N970TW

Part: REGULATOR VALVE — DEFECTIVE (A/C PACK) · airframe 51,383 hrs · 25,799 cycles

ODOR OF DIRTY SOCKS IN THE CABIN, DISSIPATED WITHOUT FLIGHT OR CABIN CREW ACTIONS. OCCURED FROM TAKEOFF ROLL THROUGH 7000 FT. ACCOMPLISHED MCM 05-96-70. ODOR DETERMINED TO BE TYPE 4 ODOR. THE AIRCRAFT WAS GROUNDED. REPLACED THE LEFT AND RIGHT AIR CONDITIONER PRESSURE REGULATOR VALVES IAW MM 21-31-01, AND THE LEFT AND RIGHT COALESCER BAGS IAW MM 21-20-02. OPS AND LEAK CHECKED GOOD.

Part: COALESCER BAG — DEFECTIVE (A/C PACK) · airframe 51,383 hrs · 25,799 cycles

ODOR OF DIRTY SOCKS IN THE CABIN, DISSIPATED WITHOUT FLIGHT OR CABIN CREW ACTIONS. OCCURED FROM TAKEOFF ROLL THROUGH 7000 FT. ACCOMPLISHED MCM 05-96-70. ODOR DETERMINED TO BE TYPE 4 ODOR. THE AIRCRAFT WAS GROUNDED. REPLACED THE LEFT AND RIGHT AIR CONDITIONER PRESSURE REGULATOR VALVES IAW MM 21-31-01, AND THE LEFT AND RIGHT COALESCER BAGS IAW MM 21-20-02. OPS AND LEAK CHECKED GOOD.

Part: REGULATOR VALVE — DEFECTIVE (A/C PACK) · airframe 51,383 hrs · 25,799 cycles

ODOR OF DIRTY SOCKS IN THE CABIN, DISSIPATED WITHOUT FLIGHT OR CABIN CREW ACTIONS. OCCURED FROM TAKEOFF ROLL THROUGH 7000 FT. ACCOMPLISHED MCM 05-96-70. ODOR DETERMINED TO BE TYPE 4 ODOR. THE AIRCRAFT WAS GROUNDED. REPLACED THE LEFT AND RIGHT AIR CONDITIONER PRESSURE REGULATOR VALVES IAW MM 21-31-01, AND THE LEFT AND RIGHT COALESCER BAGS IAW MM 21-20-02. OPS AND LEAK CHECKED GOOD.

Part: COALESCER BAG — DEFECTIVE (A/C PACK) · airframe 51,383 hrs · 25,799 cycles

ODOR OF DIRTY SOCKS IN THE CABIN, DISSIPATED WITHOUT FLIGHT OR CABIN CREW ACTIONS. OCCURED FROM TAKEOFF ROLL THROUGH 7000 FT. ACCOMPLISHED MCM 05-96-70. ODOR DETERMINED TO BE TYPE 4 ODOR. THE AIRCRAFT WAS GROUNDED. REPLACED THE LEFT AND RIGHT AIR CONDITIONER PRESSURE REGULATOR VALVES IAW MM 21-31-01, AND THE LEFT AND RIGHT COALESCER BAGS IAW MM 21-20-02. OPS AND LEAK CHECKED GOOD.

Part: LONGERON — CRACKED (BS 993) · airframe 51,058 hrs · 25,591 cycles

A CRACK INDICATION IN THE RADIUS OF THE RIGHT WHEEL WELL, LONGERON 20R, BS 993. REPAIRED THE LONGERON IAW 53-10-00-18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,058 hrs · 25,591 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FUSELAGE SKIN CRACKED AT AFT HINGE CUTOUT FOR LEFT AFT NOSE LANDING GEAR DOOR. INSTALLED REPAIR DOUBLER PER SRM 53-05-00--001 PARA 162, FIGURE 158.

Part: SKIN — CRACKED (AFT) · airframe 50,968 hrs · 25,533 cycles

AFT FUSELAGE SKIN CRACKED ON THE LEFT SIDE ABOVE THE AFT AIRSTAIRS, JUST FORWARD OF TAIL CONE EJECTION HANDLE COMPARTMENT. THE AIRCRAFT WAS GROUNDED. REPAIRED IAW 53-30-00-4 REPAIR 4.

Part: WINDOW — DELAMINATED (R1 COCKPIT) · airframe 50,612 hrs · 25,308 cycles

FIRST OFFICERS WINDSHIELD HAS A SMOOTH EDGE DELAMINATION AT THE BOTTOM FORWARD CORNER IN EXCESS OF LIMITS. REPLACED THE R1 WINDOW IAW AMM 56-10-02.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 50,322 hrs · 25,120 cycles

AIRCRAFT WAS GROUNDED. CENTER WINDSHIELD HAS ARC BURNS AND DELAMINATION AROUND THE PERIMETER. LOWER CORNERS VERY BAD. REPLACED CENTER WINDSHIELD PER AMM 56-10-01. ANTI-ICE AND ANTIFOG OPERATIONS CHECK GOOD.

Part: CSD — INOPERATIVE (LT ENGINE) · airframe 50,323 hrs · 25,120 cycles

FLIGHT RETURNED TO DEPARTURE, DUE TO A GENERATOR FAIL INDICATION. EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. REPLACED THE LEFT ENGINE CONSTANT SPEED DRIVE, LEAK AND OPS CHECKED GOOD IAW AMM 24-10-01.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 49,950 hrs · 24,879 cycles

EMERGENCY EXIT LIGHT AT ROW 22 DOESNT ILLUMINATE. FOUND DISCONNECTED AT LIGHT. CONNECTED THE EMERGENCY EXIT LIGHT AT SEAT ROW 22 IAW AMM 33-60-98. OP CHECKED NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,694 hrs · 24,707 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD EMERGENCY FLASHLIGHT IS NOT CHARGING (LED DOES NOT FLASH). REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY PER AMM 25-60-00. OPERATIONS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 49,331 hrs · 24,441 cycles

THE AIRCRAFT WAS NOT GROUNDED. DECLARED AN EMERGENCY - RT MLG UNSAFE ISSUE. PILOT REPORTED POSSIBLE STREAMER/FOD FROM RIGHT MAIN LANDING GEAR . ALL INDICATIONS NORMAL ON RETRACTION AND EXTENSION, INSPECTED BOTH WHEEL WELLS FOR POSSIBLE FOD/ UNWANTED MATERIAL. CHECKS OK, NO DEFECTS NOTED. OK FOR SERVICE . LANDING GEAR CHECK OK. NO FOD OR UNWANTED MATERIAL.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 48,898 hrs · 24,153 cycles

OVERHEAD EMERENCY EXIT LIGHT L2-637 IN THE TAIL COMPARTMENT HAS WIRING THAT IS CHAFED AND SHORTING. REPAIRED DAMAGED WIRE L795B16 PER WDM 33-51-13. OPERATIONAL CHECK GOOD.

Part: BEZEL — DAMAGED (FLASHLIGHT) · airframe 48,898 hrs · 24,153 cycles

EMERGENCY FLASHLIGHT BEZEL AT FORWARD JUMPSEAT AGAINST FORWARD LAVATORY WALL HAS A HOLE IN IT. REMOVED AND REPLACED BEZEL IAW AMM 25-41-11.

Part: COVER — OUT OF POSITION (L2 DOOR SLIDE) · airframe 48,562 hrs · 23,947 cycles

L2 DOOR SLIDE BOTTOM AFT COVER IS PROTRUDING OUT. REPOSITIONED COVER . OPS CHECKED GOOD.

Part: FITTING — CORRODED (LT WING TE FLAP) · airframe 47,598 hrs · 23,332 cycles

CORROSION ON LEFT WING OUTBOARD FLAP CENTER AFT HINGE FITTING. REMOVED AND REPLACED FITTING IAW AMM 57-40-01-201 AND ESO 800096.

Part: FITTING — CRACKED (SPOILER) · airframe 47,598 hrs · 23,332 cycles

CRACK ON RIGHT WING GROUND SPOILER FITTING. INSTALLED A NEW FITTING IAW SRM 51-30-02 AND SRM 51-30-05.

Part: PIN — DETACHED (EVAC SLIDE) · airframe 47,412 hrs · 23,202 cycles

AIRCRAFT WAS GROUNDED. L2 DOOR EMERGENCY EVACUATION SLIDE PINS DETACHED FROM COVER. REMOVED AND REPLACED SLIDE IAW AMM 25-94-17. OPERATIONAL CHECK GOOD.

Part: PITOT TUBE — FAULTY · airframe 46,515 hrs · 22,642 cycles

DURING CLIMB THE FIRST OFFICER"S PITOT HEAT FAILED RESULTING IN A NR 2 CADC FAILURE. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. REMOVED AND REPLACED FIRST OFFICER"S PITOT TUBE IAW AMM 34-11-00. OPS AND LEAK CHECKED NORMAL.

Part: PROXIMITY SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 46,368 hrs · 22,555 cycles

DURING TAKE OFF ROLL, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. THE TAKE OFF WAS ABORTED AT APPROXIMATELY 100 KNOTS. MAINTENANCE ACCOMPLISHED ADJUSTMENT AND TEST OF THE FORWARD CARGO DOOR PROXIMITY SWITCH IAW AMM 52-70-02. SYSTEM CHECKED NORMAL

Part: APU — LEAKING (ZONE 100) · airframe 45,919 hrs · 22,293 cycles

REPORTS OILY ODOR WHEN APU STARTED AT GATE. ACCOMPLISHED CARD 21-96-01 & FOUND APU OIL LEAK. REMOVED AND REPLACED AUXILIARY POWER UNIT IAW MCM 49-96-83. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,540 hrs · 21,476 cycles

OVERHEAD EMER LIGHTS INOPERATIVE IN CABIN FROM OVERWING EXITS AFT TO AFT LIGHT ATTENDANT JUMP SEAT. R & R B5-106 & B5-107 EMER LIGHT BATTERY PACKS IAW AMM 33-53-00. REFERENCE WDM 33-51-11. OPERATIONAL CHECKED GOOD IAW AMM 33-53-00. SEE ALSO AALA20151110004.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,540 hrs · 21,476 cycles

ONE PAIR OF EMER EXIT LIGHTS INTERIOR OVERWING EXIT INOPERATIVE. R & R EMER LIGHT BATTERY PACK B5-105. BOTH LT & RT AFT OVERWING EXIT LIGHT OPERATIONAL CHECKED NORMAL IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,540 hrs · 21,476 cycles

OVERHEAD EMER LIGHTS INOPERATIVE IN CABIN FROM OVERWING EXITS AFT TO AFT LIGHT ATTENDANT JUMP SEAT. R & R B5-106 & B5-107 EMER LIGHT BATTERY PACKS IAW AMM 33-53-00, REFERENCE WDM 33-51-11. OPERATIONAL CHECKED GOOD IAW AMM 33-53-00. SEE ALSO AALA20151110009.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,397 hrs · 21,392 cycles

FUSELAGE SKIN DAMAGE, STATION 212, LONGERON 17L. REPAIRED IAW SRM 53-04-02, REPAIR FIGURE 2, SHEET 19.

Part: BATTERY — FAULTY (CABIN) · airframe 44,173 hrs · 21,247 cycles

LIGHTS COME ON WHEN ACFT IS POWERED OFF. R & R WITH SERVICEABLE UNIT, CORRECTED ISSUE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

AFT SIDE OF CANT FRAME 1463 LT, ABOUT 10:00 POSITION, WEB SPLICE IS BROKEN & HAS CRACKS AT UPPER INBD CORNER. INSTALLED FILLER & DOUBLER IAW SRM 53-03-00-001 FIG 38C.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

RIGHT CANT FRAME 1474 CRACKED AT TOP OF RT LOUVER CUT OUT, & AT ATTACH FASTENER TO UPPER LOUVER SUPPORT ANGLE. INSTALLED NEW SERVICEABLE J FRAME AT STATION 1474, RT SIDE ABOVE RT LOUVER BOX IAW AARD 51-00-05-1, SRM 51-30-05, SRM 51-30-02 & SRM 51-70-05-001.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

SHEAR TIE CRACKED AT STATION 1446 BELOW L17R. STOP DRILLED CRACK & INSTALLED REPAIR ANGLE IAW AARD 53-10-00-20.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

CANT FRAME AT FS 1463 & L19R IS CRACKED. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-01-00-001 FIG 2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

CRACKED SHEAR TIE AT STATION 1437, OTBD OF LT FITTING. REPLACED SHEAR TIE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

SHEAR TIE CRACKED AT STATION 1437, OTBD OF RT FITTING. REPLACED SHEAR TIE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

CABIN CTR FLOORBOARD INTERCOSTAL STATION 1287 - 1309 IS CRACKED. REMOVED & INSTALLED NEW INTERCOSTAL.

Part: BEAM — CORRODED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

AFT CARGO DOOR BEAM CORRODED STATION 1155 - 1212. INSTALLED BEAM DOUBLER IAW AARD 53-10-00-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 44,173 hrs · 21,247 cycles

AFT CARGO LT TIE DOWN TRACK CORRODED STATION 1117 - 1136. INSTALLED NEW SECTION OF AFT CARGO LT TIE DOWN TRACK SECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,173 hrs · 21,247 cycles

CABIN SEAT TRACK NR 3 CORRODED OUT OF LIMITS FROM STATION 1221 - 1309. COMPLETED INSTALLATION OF NEW SECTION OF NR 3 SEAT TRACK IAW SRM 53-05-00 FIG 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

SEAT TRACK NR 6 CORRODED, BETWEEN STATIONS 218 & 588. R & R SEAT TRACK SECTION, BETWEEN STATIONS 216 & 588 IAW AMM 53-40-01-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

SEAT TRACK NR 6 CORRODED BETWEEN STATIONS 824 & 827. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

SEAT TRACK NR 6 CORRODED BETWEEN STATIONS 1180 & 1190. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW SRM 53-05-00 FIGURE 4A1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

SEAT TRACK NR 6 CORRODED BETWEEN STATIONS 851 & 853. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW SRM 53-05-00-001.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

RIGHT CUSP SHEET IS CRACKED BETWEEN STATIONS 218 & 237. R & R CUSP SHEET IAW AARD 51-00-05-1 & DWG 9930538.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

G2 GALLEY MOUNT AT STATION 216, FWD END OF EAST TRACK NR 6, IS CORRODED. R & R GALLEY MOUNT IAW AARD 51-00-05-1 & DWG 5930547.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

FUSELAGE FRAME CRACKED AT STATION 1401 & LONGERON 1. ACCOMPLISHED FRAME DOUBLER REPAIR IAW AARD 53-10-00-15.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,173 hrs · 21,247 cycles

CORROSION ON RT CUSP FROM STATION 384 TO 389. ACCOMPLISHED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

FUSELAGE FRAME CRACKED AT APPROX STATION 1457, STRINGER 2R. INSTALLED FWD ANGLE DOUBLER, AFT PLATE, FILLER & CLIP AT STATION 1457, L2 R IAW SRM 53-03-00-001.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,173 hrs · 21,247 cycles

CORROSION ON LT CUSP BETWEEN STATIONS 1176 & 1185, CONTINUES UNDER SEAT TRACK & FRAME FOOT. ACCOMPLISHED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,173 hrs · 21,247 cycles

CRACKED SHEAR TIE FWD SIDE OF FRAME 1380 ABOVE L14R. INSTALLED REPAIR DOUBLER AT STATION 1380, L14R IAW AARD 53-10-00-20.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,100 hrs · 21,202 cycles

CEILING EMER LIGHTS IN FIRST CLASS FAIL TO TEST. R & R B5-100 EMER LIGHT POWER SUPPLY IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: FILTER — DIRTY (RECIRC FAN) · airframe 43,339 hrs · 20,780 cycles

DURING CLIMB CREW REPORTED ELEC BURNING ODOR IN CABIN. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING CARD 21-96-01. EMERGENCY DECLARED, AND LANDING UNEVENTFUL. COULD NOT DUPLICATE. R & R RECIRCULATION FAN FILTER IAW AMM 21-20-18. RAN LT & RT PACKS WITH ENGS & APU. INSPECTED LIGHT FIXTURES, COFFEE MAKERS & CB PANELS. NO ODORS NOTED.

Part: PLATE — PUNCTURED (HORIZ STAB) · airframe 42,857 hrs · 20,523 cycles

PUNCTURE IN THE LOWER FWD PLATE OF THE HORIZONTAL STABILIZER CTR SECTION. REPAIRED PLATE IAW EA 55-038786.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 41,165 hrs · 19,625 cycles

MID CARGO DOOR STOP CRACKED. R & R DOOR STOP.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 41,165 hrs · 19,625 cycles

LEFT WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER IAW EA MD80-57-035409.

Part: WIRE — BROKEN (CABIN) · airframe 40,683 hrs · 19,380 cycles

SEAT 11D EMERGENCY LIGHT INOPERATIVE. TERMINATED BROKEN WIRE AT ESCAPE PATH LIGHT CONNECTOR AT SEAT 11D, OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 40,683 hrs · 19,380 cycles

SEAT 10D ESCAPE PATH LIGHT INOPERATIVE. TERMINATED BROKEN WIRE AT ESCAPE PATH LIGHT CONNECTOR AT SEAT 10D. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,683 hrs · 19,380 cycles

SEAT 8D ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED PROXIMITY LIGHT AT 8D. OPERATIONS CHECKED NORMAL.

Part: HEATER — FAILED (CARGO BAY) · airframe 40,481 hrs · 19,274 cycles

STL CREW REPORTED SMOKE & FUMES IN THE FWD CABIN. EMERGENCY DECLARED FLIGHT RETURNED STL LANDED WITHOUT INCIDENT. INSPECTED ACFT & FOUND FWD CARGO COMPARTMENT HEATER FAILED. DEFERRED FWD CARGO COMPARTMENT HEATER SYS EAW MEL 21-38. FLIGHT CONTINUED TO DESTINATION. REPLACED FWD CARGO HEATER AT DFW ON 03/20/2014. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 40,349 hrs · 19,213 cycles

DFW INFLIGHT ORD-PSP CREW REPORTED ENG ANTI ICE LIGHT ILLUMINATED DURING FLIGHT. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT HAND ENG OTBD ANTI ICE VLV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SEAL — DAMAGED (NLG) · airframe 39,757 hrs · 18,907 cycles

DFW CREW REPORTED DURING GEAR RETRACTION "NOSE LANDING GEAR UNSAFE" INDICATION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED METERING PIN SEALS & REPACKED NLG. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: SENSOR — DEFECTIVE (NLG) · airframe 37,365 hrs · 17,632 cycles

ORD - CREW REPORTED NOSE GEAR UNSAFE INDICATION. FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED D1-31 SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,365 hrs · 17,632 cycles

CRACK IN FUSELAGE SKIN TAIL COMPARTMENT AREA RIGHT SIDE STATION 1474. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,365 hrs · 17,632 cycles

CRACK IN FUSELAGE SKIN TAIL COMPARTMENT AREA LEFT SIDE STATION 1474. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 37,001 hrs · 17,440 cycles

CLE INFLIGHT ORD-PHL. CREW REPORTED LEFT ENGINE GENERATOR FAILED AND AUXILIARY POWER UNIT WOULD NOT START. EMERGENCY DECLARED FLIGHT DIVERTED CLE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE GENERATOR AND CONSTANT SPEED DRIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 35,176 hrs · 16,484 cycles

EMERGENCY LIGHT AT ROW 22 INOPERATIVE. SECURED LOOSE CONNECTOR. OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 35,176 hrs · 16,484 cycles

EMERGENCY LIGHT AT ROW 24 INOPERATIVE. SECURED LOOSE CONNECTOR. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (TE FLAP) · airframe 33,471 hrs · 15,632 cycles

TRAILING EDGE OF CENTER FLAP WEDGE AND TOP SKIN IS DAMAGED. INSTALLED NEW SERVICEABLE FLAP WEDGE PER PATTERN CARD 1661.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,471 hrs · 15,632 cycles

STATIONS 1041 TO 1060 LONGERONS 8 TO 9 RIGHT PREVIOUSLY WORKED DENT WITH CREASE INSIDE DENT. INSTALLED DOUBLER AT STATION 1055 LONGERONS 8 TO 9 RIGHT PER SRM 53-04-00 FIGURE 12B SHEET 4.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 33,471 hrs · 15,632 cycles

STATIONS 1041 TO 1060 LONGERONS 7 TO 8 RIGHT PREVIOUSLY WORKED DENT WITH CREASE, INSIDE DENT 9 AND 1/2 INCHES LONG AND 1 INCH TO 1 AND 1/2 INCHES WIDE. INSTALLED DOUBLER AT STATION 1055 LONGERONS 8 TO 9 RIGHT PER SRM 53-04-00 FIGURE 12B SHEET 4.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,471 hrs · 15,632 cycles

HAIL DAMAGE DENT IN FUSELAGE SKIN, STATION 332, ABOVE LONGERON 3 LEFT. INSTALLED INTERNAL DOUBLER AND SKIN FILLER STATION 332 BETWEEN LONGERONS 2 AND 3 PER BOEING DRAWING SG09530001 FIGURE F1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,471 hrs · 15,632 cycles

CORROSION ON SUBFLOOR UNDER G-1 GALLEY PAN. INSTALLED DOUBLER ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: DOOR — DAMAGED (ENTRY DOOR) · airframe 33,471 hrs · 15,632 cycles

FORWARD ENTRY DOOR OUTER SKIN DAMAGED AT HOOK CUTOUT. BLENDED TO REMOVE DAMAGE AT HOOK CUT-OUT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 20A.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,471 hrs · 15,632 cycles

NUMBER 6 SEAT TRACK STATIONS 631 TO 633 CORROSION REMOVAL OUT OF LIMITS. INSTALLED SEAT TRACK PLUG PER AARD53-20-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,471 hrs · 15,632 cycles

NUMBER 6 SEAT TRACK STATIONS 546 TO 547 CORROSION REMOVAL OUT OF LIMITS. INSTALLED SEAT TRACK PLUG PER AARD53-20-10.

Part: UNLOCK SWITCH — INOPERATIVE (THRUST REVERSER) · airframe 32,597 hrs · 15,202 cycles

DFW - CAPTAIN REPORTED ON CLIMBOUT LEFT THRUST REVERSER BLUE UNSAFE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. FOUND UPPER UNLOCK SWITCH INOPERATIVE. REPLACED SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UNLOCK SWITCH — FAULTY (THRUST REVERSER) · airframe 31,350 hrs · 14,619 cycles

DFW - CREW REPORTED LEFT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED IN FLIGHT. ACCOMPLISHED QRH PROCEDURE. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. LIGHT REMAINED ILLUMINATED FOR DURATION OF FLIGHT AND AFTER AIRCRAFT REMAINED PARKED AT GATE. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT THRUST REVERSER UNLOCK SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 29,355 hrs · 13,703 cycles

INTERNAL DOUBLER AT STATION 628 LONGERON 30 DAMAGED BEYOND REPAIR. INSTALLED REPAIR PER EA 53-009526.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,355 hrs · 13,703 cycles

DOUBLER FOR RADIO ALTIMETER AT STATION 725 CORRODED. REPLACED DOUBLER WITH NEW PER SRM 53-04-00 FIGURE 44 SHEET 1 TO 4 BOEING SR09530107 E58 6355549.

Part: SHUTOFF VALVE — STICKING (FUEL SYSTEM) · airframe 29,113 hrs · 13,585 cycles

EWR - CREW REPORTED RIGHT ENGINE OIL TEMPERATURE HIGH. EMERGENCY DECLARED RETURNED EWR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE FUEL HEAT SHUTOFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — WEAK (CABIN) · airframe 28,072 hrs · 13,163 cycles

EMERGENCY LIGHT BATTERY PACK AB5-4 AT STATION 1154 HAS VERY LOW OUTPUT. REPLACED BATTERY PACK.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 27,691 hrs · 13,004 cycles

TUL - INFLIGHT ORD-DFW. CREW REPORTED ENGINE OIL FILTER CLOG LIGHT ON AND LEFT ENGINE COMPRESSOR STALL. LEFT ENGINE PULLED TO IDLE BUT WAS NOT SHUT DOWN. EMERGENCY DECLARED, LANDED TUL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ON AUG 21,2009 AT TUL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OIL FILTER — DEFECTIVE (LEFT) · airframe 27,690 hrs · 13,003 cycles

MCI - INFLIGHT DFW-ORD. CREW REPORTED LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED AT FL320. ALL ENGINE INDICATIONS STAYED NORMAL. ENGINE OPERATED AT IDLE THRUST TILL LANDING. LIGHT STAYED ILLUMINATED. EMERGENCY DECLARED, LANDED MCI WITHOUT INCIDENT. REMOVED AND REPLACED LEFT ENGINE OIL FILTER AND ACCOMPLISHED MCM 71-91-12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,490 hrs · 12,904 cycles

SFO - SEAT 24D EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE BROKEN PIN CONNECTOR. OPS CHECKED NORMAL.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,490 hrs · 12,904 cycles

SFO - EMERGENCY EXIT LIGHT AT SEAT 32D INOPERATIVE. REMOVED AND REPLACED THE BROKEN PIN CONNECTOR. OPS CHECKED OK.

Part: PIN — BROKEN (CONNECTOR) · airframe 27,476 hrs · 12,899 cycles

SFO - EMERGENCY EXIT LIGHT ON SEAT 32D INOPERATIVE. REMOVED AND REPLACED BROKEN PIN CONNECTOR. OPS CHECK OK AS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,165 hrs

SFO - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUBMER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LONGERON — CRACKED (BS 1418) · airframe 24,845 hrs · 11,782 cycles

LONGERON 2 RT HAS 1 INCH CRACK AT STATION 1418. ACCOMPLISHED SPLICE REPAIR IN ACCORDANCE WITH AARD 53-30-00-2.

Part: ELECTRONIC UNIT — INOPERATIVE (FIRE DETECTION) · airframe 23,178 hrs

DFW - INFLIGHT T1507/12MAR - CREW REPORTED AFT CARGO FIRE LIGHT ILLUMINATED. DISCHARGED BOTTLES ONE AND TWO. LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE FOUND. REPLACED FIRE EXTINGUISH BOTTLE AND AFT CARGO LINE FILTER. REPLACED AFT CARGO ELECTRONIC UNIT AND NUMBER TWO SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 22,206 hrs

SAT INFLIGHT T1303/12NOV - NUMBER TWO ENGINE HAD COMPRESSOR STALLS ON INITIAL CLIMB-OUT PASSING 3500 FEET. CREW HEARD THREE OR FOUR BANGS. ENGINE WAS BROUGHT TO IDLE UNTIL LANDING. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. FOUND INTERNAL DAMAGE TO 12 AND 13 STAGE. REPLACED NUMBER TWO ENGINE ON 13 NOV 2007 AT SAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

LGA - EMERGENCY FLASHLIGHTS AT BOTH FORWARD POSITIONS HAVE SAFETY STRAPS BROKEN. REPLACED SAFETY STRAPS FOR EMERGENCY FLASHLIGHTS AT BOTH FORWARD POSITIONS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LGA - FOUND EMERGENCY PORTABLE LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY PORTABLE LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 6 HAS MISSING LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROW 25 ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: POWER SUPPLY — WORN · airframe 8,118 hrs · 4,442 cycles

DURING OVERNIGHT MAINTENANCE, OPERATION CHECK OF EGRESS LIGHTING FAILED. REPAIRED BY REPLACING EMERGENCY LIGHT POWER SUPPLY (TWA PN 93-0267), OPS-CK ASSURED NORMAL PERFORMANCE. LAST-CC / STL 7/6/01

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,306 hrs · 3,937 cycles

THE EGRESS LIGHT WAS INOPERATIVE AT ROW 24 AND THE FWD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMP AT ROW 24, P/N 7732, AND THE BATTERIES, P/N 408822-101, FOR THE OVERWING LIGHTS.

Part: MODULE — WORN (ROW 22) · airframe 3,274 hrs · 1,821 cycles

THE RED EGRESS LIGHTS WERE INOPERATIVE AT ROW 22D AND THE LEFT SIDE NUMBER 2 DOOR. REPLACED LIGHT MODULES (P/N 0105606-003) AT ROW 22D, AND (P/N 0105606-002) AT L2 DOOR. CHECK-C 7-28-00 JFK.