N699AN

Part: GEARBOX — INOPERATIVE (TE FLAP) · airframe 55,345 hrs · 19,034 cycles

DFW - CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE AND LIGHT. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 FLAP GEARBOX AND TRANSMISSION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GEARBOX — MALFUNCTIONED (TE FLAP) · airframe 55,242 hrs · 18,994 cycles

MCO - CREW REPORTED FLAPS JAMMED AT 20 DEGREES. ACCOMPLISHED GO AROUND. EMERGENCY DECLARED FLIGHT LANDED MCO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT OUTBOARD TRAILING EDGE FLAP TEE GEARBOX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RADOME — PUNCTURED (ZONE 100) · airframe 54,191 hrs · 18,609 cycles

INFLIGHT, CREW REPORTED POSSIBLE LIGHTNING STRIKE DAMAGE. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. DISCOVERED A PUNCTURE IN UPPER RADOME. REPLACED RADOME. SYSTEM GROUND CHECKED NORMAL.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 53,400 hrs · 18,314 cycles

STL - CREW REPORTED LOSS OF RIGHT HYDRAULIC SYSTEM AND PRESSURE. EMERGENCY DECLARED FLIGHT LANDED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DELTA P INDICATOR AT RIGHT HYDRAULIC SYSTEM PRESSURE MODULE BLOWN OUT CAUSING HYDRAULIC FAILURE. REPLACED VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMISSION — INOPERATIVE (TE FLAP) · airframe 52,569 hrs · 17,979 cycles

TUL - CREW REPORTED FLAP DISAGREE ON DESCENT. EMERGENCY DECLARED FLIGHT LANDED TUL WITHOUT INCIDENT. ON TAXI INTO GATE, FLAPS/SLATS WOULD NOT STOW. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT OUTBOARD TRAILING EDGE FLAP TRANSMISSION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PILOT VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 52,101 hrs · 17,799 cycles

MIA - CREW REPORTED LEFT ENGINE BLEED EICAS MESSAGE WITH ASSOCIATED OFF LIGHT IN BLEED VALVE SWITCH. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE HIGH STAGE PILOT VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 51,643 hrs · 17,632 cycles

SEAT 27D EMERGENCY LIGHT INOPERATIVE. REPLACED CONNECTOR FOR SEAT 27D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: PIN — LOOSE (FUEL GOVERNOR) · airframe 50,797 hrs · 17,312 cycles

TUL - DURING FLIGHT AIRCRAFT HAD UNCOMMANDED RIGHT ENGINE SHUTDOWN. SPAR VALVE AND ENGINE LIGHTS OPERATED NORMALLY. FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FUEL FLOW GOVERNOR DUE TO LOOSE PIN ON CONNECTOR FOR FUEL FLOW. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: A/C PACK — DIRTY (AC BAY) · airframe 50,792 hrs · 17,306 cycles

TUL - CREW REPORTED AFTER TAKEOFF FUMES BUT NO SMOKE IN CABIN AND COCKPIT. FLIGHT CREW WENT ON O2. RIGHT PACK WAS SHUTDOWN AND FUMES DISSIPATED. EMERGENCY DECLARED FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED PACK BURNS ON BOTH PACKS PER AMM 21-00-01-2. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 50,792 hrs · 17,305 cycles

DEEP BLEND ON NUMBER 7 SLAT UPPER SKIN (MKD). REMOVED CORRODED AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,792 hrs · 17,305 cycles

FORWARD CARGO DOOR (AAID BBDQZGZ, S/N SAC0061) NUMBER 5 BEAM HAS HEAVY CORROSION BELOW HANDLE AT INNER SKIN ANGLE. REMOVED AND REPLACED BEAM PER ESO 90114.

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,792 hrs · 17,305 cycles

FORWARD CARGO DOOR (AAID BBDQZGZ, S/N SAC00061) HAS A CORRODED T-CHORD AT BOTTOM OF DOOR 20 INCHES FROM FORWARD SIDE. REMOVED AND REPLACED T-CHORD AT BOTTOM OF DOOR 20 INCHES FROM FORWARD SIDE PER ESO90114.

Part: STRUCTURE — WORN (CARGO DOOR) · airframe 50,792 hrs · 17,305 cycles

FORWARD CARGO DOOR (AAID BBDQZGZ, S/N SAC0061) HAS A WORN AND DENTED CORNER SEAL LANDING AT THE LOWER, AFT CORNER. REMOVED AND REPLACED LOWER AFT CORNER SEAL LANDING PER ESO 90114.

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,792 hrs · 17,305 cycles

FORWARD CARGO DOOR (AAID BBDQZGZ, S/N SAC00061) HAS A CORRODED T-CHORD AT BOTTOM OF DOOR 29 INCHES FROM FORWARD SIDE. REMOVED T-CHORD. BLENDED TO REMOVE CORROSION, TREATED, PRIMED, AND PAINTED T-CHORD. RE-INSTALLED T-CHORD PER ESO90114.

Part: STRUCTURE — WORN (CARGO DOOR) · airframe 50,792 hrs · 17,305 cycles

FORWARD CARGO DOOR (AAID BBDQZGZ,S/N SAC00061) HAS A WORN AND DENTED LOWER EDGE SEAL LANDING. REMOVED AND REPLACED LOWER EDGE SEAL LANDING PER ESO90114.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,792 hrs · 17,305 cycles

FWD CARGO DOOR (AAID BBDQZGZ, S/N SAC00061) HAS A CORRODED INTERCOSTAL WEB 29 INCHES FROM FORWARD SIDE ALONG LOWER EDGE OF DOOR. REMOVED AND REPLACED INTERCOSTAL WEB 29 INCHES FROM FORWARD SIDE ALONG LOWER EDGE OF DOOR PER ESO90114.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,792 hrs · 17,305 cycles

FORWARD CARGO DOOR (AAID BBDQZGZ, S/N SAC00061) HAS A CORRODED INTERCOSTAL WEB 39 INCHES FROM FORWARD SIDE ALONG LOWER EDGE OF DOOR. REMOVED AND REPLACED INTERCOSTAL WEB 39 INCHES FROM FORWARD SIDE ALONG LOWER EDGE OF DOOR PER ESO90114.

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,792 hrs · 17,305 cycles

FORWARD CARGO DOOR (AAID BBDQZGZ, S/N SAC00061) HAS LIGHT CORROSION ON T-CHORD AT BOTTOM OF DOOR 39 INCHES FROM FORWARD SIDE. (MKD). REMOVED AND REPLACED T-CHORD AT BOTTOM OF DOOR 39 INCHES FROM FORWARD SIDE PER ESO90114.

Part: SKIN — DAMAGED (DOOR) · airframe 50,792 hrs · 17,305 cycles

SEVERAL LIGHTNING STRIKES ALONG TOP OF DOOR OUTER SKIN. CUT OUT DAMAGE AND INSTALLED DOUBLER PER EA-COMP 52-14144.

Part: PAN — GOUGED (L4 DOOR) · airframe 50,792 hrs · 17,305 cycles

LEFT NUMBER 4 DOOR, HANDLE PAN GOUGED AT HANDLE LATCH AREA. COMPLETED INSTALLATION OF HANDLE PAN PER ESO90108.

Part: PAN — GOUGED (L2 DOOR) · airframe 50,792 hrs · 17,305 cycles

LEFT NUMBER 2 DOOR PAN GOUGED. REMOVED AND REPLACED WITH NEW HANDLE PAN PER ESO 90282.

Part: DOOR — WORN (CARGO DOOR) · airframe 50,792 hrs · 17,305 cycles

AFT CARGO DOOR BOTTOM SEAL LANDING WORN. INSTALLED NEW SEAL LANDING PER ESO 90121.

Part: DOOR — WORN (CARGO DOOR) · airframe 50,792 hrs · 17,305 cycles

AFT CARGO DOOR LOWER CENTER EDGE IS BENT AND WORN. INSTALLED NEW SEAL LANDING PER ESO 90121.

Part: PUMP — LEAKING (RT ENGINE) · airframe 48,954 hrs · 16,661 cycles

DFW - DURING CRUISE, CREW NOTED SEVERAL EICAS MESSAGES RELATING TO RIGHT HYDRAULIC QUANTITY, RIGHT HYDRAULIC PUMP, AND RIGHT HYDRAULIC PRESSURE. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK IN FILTER MODULE AREA OF RIGHT ENGINE PYLON. REPLACED RIGHT ENGINE HYDRAULIC PUMP AND CASE DRAIN/PRESSURE FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,421 hrs · 16,470 cycles

FOUND CRACK AT LEFT WING, AFT SKIN OF NUMBER ONE SLAT AT INBOARD DRIVE TRACK. INSTALLED DOUBLER REPAIR UNDER AARD 57-43-00-4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,944 hrs · 16,293 cycles

EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LAMP AT SEAT 26D.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,944 hrs · 16,293 cycles

SEAT MOUNTED EMERGENCY LIGHT IN FORWARD COACH INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD COACH SEAT EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - SEAT EMERGENCY LIGHTS FOR ROWS 17 TO 25 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EMERGENCY LIGHTS FOR ROWS 17 TO 25.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - AFT EXTERIOR RIGHT NUMBER 3 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT EXTERIOR RIGHT NUMBER 3 DOOR EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FIRST CLASS SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS SEAT EMERGENCY LIGHTS.

Part: HEAT EXCHANGER — CRACKED (RT AC PACK) · airframe 46,442 hrs · 15,770 cycles

DFW - AIRCRAFT COULD NOT CONTROL PRESSURIZATION. EMERGENCY DECLARED, RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TEMPERATURE CONTROL VALVE AND COMPRESSOR OUTLET TEMPERATURE SENSOR VALVE. FOUND RIGHT AIR CONDITIONER PACK RE-HEATER CRACKED. REPLACED RE-HEATER ASSEMBLY HEAT EXCHANGER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PUMP — FAILED (HYDRAULIC SYS)

INFLIGHT - CREW REPORTED CENTER HYDRAULIC SYSTEM QUANTITY LOSS. LANDED DFW WITHOUT INCIDENT. REPLACED NUMBER TWO CENTER HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HYDRAULIC LINE — LEAKING (NLG WW) · 44,054 cycles

POS INFLIGHT T1818/15AUG. DURING CLIMB CREW REPORTED LT HYDRAULIC FLUID LOSS. RETURNED TO POS AND LANDED. DURING LANDING 3 BRAKES SEIZED. REPLACED BROKEN FLEX HYDRAULIC HOSE FROM NOSE WHEEL DOORS. REPLACED NR 2, 6 AND 8 BRAKES DUE TO OVERHEAT. ALSO REPLACED NR 2 AND 4 MAIN TIRES. SYSTEM GROUND CHECKED NORMAL OPS.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT)

MIA EMERGENCY LIGHT AT SEAT 17DEF INOPERATIVE. SECURED WIRING HARNESS FOR EMERGENCY LIGHT AT SEAT 17DEF. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT) · airframe 43,853 hrs

MIA EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. SECURED WIRING HARNESS FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: WIRE HARNESS — INOPERATIVE (FIRE WARNING) · airframe 42,610 hrs

SJU INFLIGHT T412/13MAR STT TO JFK - CREW REPORTED RIGHT ENGINE FIRE WARNING INTERMITTENT. LANDED SJU WITHOUT INCIDENT. REPLACED RIGHT ENGINE FIRE LOOP HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OIL CAP — LOOSE (LT ENGINE)

RNO INFLIGHT T1758/02OCT - LEFT ENGINE OIL QUANTITY LOSS INDICATION. CREW SHUT DOWN NUMBER ONE ENGINE INFLIGHT. LANDED RNO WITHOUT INCIDENT. SINGLE ENGINE TIME 25 MINUTES. FOUND LOOSE OIL CAP. RESECURED OIL CAP FOR NUMBER ONE ENGINE AND ADDED OIL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 9 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 9 FOR EMERGENCY LIGHTS AT SEAT ROWS 9 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COVER — LOOSE (CABIN)

MIA - FOUND EMERGENCY LIGHT COVER AT SEAT 22D LOOSE. REPOSITIONED AND SECURED COVER AT SEAT 22D FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHTS AT FORWARD CABIN, MID CABIN, AND AFT CABIN INOPERATIVE. REPLACED BATTERY PACKS AT FIRST CLASS GALLEY FOR FORWARD CABIN EMERGENCY LIGHTS. REPLACED BATTERY PACK IN CEILING ABOVE SEAT 19EFG FOR MID CABIN EMERGENCY LIGHTS, AND REPLACED BATTERY PACK IN AFT GALLEY FOR AFT CABIN EMERGENY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHT AT MID CABIN SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL CORROSION FOUND ON NUMBER FOUR SEAT TRACK AT ANCHORS FOR COFFEE BAR AT STATIONS 676 AND 686. CORROSION AREA WAS FOUR INCHES BY 10 INCHES AND LOCATED ON CABIN FLOOR. REPLACED NUMBER FOUR SEAT TRACK AT STATION 640 THROUGH 780. (CLOSED)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL CORROSION FOUND ON NUMBER 3 SEAT TRACK AT STATION 676 AND 686 - ANCHORS FOR COFFEE BAR. CORRODED AREA IS FOUR INCHES BY 10 INCHES ON CABIN FLOOR. REPLACED NUMBER THREE SEAT TRACK FROM STATION 640 TO STATION 780. (CLOSED)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21D INOPERATIVE. CONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT PATH LIGHTING AT SEAT 4E INOPERATIVE. SECURED EMERGENCY EXIT PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COFFEEMAKER — DEFECTIVE (GALLEY)

SJU - FLT 1574 - EN ROUTE SJU-BOS - DETECTED SMELL AND SMOKE IN CABIN. RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 3 COFFEEMAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SELECTOR VALVE — DEFECTIVE (NLG)

BDA - FLT 1443 - EN ROUTE BDA-JFK, SHORTLY AFTER TAKEOFF, GEAR RETRACTION EICAS DISAGREE MESSAGE ILLUMINATED. NOSE GEAR LIGHT REMAINED GREEN. NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED BDA AND LANDED WITHOUT FURTHER INCIDENT. PERFORMED FUNCTIONAL CHECK ON NOSE LANDING GEAR. UNABLE TO DETECT FAULT. REPLACED LANDING GEAR SELECTOR VALVE AS A PRECAUTIONARY MEASURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHT INOPERATIVE AT COFFEE BAR. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT COFFEE BAR. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 19 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BALLAST — OVERHEATED (CABIN OVERHEAD)

MSY - FLT 1894 - EN ROUTE DFW/SJU DURING CRUISE, SMOKE NOTED IN CABIN BY L1 DOOR. AIRCRAFT DIVERTED TO MSY AND LANDED OVERWEIGHT WITHOUT INCIDENT. REMOVED FORWARD ENTRYWAY CEILING PANELS AND CHECKED LIGHT BALLASTS. PLACARDED TWO FLUORESCENT LIGHTS IN FORWARD ENTRY OVERHEAD DUE TO TWO BALLASTS (M10381 AND M10382) FOUND HOT, BUT NOT SMOKING. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. SUBSEQUENTLY AT DFW/06, FORWARD ENTRY OVERHEAD BALLASTS REPLACED. SYSTEM GROUND CHECKED, NORMAL OPERATION WITH NO SMOKE OR ODOR NOTED. REMOVED PLACARD FOR FORWARD ENTRY OVERHEAD LIGHTS. (X)