N984TW

Part: OVERHEAT SENSOR — FAULTY (TAIL) · airframe 51,823 hrs · 26,657 cycles

DURING FLIGHT, CREW RECEIVED AN TAIL COMPARTMENT HIGH TEMPERATURE LIGHT. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED LEFT TAIL COMPARTMENT OVERHEAT SENSORS IAW AMM 36-20-02, AND FOUND THE A/C DUCT LOOSE, SECURED THE DUCT IAW AMM 21-20-15. OPS & LEAK CHECKED GOOD.

Part: OVERHEAT SENSOR — FAULTY (TAIL) · airframe 51,823 hrs · 26,657 cycles

DURING FLIGHT, CREW RECEIVED AN TAIL COMPARTMENT HIGH TEMPERATURE LIGHT. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED LEFT TAIL COMPARTMENT OVERHEAT SENSORS IAW AMM 36-20-02, AND FOUND THE A/C DUCT LOOSE, SECURED THE DUCT IAW AMM 21-20-15. OPS & LEAK CHECKED GOOD.

Part: STRAP — BROKEN (TAILCONE SLIDE) · airframe 51,574 hrs · 26,495 cycles

TAILCONE SLIDE RETAINING STRAP ANGLE BROKEN. THE AIRCRAFT WAS GROUNDED. MAINTENANCE INSTALLED A NEW STRAP ASSY ON TAILCONE SLIDE. OKAY FOR SERVICE IAW AMM 25-62-01.

Part: SKIN — CRACKED (BS 83-110) · airframe 51,482 hrs · 26,435 cycles

CRACKED FUSELAGE SKIN AT THE NOSE GEAR RIGHT DOOR, AFT HINGE CUT OUT. REPAIRED THE SKIN IAW SRM 53-05-00-001.

Part: SWITCH — LOOSE (THRUST REVERSER) · airframe 51,049 hrs · 26,166 cycles

AIRCRAFT WAS GROUNDED. RIGHT ENGINE THRUST REVERSER LIGHT STAYS ON. AC RETURNED TO DFW AS THE RIGHT THRUST REVERSER DEPLOYED INDICATION LIGHT. EMERGENCY WAS DECLARED AND THE AC RETURNED TO DFW. AC LANDED WITHOUT INCIDENT, LANDING WAS NOT OVERWEIGHT. TIGHTEN AND CLEANED THRUST REVERSER SWITCH ON RIGHT HAND ENGINE OPERATIONS AND LEAK CHECK GOOD PER AMM 78-32-02.

Part: BRACKET — DAMAGED (GIRT BAR) · airframe 50,754 hrs · 25,973 cycles

RETENTION BRACKET FOR ESCAPE SLIDE GIRT BAR DAMAGED/UNSECURED AT FOWARD SERVICE DOOR R1. REPAIRED R-1 GIRT BAR RETENTION BRACKET PER EA 281123. THE AIRCRAFT WAS GROUNDED.

Part: SCREW — MISSING (GIRT BAR) · airframe 50,609 hrs · 25,863 cycles

FORWARD GALLEY EMERGENCY SLIDE GIRT BAR IS MISSING ONE RIGHT SCREW THAT SECURES THE SLIDE TO THE BAR. REPLACED EMERGENCY SLIDE GIRT BAR HOLDER RIGHT SCREW IAW EA 280506.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 50,167 hrs · 25,578 cycles

AIRCRAFT WAS GROUNDED. COPILOTS WINDSHIELD HAS FRACTURE IN CENTER PLY AT LOWER INBD CORNER. REPLACED WINDSHIELD PER AMM 56-10-02.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 49,939 hrs · 25,439 cycles

FORWARD JUMP SEAT FLASHLIGHT LED DOES NOT FLASH. REPLACED THE BATTERY IAW MM 25-60-00. OK FOR SERVICE.

Part: PANEL — FAULTY (CABIN) · airframe 49,860 hrs · 25,394 cycles

EMERGENCY LIGHT WAS NOT ARMED AND LIGHT WAS FLASHING ON DURING TAXI. LIGHT WAS ON STEADY WHEN STOPPED. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE OVERHEAD PANEL IAW AMM 31-12-01, AND 33-12-01. PERFORMED A SATISFACTORY OPS CHECK.

Part: SWITCH — DEFECTIVE (EMERGENCY LIGHTS) · airframe 49,858 hrs · 25,392 cycles

EMERGENCY LIGHTS NOT ARMED AND FLASHED ON AND OFF DURING FLIGHT. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH S1-177 PER WDM 33-51-11. TESTED GOOD.

Part: LATCH — OUT OF ADJUST (AFT PAX DOOR) · airframe 48,096 hrs · 24,242 cycles

AFT ENTRY TAILCONE DOOR LATCH DOES NOT STAY UP OR LATCHED. ADJUSTED UPPER LATCH TO COVER EMERGENCY HANDLE IAW AMM 52-12-00. OPS CHECKED GOOD.

Part: SENSOR — FAULTY (ZONE 100) · airframe 47,981 hrs · 24,171 cycles

CLIMBING FROM FL330 TO FL350 AIRSPEED INCREASED TO OVERSPEED - USED STANDBY AIRSPEED. BOTH CAP AND FO INDICATIONS WERE OVERSPEED. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED WITHOUT FURTHER INCIDENT. ON FINAL APPROACH AIRSPEED DID NOT APPEAR NORMAL. MAINTENANCE REPLACED THE RAM AIR TEMP PROBE IAW AMM 34-16-02. OPS CHECKS OKAY. PERFORMED PITOT/STATIC LINES DRAIN CHECK. PERFORMED ADJUSTMENT TEST OF PITOT STATIC SYSTEMS. ALL WITHIN TOLERANCE. ALL INDICATORS WITHIN TOLERANCE. ALL TESTS ACCOMPLISHED IAW AMM 34-11-00. THE AIRCRAFT WAS GROUNDED.

Part: REGULATOR VALVE — FAULTY (AC BAY) · airframe 47,933 hrs · 24,142 cycles

AFTER TAKE OFF F/A CALLED COCKPIT REPORTING STRONG ELECTRIC BURNING FUMES IN CABIN. SOME ODOR IN COCKPIT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD ORD WITHOUT FURTHER INCIDENT. MAINTENANCE, WHILE TROUBLESHOOTING, FOUND A WIRE SPLICE CONTACTING DUCT BELOW LT ACM. REPLACED CONNECTOR IAW SWP MM 20-31-01. MAINTENANCE CONTINUED TROUBLESHOOTING AND REPLACED THE LT PRSOV IAW MM 21-31-01-2, OPS AND LEAK CHECKS OK. AS A PRECAUTION, ALSO REPLACED BOTH LEFT AND RIGHT PACK COALESCER BAGS IAW AMM 21-20-02, AND CABIN AIR RECIRCULATION FAN FILTER IAW AMM 21-20-18, ALL OPS AND LEAK CHECKS OK. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR AALA20170414009)

Part: REGULATOR VALVE — FAULTY (AC BAY) · airframe 47,933 hrs · 24,142 cycles

AFTER TAKE OFF F/A CALLED COCKPIT REPORTING STRONG ELECTRIC BURNING FUMES IN CABIN. SOME ODOR IN COCKPIT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD ORD WITHOUT FURTHER INCIDENT. MAINTENANCE, WHILE TROUBLESHOOTING, FOUND A WIRE SPLICE CONTACTING DUCT BELOW LT ACM. REPLACED CONNECTOR IAW SWP MM 20-31-01. MAINTENANCE CONTINUED TROUBLESHOOTING AND REPLACED THE RT PRSOV IAW MM 21-31-01, OPS AND LEAK CHECKS OK. AS A PRECAUTION, ALSO REPLACED BOTH LEFT AND RIGHT PACK COALESCER BAGS IAW AMM 21-20-02, AND CABIN AIR RECIRCULATION FAN FILTER IAW AMM 21-20-18, ALL OPS AND LEAK CHECKS OK. THE AIRCRAFT WAS GROUNDED. (SEE ALSO SDR AALA201704189031)

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,864 hrs · 24,102 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT ACCESSORY COMPARTMENT RIGHT SHEAR TIE CRACKED AT FUSELAGE STATION 1380, LONGERON 13R. REPAIRED IAW AARD 53-10-00-20.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,864 hrs · 24,102 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT ACCESSORY COMPARTMENT LEFT SHEAR TIE CRACKED AT FUSELAGE STATION 1380, LONGERON 13L. REPAIRED IAW AARD 53-10-00-20.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 47,864 hrs · 24,102 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. MID CARGO DOOR THIRD UPPER FORWARD DOOR STOP PAD FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW AARD 51-00-05-1, DRAWINGS CDK 2345 AND 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 47,864 hrs · 24,102 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. MID CARGO DOOR FIRST UPPER AFT DOOR STOP PAD FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW AARD 51-00-05-1, DRAWINGS CDK2345 AND 5910141.

Part: CLAMP — BROKEN (ZONE 200) · airframe 47,396 hrs · 23,811 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-COS FLIGHT RETURNED TO DFW ACCOUNT TAIL COMPARTMENT OVERHEAT INDICATION. LANDING UNEVENTFUL. REMOVED AND REPLACED AIR CONDITIONING FLOW CONTROL VALVE CLAMP IAW AMM 21-31-02. LEAK AND OPERATIONAL CHECK GOOD. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,968 hrs · 23,551 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY LIGHTS OVERHEAD AT SEATS 7B 9D AND 11B STAY ON WITH POWER AND BATTERY SWITCH IS OFF. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 46,458 hrs · 23,231 cycles

CEILING MOUNTED EMERGENCY LIGHT BETWEEN SEAT ROW 11 AND 18 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 44,717 hrs · 22,216 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS AT OVERWING EXIT AT CTR DOES NOT GO OFF. R & R BATTERY PACK B5-102 IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

CORROSION FOUND ON FLOORBEAM AT STATION 1309. BLENDED CORROSION OUT OF LIMITS. INSTALLED NESTED ANGLE REPAIRS AT STATION 1309, RBL 19 & LBL 22 IAW AARD 53-20-00-21 & EA 255505, DATED 10 21 15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

SEAT TRACK NR 4 SPLICE AT STATION 250 - 265, HAS CORROSION VIEWED FROM THE CARGO COMPARTMENT. REMOVED & INSTALLED NEW SEAT TRACK IAW AMM 53-40-01-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

CRACK IN ANGLE, BOTTOM SIDE OF INTERCOSTAL FWD END, STATION 826, BELOW SEAT TRACK NR 5. FABRICATED TWO EACH REPAIR ANGLES & INSTALLED IAW EA 255344.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

FLOORBOARD SUPPORT ANGLE, CRACKED 2 INCHES AT STATION 231, BL0. REMOVED & INSTALLED NEW FLOORBOARD SUPPORT ANGLE IAW AARD 51-00-05-1 & DWG 5930544.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

SEAT TRACK NR 6 IS CORRODED OUT OF LIMITS. R & R SEAT TRACK NR 6 FROM STATIONS 218 - 351 IAW AMM 53-40-01-2 & SRM 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

RIGHT OTBD NR 6 SEAT TRACK CUSP CORRODED AT STATION 1203 - 1206. INSTALLED CUSP DOUBLER REPAIR IAW AARD 53-20-00.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

AFT DOOR JAMB, VAULT DOOR CTR STOP FITTING CRACKED, RT OTBD SIDE OF DOOR JAMB. REMOVED & INSTALLED NEW VAULT DOOR CENTER STOP FITTING IAW AARD 51-00-05 & DWG 5717579.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

CABIN SUBFLOOR & DOUBLER CRACKED, STATION 218, UNDER & OTBD OF NR 4 SEAT TRACK. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,463 hrs · 22,062 cycles

AFT CARGO DOOR LOWER CUT OUT SILL WEB CORRODED UNDERNEATH HOLES STATION 1155 - 1211. REPLACED AFT CARGO DOOR LOWER CUT OUT SILL WEB IAW SRM 51-30-01, SRM 51-30-05, SRM 51-30-02 & SRM 51-10-03.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

G2 GALLEY MOUNT IN FWD END NR 6 SEAT TRACK, CORRODED OUT OF LIMITS. R & R GALLEY MOUNT IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,463 hrs · 22,062 cycles

CORROSION OUT OF LIMITS ON RT CUSP AT STATION 389. INSTALLED REPAIR DOUBLER ON RT CUSP AT STATION 389 IAW AARD 53-20-00-16.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 44,463 hrs · 22,062 cycles

RIGHT WING, GND SPOILER ACTUATOR SUPPORT FITTING CRACKED AT FWD INBD CHAMFER. REPLACED RT WING GND SPOILER SUPPORT FITTING WITH NEW FITTING.

Part: LENS — MISSING (CABIN) · airframe 41,856 hrs · 20,608 cycles

ESCAPE PATH LIGHT AT SEAT 5D MISSING LENS. REPLACED LENS FOR ESCAPE PATH LIGHT AT SEAT 5D. OPERATIONS CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,613 hrs · 20,481 cycles

CRACK IN FRAME AT STATION 1418 & LONGERON 2 RT. INSTALLED DOUBLER REPAIR IAW SRM 53-03-00-001 FIGURE 31A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 41,613 hrs · 20,481 cycles

LONGERON 2 RT CRACKED AFT OF STATION 1418. INSTALLED LONGERON SPLICE & DOUBLER IAW SRM 53-02-00-001 FIGURE 18.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,613 hrs · 20,481 cycles

CRACK IN FRAME AT STATION 1401 & LONGERON 1 LT. INSTALLED DOUBLER IAW AARD 53-10-00-15.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 41,613 hrs · 20,481 cycles

FORWARD CARGO DOOR THIRD STOP FROM THE BOTTOM ON THE FWD SIDE OF THE DOOR WAS FOUND CRACKED. INSTALLED NEW CARGO DOOR STOP FITTING.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 41,613 hrs · 20,481 cycles

STATION 1418 LONGERON 2 LT CRACKED. INSTALLED SPLICE REPAIR IAW SRM 53-02-00-001 FIGURE 18.

Part: DUCT — FAILED (AC BAY) · airframe 41,596 hrs · 20,469 cycles

TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AFTER TAKEOFF. LIGHT WENT OUT WHEN POWER WAS REDUCED TO IDLE. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND DUCT FAILED AT MOVABLE JOINT AREA. REPLACED DUCT ASSEMBLY ON RT SYS. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 41,588 hrs · 20,464 cycles

CRACK ON INBD FACE OF NR 4 LT SLAT TRACK INBD SUPPORT RIB. INSTALLED REPAIR DOUBLER IAW MCM CARD 57-98-05 & EA MD80-57-036318.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 41,588 hrs · 20,464 cycles

CRACK ON INBD FACE OF NR 4 RT SLAT TRACK INBD SUPPORT RIB. INSTALLED REPAIR DOUBLER IAW MCM CARD 57-98-06 & EA MD80-57-036318.

Part: CLAMP — LOOSE (AC BAY) · airframe 41,500 hrs · 20,415 cycles

TAIL COMPARTMENT OVERHEAT INDICATION & LT PACK SHUTDOWN IN CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. FOUND LEAK BETWEEN LT AIR CYCLE MACHINE & HEAT EXCHANGER. TIGHTENED HEAT EXCHANGER CLAMP. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY — NOT SEATED (CABIN) · airframe 38,804 hrs · 19,008 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS FOR CATWALK INOPERATIVE. RESEATED BATTERIES FOR BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,669 hrs · 18,927 cycles

DENT AT STATION 1278 & LONGERON 21 RT. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT WITH NO CRACKS NOTED. ACCOMPLISHED TEMPORARY REPAIR IAW EA MD80-53-030836.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 37,112 hrs · 18,100 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 35,821 hrs · 17,446 cycles

LGA - CREW REPORTED WEATHER RADAR INOPERATIVE. FLIGHT RETURNED LGA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR ANTENNA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (OIL SYSTEM) · airframe 35,777 hrs · 17,422 cycles

DFW - CREW REPORTED RIGHT OIL STRAINER CLOG LIGHT ILLUMINATED IN CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OIL QUANTITY TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: APU — DIRTY (APU BAY) · airframe 33,963 hrs · 16,448 cycles

LAS - CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND EXCESSIVE RESIDUAL OIL FROM AUXILIARY POWER UNIT. CLEANED AREA AND DRAINED OIL. ACCOMPLISHED PACK BURNOUT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — DISCONNECTED (AC BAY) · airframe 33,776 hrs · 16,358 cycles

DFW - CREW REPORTED PRESSURIZATION FLOW LIGHT ILLUMINATED ON CLIMBOUT AND SINGLE PACK OPERATION WOULD NOT PRESSURIZE AIRCRAFT. ACCOMPLISHED PRESSURE FLOW LIGHT QRH. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RECONNECTED RIGHT PACK SUPPLY DUCT THAT WAS DISCONNECTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

FORWARD AIR STAIR SUPPORT/FRAME IS CRACKED AT STATION 160 JUST INSIDE OF AIR STAIR DOORWAY. INSTALLED SERVICEABLE SUPPORT PER AARD 51-10-00-5, IPC 53-40-00-13A AND SRM 51-60-00.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP STATIONS 859 LIGHTENING HOLE PREVIOUSLY BLENDED OUT OF LIMITS. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP CORROSION OUT OF LIMITS IN SEVERAL AREAS. INSTALLED NEW CUSP SHEET LEFT STATIONS 712 TO 788.

Part: SKIN — BENT (ENTRY DOOR) · airframe 33,746 hrs · 16,338 cycles

FORWARD ENTRY DOOR, LOWER SKIN BENT AND OIL CANNED. ACCOMPLISHED REPAIR PER AARD 52-10-00-2.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP STATION 900 LIGHTENING HOLE PREVIOUSLY BLENDED OUT OF LIMITS. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP STATION 1092, BELOW OUTBOARD FLANGE NUMBER 2 SEAT TRACK CRACKED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: WEB — DAMAGED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

OBLONG HOLE IN SUBFLOOR, BELOW G2 GALLEY INBOARD AFT MOUNT. REPAIRED MOUNT PER EA MD80-53-019610.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

NUMBER 1 LONGERON STATION 180 CRACKED. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

NUMBER 2 SEAT TRACK STATIONS 1100 TO 1102 CORRODED. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05-00 FIGURE 4F.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

CORROSION ON SUB-FLOOR UNDER G-1 DRAIN PAN. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

RIGHT CUSP STATION 897 CRACKED. ACCOMPLSHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP LOWER SIDE STATIONS 484-503 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

RIGHT CUSP STATION 595 DAMAGED. REPLACED RIGHT CUSP SHEET STATIONS 579 TO 598 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP SHEET STATIONS 1174 TO 1250 CORRODED. INSTALLED NEW LEFT CUSP SHEET STATIONS 1174 TO 1250.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED REPAIR DOUBLER AT SUBFLOOR UNDER G1 DRAIN PAN AREA PER EA MD80-53-019663.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

RIGHT CUSP STATION 880 CRACKED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

RIGHT CUSP STATION 220 CRACKED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP SHEET STATIONS 1098 TO 1174. INSTALLED NEW LEFT CUSP SHEET STATION 1098 TO 1174.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,746 hrs · 16,338 cycles

LEFT CUSP STATION 218 CRACKED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

RIGHT HAND CUSP BOTTOM SIDE STATION 1218 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

G2 GALLEY FORWARD OUTBOARD MOUNT AT STATION 215 RIGHT BUTTLINE 55 CORRODED. INSTALLED NEW MOUNT PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

NUMBER 6 SEAT TRACK STATIONS 361 TO 365 CORRODED. INSTALLED PLUG PER SRM 53-05-00 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

NUMBER 6 SEAT TRACK STATIONS 594 TO 598 CORRODED. INSTALLED PLUG REPAIR PER SRM 53-05-00 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

SEAT TRACK NUMBER 1 STATION 1174 CORRODED. REPLACED NUMBER 1 SEAT TRACK STATIONS 1174 TO 1309 PER AMM 53-40-01-2.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

CORROSION ON G2 GALLEY TIE DOWN FITTING [MOUNT] STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED NEW MOUNT SRM 51-30-05.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

CORROSION ON THE LEFT TIE DOWN TRACK SPLICE STATIONS 1213 TO 1220. INSTALLED NEW TIE DOWN TRACK SPLICE PER SRM 51-30-02.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 33,746 hrs · 16,338 cycles

FORWARD ENTRY DOOR LOWER OUTER SKIN IS BENT AND OIL CANNED. STRAIGHTENED BENT AREAS OF LOWER SKIN. DYE CHECKED AND FOUND NO CRACK INDICATION. INSTALLED REPAIR DOUBLER PER AARD 52-10-00-2 REPAIR 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,746 hrs · 16,338 cycles

NUMBER 6 SEAT TRACK STATIONS 530 TO 532 CORRODED. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 32,539 hrs · 15,700 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND REPAIRED CONNECTOR. OPS CHECK NORMAL.

Part: DUCT — LEAKING (AC BAY) · airframe 32,353 hrs · 15,607 cycles

MSY - CREW REPORTED TAIL COMPARTMENT OVERHEAT INDICATION. EMERGENCY DECLARED FLIGHT RETURNED MSY LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT 1860 LEAKING. PLACARD LEFT PACK AS INOPERATIVE. REPLACED DUCT AT DFW ON 04/14/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SCHRADER VALVE — DEFECTIVE (NLG) · airframe 29,561 hrs · 14,281 cycles

TUL - CREW REPORTED NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND STRUT FLAT. REPLACED NOSE LANDING GEAR STRUT SCHRADER VALVE AND SERVICED STRUT. PERFORMED FIVE GEAR SWINGS AND NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — FAILED (NR 1) · airframe 28,334 hrs · 13,735 cycles

ON FINAL NUMBER ONE ENGINE BEGAN TO VIBRATE AND SURGE. MOVED THROTTLE TO IDLE. LANDED WITHOUT INCIDENT. FOUND METAL IN TAILPIPE. REPLACED NUMBER ONE ENGINE ON 17 NOV 2009 AT ORD.

Part: LIGHT — LOOSE (CABIN) · airframe 24,736 hrs

SFO - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. SECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: WIRE HARNESS — LOOSE (CABIN) · airframe 24,736 hrs

SFO - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. SECURED WIRE HARNESS FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LENS — MISSING (CABIN) · airframe 24,736 hrs

SFO - EMERGENCY LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: TERMINAL — DIRTY (CABIN) · airframe 24,122 hrs

SFO - EMERGENCY LIGHT AT OVERHEAD FROM AFT FIRST CLASS TO SEAT ROW 18 INOPERATIVE. CLEANED BATTERY PACK TERMINAL FOR EMERGENCY LIGHTS AT OVERHEAD FROM AFT FIRST CLASS TO SEAT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

EMERGENCY LIGHT LENS AT LT NR 4 DOOR MISSING. REPLACED LT NR 4 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

CEILING EMERGENCY LIGHT AT SEAT ROWS 24DEF TO 28DEF INOPERATIVE. REPLACED BATTERY PACK AT SEAT 25DEF FOR INOPERATIVE CEILING EMERGENCY LIGHTS AT SEAT ROWS 24DEF TO 28DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: FIRE DETECTOR — INOPERATIVE (NR 2 NACELLE)

LAS - INFLIGHT LAX ORD NUMBER TWO ENGINE FIRE WARNING LOOP-B WHILE LOOP-A ON PLACARD. AIRCRAFT DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. NO OTHER INDICATIONS OF FIRE. NO FIRE WAS CONFIRMED UPON LANDING. REPLACED LOWER FIRE DETECTION UNIT ON RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — MAKING METAL (RIGHT)

BUF INFLIGHT T305/23OCT - RIGHT ENGINE WAS SHUT DOWN BY CREW DUE TO OIL FILTER CLOG LIGHT ILLUMINATING. FOUND METAL IN SCREEN AND FILTER AND OIL TANK. REPLACED ENGINE. FLIGHT DATA RECORDER DOWNLOAD REQUESTED BY ENGINEERING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT AT 11D INOPERATIVE. REPLACED EMERGENCY LIGHT SOCKET AT SEAT 11D. SYSTEM GROUND CHECKED. NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT 11D INOPERATIVE. RECONNECTED SEAT EMERGENCY LIGHT AT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — INOPERATIVE (RIGHT)

DFW - FIFTEEN MINUTES BEFORE LANDING THE RIGHT ENGINE OIL QUANTITY WENT TO ZERO. AFTER A COUPLE OF MINUTES THE AMBER LOW OIL QUANTITY LIGHT CAME ON QUICKLY FOLLOWED BY THE RED LIGHT. THE RIGHT ENGINE WAS SHUTDOWN PER CHECKLIST. THE SHUTDOWN WAS NORMAL. THEN ENGINE WINDMILLED FOR 8 TO 10 MINUTES UNTIL LANDING. LANDED DFW WITHOUT INCIDENT. FLIGHT DATA RECORDER DOWNLOADED PER ENGINEERING. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,771 hrs · 4,960 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM SEAT ROW 28 AFT. REPLACED THE POWER SUPPLY. CHECK-C 12-17-02 STL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,550 hrs · 4,836 cycles

THE EGRESS LIGHT WAS INOPERATIVE AT THE FWD EMERGENCY EXIT AND 5 ROWS FORWARD. REPLACED THE BATTERY PACK AT ROW 16. CHECK-C 12-17-02 STL.

Part: SKIN — BENT (CARGO DOOR) · airframe 5,764 hrs · 3,129 cycles

DURING CHECK-C MAINT THE FWD CARGO DOOR SKIN BELOW THE DOOR HANDLE WAS BENT INWARD. INSTALLED DOUBLER PER SRM 52-05, FIG 30.

Part: SKIN — BENT (CARGO DOOR) · airframe 5,764 hrs · 3,129 cycles

DURING CHECK-C MAINT THE MID CARGO DOOR SKIN BELOW THE DOOR HANDLE WAS BENT INWARD. INSTALLED DOUBLER PER SRM 52-05, FIG 30.