STANDBY MODE.  UNABLE TO CONTROL PRESSURIZATION IN STANDBY AC AND DC MODE.  FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER.  REF 95ZZZZ231.


REMARKS:
PIT - FLT 19 - UNABLE TO CONTROL PRESSURIZATION AFTER TAKEOFF.  FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND MANUAL DC CIRCUIT BREAKER POPPED, RESET C/B.  REPLACED OVERHEAD CONTROL PANEL.  ALL CHECKS NORMAL.  REF 95ZZZZ232.


REMARKS:
PBI - FLT 188 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF.  FLIGHT RETURNED TO PBI WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE FOUND DUCT CLAMP AND SEAL LOOSE ON AFT SIDE OF AFT PRESSURE BULKHEAD.  REINSTALLED CLAMP AND SEAL.  FOUND PACK VALVE ON LEFT PACK NOT OPENING.  REPLACED LEFT PACK VALVE.  REF 95ZZZZ233.


REMARKS:
CLT - LOW LEVEL EMERGENCY EXIT SIGN MISSING, ROW 10AC.  MAINTENANCE REPLACED EXIT SIGN.  (Z)


REMARKS:
CLT - FLT 1157 - CAPTAIN'S FLIGHT INSTRUMENTS, AIRSPEED, ALTIMETER FAILED AND GPWS WARNING CAME ON.  FLIGHT RETURNED TOCLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED NR 1 ADC.  OPS CHECK OK.  PERFORMED OVERWEIGHT LANDING INSPECTION, CHECKS OK.  (Z)


REMARKS:
PIT - FORWARD SECTION OF FLOOR TRACK LIGHTING INOPERATIVE.  MAINTENANCE REPLACED BOTH DIODES IN EMERGENCY CABIN FLOOR LIGHTING SYSTEM.  (Z)


REMARKS:
SRQ-TPA - FLT 2030 - ON TAKEOFF CREW RECEIVED RIGHT LANDING ALERT AFTER GEAR UP SELECTION, GEAR INDICATIONS NORMAL.  RECYCLED GEAR SEVERAL TIMES AND DIVERTED FLIGHT TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED BOTH MAIN LANDING GEAR DOOR UPLOCK ACTUATORS ON THE RIGHT HAND MAIN LANDING GEAR.  OPS CHECK OK.  (Z)


REMARKS:
DCA - FLT 200 - ON TAKEOFF, TOWER ADVISED FLIGHT THAT FUEL WAS BEING SIPHONED OUT OF WING.  FLIGHT RETURNED TO DCA WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED LT O/B FUEL VENT VALVE.  NO LEAKS NOTED.  (Z)


REMARKS:
GSO - FLT 2243 - FLIGHT EN ROUTE TPA TO BWI WHEN NR 1 START VALVE OPEN LIGHT CAME ON.  CREW SHUTDOWN NR 1 ENGINE AND DIVERTED TO GSO WHERE LANDING WAS WITHOUT INCIDENT.  MAINTENANCE REPLACED START VALVE ASSEMBLY AND START VALVE SWITCH.  RAN NR 1 ENGINE, LEAK AND OPS CHECK NORMAL.  (Z)


REMARKS:
PIT - FOUR OVERWING EXIT LIGHTS AND OVERHEAD EXIT LIGHTS DO NOT ILLUMINATE WITH GEAR DOWN.  MAINTENANCE REPLACED RELAY K2618-A, CHECK NORMAL.  (Z)


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND AFT CARGO DOOR WEB ANGLE CRACKED AT 4TH RIVET AT LOWER FWD STOP.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND BELTFRAME AT BS 967 CORRODED AT SHEAR TIE.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CRACKED AT UPPER CHORD FWD FLANGE RADIUS UNDER SEAT TRACK, BS 520 RBL 25. REPAIRED PER SWA ACO 583-53 R1.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT WING NUMBER 4 SLAT O/B AUX TRACK CUTOUT CRACKED.  REPAIRED PER SWA RA 1-257-0277.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM WEB GROOVED AT BS 294.5 RBL 15.  REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM WEB CORROSION AT BS 1016 AT FWD FLANGE LBL 10.  REPAIRED PER SWA RA 1-253-1298.


REMARKS:
CDG - DURING CRUISE NR 4 ENGINE NACELLE TEMPERATURE INDICATOR SHOWED BOTH FIRE DETECTION LOOPS IN THE OVERHEAT RANGE.  REDUCTION OF ENGINE THRUST AND SUBSEQUENT SHUTDOWN REVEALED TEMPERATURE INDICATOR IN ERROR.  CLEANED LOOP CONNECTORS ANDCONNECTORS OF LOWER AFT LOOP.  OP CHECKS NORMAL.


REMARKS:
STL - DURING POST FLIGHT, FOUND NR 1 FRONT BRAKE TORQUE ARM DISCONNECTED FROM BRAKE.  BOLT, MFG P/N NAS6405U70D, AND PIN, MFG P/N 1523067-101, WERE MISSING.  REPLACED NR 1 BRAKE, BRAKE TORQUE ARM, PIN, BOLT AND LANDING GEAR STRUT DOOR.  LANDING GEAR OPERATION AND BRAKE SYSTEMS CHECKED NORMAL.  REF 95ZZZW744.


REMARKS:
STL - DURING CRUISE SINGLE SERVING CART ELECTRICAL CABLE SHORTED CAUSING SMOKE IN CABIN.  DISCONNECTED ELECTRICAL CABLE.  REPLACED ELECTRICAL CABLE, MFG P/N B03668-2.  SINGLE SERVING CART OPERATION CHECKED NORMAL.


REMARKS:
MCI - DURING INVESTIGATION OF EMERGENCY LIGHT PROBLEMS, FOUND RUDDER CABLE B-1 BURNT.  FOUND EMERGENCY LIGHT BATTERY PACK WIRE RUBBING ON RUDDER CABLE AT STA 1060.  REPLACED RUDDER CABLE AND REPAIRED BATTERY PACK WIRE, CLAMPED WIRE TO CLEAR CABLE.  RUDDER OPERATION AND EMERGENCY LIGHT OPERATION CHECKED NORMAL.


REMARKS:
LGA - DURING CRUISE AT FL 370 A BLUE HAZE APPEARED IN CABIN.  DESCENDED TO FL 330 AND TURNED OFF HIGH PRESSURE BLEEDS AND BLUE HAZE DISSIPATED.  FOUND APU LEAKING OIL.  PLACARDED APU INOPERATIVE PER MEL.  REPLACED BOTH WATER SEPARATOR COALESCER BAGS.  PRESSURIZATION AND AIR CONDITIONING SYSTEMS CHECKED NORMAL.


REMARKS:
STL - AFTER TAKEOFF RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION, AND LANDING GEAR DOOR OPENED DURING UPLATCH CHECK.  FOUND DOOR LATCH MECHANISM, MFG P/N 5915169-5506, WOULD NOT ALWAYS ENGAGE DOORROLLERS.  RIGGED DOOR LATCH MECHANISM.  LANDING GEAR DOOR AND LIGHT INDICATION CHECKED NORMAL.


REMARKS:
STL - DURING CRUISE E GALLEY OVEN, MFG P/N 50381, BEGAN SMOKING WHEN TURNED ON.  TURNED OFF OVEN.  REPLACED OVEN AND OPERATION CHECKED NORMAL.


REMARKS:
CLT - NR 2271 - FLIGHT EN ROUTE TPA TO BWI WHEN NR 1 ENGINE INDICATED HIGH EGT AND FUEL FLOW.  FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE SECURED LOOSE CLAMP ON 13 STAGE DUCT.  LEAK CHECK OK.  RAN ENGINES, CHECKS NORMAL.  NO SPLIT IN THROTTLES OR PARAMETERS.  (W)


REMARKS:
ORF - FLT 2271 - DURING CLIMB-OUT OF ORF, NR 1 ENGINE REVERSE LIGHT AND NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED.  FLIGHTRETURNED TO ORF WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED DUCT ASSEMBLY AND REPAIRED WIRING IN WIRING BUNDLE 2198.  ENGINE OPERATION AND LEAK CHECK SATISFACTORY.  (W)


REMARKS:
BTR - FLT NR 0431 - AT FL 310, CREW RECEIVED RED LIGHTS IN THE COCKPIT.  THE CABIN PRESSURE BEGAN CLIMBING RAPIDLY.  AIRCRAFT MADE AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO BTR.  REPLACED OVERHEAD SELECTOR PANEL DUE TO CONTROLLERINOP.  (W)


REMARKS:
LAX - AFTER TAKEOFF NR 2 ENGINE, S/N 1422, HAD COMPRESSOR STALLS.  REDUCED POWER ON NR 2 ENGINE.  FOUND METAL PARTICLESIN TAIL PIPE.  REPLACED ENGINE S/N 1422.  ENGINE OPERATION CHECKS NORMAL.  ENGINE TOTAL TIME 6,334, TOTAL CYCLES 7,267.


REMARKS:
FLT NR 515 - ATL-FLL - ON THE GATE IN ATL SMOKE WAS REPORTED IN AFT CABIN ROW 25 CDE.  FOUND RT CABIN UTITLITY RECEPTACLE (R5-213) AT STATION 909-R BURNED.  INSPECTED SURROUNDING AREA FOR DAMAGE.  NO DEFECTS NOTED.  DAMAGE LIMITED TO RECEPTACLE.  REPLACED RECEPTACLE.  OPS CHECK NORMAL PER MM 33-20.  (W)


REMARKS:
STL - FLT 1143 - THE FIRST OFFICERS OUTER WINDOW SHATTERED WHILE IN FLIGHT.  THE FLIGHT DIVERTED TO STL.  MAINTENANCE REPLACED THE FIRST OFFICERS WINDSHIELD AND REPLACED THE RIGHT WINDSHIELD HEAT CONTROLLER, P/N 6240665.


REMARKS:
LAX - FLT 2139 - AIR LEAK FROM MAIN ENTRANCE DOOR AFTER TAKEOFF.  FLIGHT RETURNED TO LAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED LEFT FORWARD ENTRY DOOR SEAL.  OPS AND LEAK CHECK OK.  (W)


REMARKS:
PHL - FLT 941 - FLIGHT EN ROUTE BOS TO DCA, WHEN NR 1 ENGINE OIL TEMPERATURE AND PRESSURE INDICATORS DROPPED TO ZERO.  CREW SHUT DOWN NR 1 ENGINE AND DIVERTED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT.  MAINTENANCE RESET D8 CIRCUITBREAKER.  ALL ENGINE INDICATIONS NORMAL.  (W)


REMARKS:
CLT - EXTERIOR EXIT LIGHTS BY AFT OVERWING EXITS ON BOTH SIDES OF AIRCRAFT ARE INOPERATIVE.  MAINTENANCE RELEASED ON MEL 33-14.  REPLACED BATTERY PACKS ON EMERGENCY LIGHTS.  SYSTEM OPS CHECK GOOD.  REMOVED MEL.  (W)


REMARKS:
PVD - ROWS 10, 11, 12L AISLE MARKER EMERGENCY LIGHTS INOPERATIVE AND EMERGENCY LIGHT FOR LEFT ESCAPE WINDOW INOPERATIVE.  MAINTENANCE REPLACED FUSE IN BATTERY PACK M1479 AT STATION 598.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND LEVEL II CORROSION REF CPCP TASK NR C58-53300 FLOORBEAM TOP ANGLE STATION 1338RIGHT LAV.  ACCOMPLISHED SPLICE REPAIR FLOORBEAM AND REPLACED ANGLE PER USAIR TYPICAL REPAIR 53-10-14.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND CHAFED AREA STATION 1401-1418 LONGERON 8 LEFT.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2 AND USAIR TYPICAL REPAIR 53-10-17.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND CRACK 1.25 INCHES LEFT UPPER FORWARD CORNER OF MAIN ENTRANCE DOOR FUSELAGE SKIN (X-RAY INSPECTION).  CUT OUT DAMAGED AREA AND INSTALLED FILLER EXTERNAL DOUBLERS PER SRM 53-05 FIG 26.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND HOLES ELONGATED CAPTAINS AFT OUTBOARD SEAT TRACK.  INSTALLED SET TRACK REPAIR KIT PER USAIR TYPICAL REPAIR 53-20-06 REV A.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND HOLES ELONGATED FLIGHT OFFICER AFT OUTBOARD SEAT TRACK.  INSTALLED REPAIR KIT PER USAIR TYPICAL REPAIR 53-20-06 REV A.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND DENT 2.375 INCH BY 1.75 INCH BY .080 INCH DEEP STATION 296 BETWEEN LONGERON 24L AND 23L.  CUT OUT DAMAGED AREA AND INSTALLED INTERNAL FINGER DOUBLER REPAIR PER SRM 53-04 FIG 38.  (W)


REMARKS:
PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH BY 2 INCH BY .030 INCH DEEP DENT STATION 484 BETWEEN LONGERON 21L AND22L.  CUT OUT DAMAGED AREA AND INSTALLED INTERNAL FINGER DOUBLER REPAIR PER SRM 53-04 FIG 38 VIEW L.  (W)


REMARKS:
PIT -DURING Q-6 CHECK INSPECTION, FOUND .75 INCH CRACK STATION 160 LONGERON 4 LEFT.  SPLICED NEW SECITON OF LONGERON INPER SRM 53-02 FIG 2.  (W)


REMARKS:
PIT - DURING FC- CHECK INSPECTION, FOUND 4 INCH CRACK BETWEEN STRINGER 72 AND 74 AFT SIDE OF FORWARD PRESSURE BULKHEAD CONNECTION ANGLE.  SIP INSPECTION REF 53-10-06.  STOP DRILLED CRACK FABRICATED AND INSTALLED NEW CONNECTION ANGLE DOUBLER PER SRM 53-11-08 PG 2.  (W)


REMARKS:
PIT - DURING FC-2 CHECK INSPECTION, FOUND 5 .125 INCH LONG CRACKS, 3 IN VERTICAL STAB CONNECTION ANGLE INTERMEDIATE SPAR II AND 2 IN INTERMEDIATE SPAR I CONNECTION ANGLE RT.  CONFIRMED VISUAL BY EDDY CURRENT.  REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-31-00 PG 2.  (W)


REMARKS:
IND - DURING CX-2 INSPECTION, FOUND A .25 INCH CRACK AND CORROSION THE AFT CARGO DOOR LOWER SILL DOOR JAM PAN STATION 732 TO 749 AT LONGERON 28R.  REMOVED CORROSION AND CRACKED AREA AND ACCOMPLISHED PAN SPLICE REPAIR PER SRM 53-05 FIG 44.(W)


REMARKS:
PIT - WHILE ACCOMPLISHING PRODUCTION CONTROL ITEM 949, FOUND A .5 INCH CRACK RADIALLY IN LONGERON 2R STATION 680 VISUALINSPECTION.  ACCOMPLISHED SPLICE REPAIR PER SRM53-02 FIG 2 AND USAIR TYPICAL REPAIR 53-10-17.  (W)


REMARKS:
IND - DURING CX-2 INSPECTION ACCOMPLISHED SID INSPECTION PSE REF 53.09.001, FOUND .5 INCH CRACK ACROSS LONGERON AT STATION 408 LONGERON 17 RIGHT.  ACCOMPLISHED LONGERON SPLICE REPAIR PER SRM 53-02 PG 2A AND USAIR EA 30247.  (W)


REMARKS:
IND - DURING SCHEDULED PRODUCTION CONTROL ITEM NR 949, FOUND .125 INCH CRACK IN SKIN OF RIVET STATION 775 LONGERON 1 RT.  EDDY CURRENT INSPECTION.  ACCOMPLISHED REPAIR IAW SRM 53-04.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA .5 INCH BY .5 INCH STATION 500 RT.  REPAIRED PER SRM 51-40-3.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 2 INCH BY 2 ICH F/S 500 A RT S-26 R.  REPAIRED PER SRM 51-40-3.  CORROSION TASK NR C53-208-01.  CORROSION LEVEL 2.  (W)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH AREA OF CORROSION FORWARD SERVICE DOOR 'Z' ANGLE STATION 302 TO 322, WL 208.  REPAIRED PER BOEING DRAWING NR 65-45875 SRM 51-10-1 PG 5.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (W)


REMARKS:
EVV - FLT 0689 - ON DESCENT TO EVV, CREW RECEIVED FLUCTUATING OIL PRESSURE ON THE NR 1 ENGINE THEN RECEIVED A CAWS WARNING.  AN EMERGENCY WAS DECLARED.  THE CREW SHUTDOWN THE NR 1 ENGINE.  SINGLE ENGINE TIME WAS 15 MINUTES.  MAINTENANCE REMOVED THE OIL FILTER AND SCREWS TO CHECK FOR MATERIAL.  ALL CHECKED GOOD.  THEY FOUND THE OIL LEAK TO BE COMING FROM THEGENERATOR.  THE SHAFT AND SEAL ASSEMBLY WAS REPLACED.  OPERATIONAL CHECKED NORMAL.  (W)


REMARKS:
CAE - THE EMERGENCY LIGHTS WOULD NOT SHUT OFF.  MAINTENANCE REPLACED THE POWER SUPPLY.  (W)


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND AFT SECTION OF CABIN EMERGENCY EXIT LIGHTING INOP.  REPLACED BATTERY PACK PER BOEING MM.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND 2 FLOOR TRACK LIGHTS INOP AT AFT SECTION OF CABIN.  REPAIRED AND RECONNECTED TWO WIRESPER BOEING MM.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHTING FROM ROWS 19 THROUGH 21 INOP.  RECONNECTED WIRE TERMINALS TO LIGHT ASSEMBLY PER BOEING MM.


REMARKS:
PASSENGER KICKED RED EMERGENCY EXIT LIGHTS APART.  REPAIRED AND SECURED WIRES PER BOEING M/M.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND NUMEROUS EMERGENCY LIGHTS IN AFT CABIN AREA NOT TESTING.  REPLACED LIGHT BATTERY PACK PER BOEING M/M.


