N609AA

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 67,041 hrs · 17,834 cycles

CORROSION ON LT WING SLAT BETWEEN WS 509.50 TO 537.50 APPROX 47 INCHES INBD FROM OTBD END, 6 INCHES UP FROM LE. INSTALLED FILLER & DOUBLER ON LT WING SLAT IAW AARD 57-43-00-1 & SRM 57-43-01-2R.

Part: BEARING — WORN (THROTTLE DRUM) · airframe 66,763 hrs · 17,767 cycles

STIFF THROTTLE ON NR 1 ENG, WOULD NOT HOLD AUTO THROTTLES ENGAGED. FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R ALL BEARINGS IN LT PYLON THROTTLE STRUT DRUM ASSEMBLY. ACFT FLEW 4.5 HOUR FCF WITH NO REPEAT. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: DETECTOR — FAULTY (LT ENGINE) · airframe 66,734 hrs · 17,760 cycles

CREW REPORTED DURING FUNCTIONAL FLIGHT CHECK FOR LT THROTTLE BINDING THEY RECEIVED LT ENG OVERHEAT MSG. EMER DECLARED FLIGHT RETURNED & ACFT REMOVED FROM SERVICE. REPLACED LT ENG OVERHEAT DETECTOR ASSEMBLY TS5064 & TS5065. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: CLUTCH — INOPERATIVE (AUTOTHROTTLE SYS) · airframe 66,617 hrs · 17,722 cycles

LEFT ENG THROTTLE BINDING WHEN PULLED BACK. CREW SHUTDOWN ENG SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT AUTO THROTTLE CLUTCH PACK.

Part: PUMP — MALFUNCTIONED (RT ENGINE) · airframe 65,698 hrs · 17,488 cycles

CREW REPORTED RT CTR FUEL PUMP LIGHT ILLUMINATED WITH ASSOCIATED EICAS MSG. APPROX 30 MINUTES LATER RT ENG BEGAN SURGING. RT ENG BLEED LIGHT ILLUMINATED WITH EICAS MSG & STATUS MSG FOLLOWED, RT ENG SPEED CARD. EMER DECLARED RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. RESET RT CTR FUEL PUMP & REPLACED RT ENG SPEED CARD. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,760 hrs · 16,995 cycles

LT NR 2 DOOR EMERGENCY EXIT SIGN FAILED TO ILLUMINATE. REPLACED BATTERY PACK FOR LT NR 2 DOOR EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 63,652 hrs · 16,972 cycles

HNL INFLIGHT OGG-LAX CREW REPORTED RT ENGINE BLEED LIGHT ILLUMINATED ON TAKEOFF. EMERGENCY DECLARED FLIGHT DIVERTED HNL LANDED WITHOUT INCIDENT. PLACARDED RT PRESS REGULATING & SHUT OFF VLV INOPERATIVE IAW MEL. REPLACED RT REVERSE FLOW CONTROLLER AT LAX ON 11/14/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: PLATE — CORRODED (RT HORIZ STAB) · corrosion level 3 · airframe 60,640 hrs · 16,247 cycles

RIGHT LOWER HORIZONTAL STABILIZER PIVOT PLATE CORROSION AROUND FASTENER AT FORWARD INBOARD END. REMOVED CORROSION AND ACCOMPLISHED REPAIR PER EA B757-55-029242.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 58,095 hrs · 15,614 cycles

VVI - CREW REPORTED LEFT ENGINE INGESTED MEDIUM SIZE BIRD. EMERGENCY DECLARED, FLIGHT RETURNED VVI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT MIA ON 05/26/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT) · airframe 57,906 hrs · 15,547 cycles

LAX - CREW REPORTED LEFT ENGINE OIL BYPASS LIGHT ILLUMINATED THEN 15 MINUTES LATER HAD UNCOMMANDED SHUT DOWN (SINGLE ENGINE TIME 80 MINS). EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT LAX ON 04/23/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,116 hrs · 15,347 cycles

ROWS 9 TO 16 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY BATTERY PACK FOR ROWS 9 TO 16 EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,588 hrs · 15,212 cycles

FLOORBEAM STABILIZER STRAP WAS FOUND TO BE CRACKED. INSTALLED DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,588 hrs · 15,212 cycles

CRACKED STIFFENER ON FUSELAGE FRAME AT STATION 365 LEFT BUTTLINE 30. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-51-2R 1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,588 hrs · 15,212 cycles

FRAME AT STATION 1600 STRINGER 23 TO 25 LEFT CORRODED. ACCOMPLISHED NESTED ANGLES REPAIR PER SRM 53-00-07-2R-5 SHEET 8.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,588 hrs · 15,212 cycles

ACCIDENTAL IMPACT TO STATION 1640 RIGHT BUTTLINE 56. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-70-13-0G.

Part: PAN — GOUGED (L2 DOOR) · airframe 56,588 hrs · 15,212 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,248 hrs · 15,133 cycles

EMERGENCY LIGHTS FOR UPPER RIGHT AFT CABIN ARE INOPERATIVE. REPLACED BATTERY PACK M736. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,198 hrs · 14,882 cycles

SIDE EXIT SIGN ON RIGHT AFT OVERWING DOOR INOPERATIVE. REPLACE BATTERY PACK FOR SIDE EXIT SIGN ON RIGHT AFT OVERWING DOOR. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,160 hrs · 14,177 cycles

SEAT MOUNTED ESCAPE PATH LIGHTS FORWARD SECTION OF COACH INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD SECTION OF COACH, OPS CHECKED NORMAL.

Part: PRESSURE SWITCH — FAULTED (ZONE 500) · airframe 51,672 hrs · 14,069 cycles

HNL - CREW REPORTED LEFT CENTER FUEL LOW PRESSURE LIGHT ILLUMINATED IN CRUISE ON OVERHEAD AND NO ASSOCIATED EICAS MESSAGE. EMERGENCY DECLARED RETURNED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT FUEL LOW PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — FAILED (CABIN) · airframe 49,758 hrs · 13,624 cycles

EMERGENCY LIGHTS AT SEAT ROWS 17D TO 26D INOPERATIVE. REPLACED BATTERY PACK AND CHARGER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,866 hrs · 13,410 cycles

EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP AT SEAT 36D. OPS CHECKED NORMAL.

Part: FAN — FAILED (CABIN) · airframe 48,639 hrs · 13,346 cycles

PTY - CREW REPORTED ELECTRICAL ODOR IN CABIN AFTER UNKNOWN THUMP WAS FELT. EMERGENCY DECLARED, RETURNED TO PTY WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT RECIRCULATION FAN AT MIA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,364 hrs · 13,281 cycles

DFW - EMERGENCY LIGHT AT SEAT 18D AND 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEATS 18D AND 22D.

Part: WIRE — BROKEN (ENTERTAIN SYS) · airframe 48,220 hrs · 13,242 cycles

MCO - SHORTLY AFTER TAKEOFF ELECTRICAL SMELL NOTICED IN FORWARD COACH AREA. EMERGENCY DECLARED AND RETURNED MCO WITHOUT INCIDENT. PERFORMED INSPECTION OF CABIN AND FOUND SMELL COMING FROM NUMBER FOUR ENTERTAINMENT MONITOR. FOUND CHAFED AND BROKEN WIRE ON CONNECTOR TO MONITOR. REPAIRED WIRE ON CONNECTOR FOR MONITOR NUMBER FOUR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — INOPERATIVE (LT ENGINE) · airframe 47,820 hrs · 13,154 cycles

LAX - AIRCRAFT EXPERIENCED A LEFT HYDRAULIC SYSTEM FAILURE AFTER TAKEOFF. EMERGENCY DECLARED RETURNED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT PYLON ENGINE DRIVEN PUMP HYDRAULIC MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,862 hrs · 12,688 cycles

CHANNEL CORRODED AT GALLEY MOUNT, REPLACED CHANNEL IAW SRM 53-00-51.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,862 hrs · 12,688 cycles

AFT LAVATORY MOUNT CORRODED, REPLACED LAVATORY MOUNT FITTING IAW SRM 51-10-02.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,862 hrs · 12,688 cycles

LAVATORY MOUNT FITTING CORRODED. REPLACED MOUNT FITTING IAW SRM 51-10-02.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,862 hrs · 12,688 cycles

CORROSION ON LAVATORY MOUNT FITTING RT SIDE AFT LAVATORY, REPLACED FITTING IAW SRM 51-00-02.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,862 hrs · 12,688 cycles

LAVATORY MOUNT CORRODED, RERLACED MOUNT IAW SRM 51-10-02

Part: SKIN — DENTED (ZONE 100) · airframe 45,862 hrs · 12,688 cycles

FUSELAGE SKIN HAS DENT, REPAIRED DENT IAW SRM 53-00-01-2R.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,862 hrs · 12,688 cycles

CORROSION ON LAVATORY MOUNT LT SIDE OF AFT LAVATORY, REPLACED FITTING IAW SRM 53-00-51.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,862 hrs · 12,688 cycles

LAVATORY MOUNT FITTING CORRODED, REPLACED MOUNT FITTING IAW SRM 51-10-02.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,503 hrs

LAX SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 17 TO 26 INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHTS AT SEAT ROWS 17 TO 26. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,476 hrs

LAX - EMERGENCY LIGHTS AT SEAT ROWS 17D TO 27D INOPERATIVE. FOUND SEAT 18D SHORTED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT SEAT ROWS 17D TO 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHAFT — DAMAGED (LT ENGINE)

IAH INFLIGHT T931/15SEP LAX TO MIA - NUMBER ONE ENGINE OIL LOSS. CREW PERFORMED IN FLIGHT SHUT DOWN OF NUMBER ONE ENGINE. SINGLE ENGINE TIME 18 MINUTES. LANDED IAH WITHOUT INCIDENT. FOUND NUMBER ONE ENGINE TOWER SHAFT AND HOUSING DAMAGED. REPLACED NUMBER ONE ENGINE ON 16 SEP 2007 AT IAH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CARD — INOPERATIVE (FIRE DECTECTION)

LAX - ON TAKEOFF ROLL, SLIGHT MOMENTARY RED LIGHT ON EICAS AT 300 FEET BOTH AFT CARGO AND FIRE WARNING LIGHTS ILLUMINATED AND LEFT ENGINE OVERTEMP LIGHT ILLUMINATED. LIGHTS EXTINGUISHED AFTER ONE MINUTE. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FLIGHT DATA RECORDER DOWNLOAD REVEALED NO ENGINE OVERTEMP. REPLACED FIRE TEST PANEL AND FIRE DETECTION LOGIC CARD M10427. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (NLG)

SFO INFLIGHT T0392/29MAR - NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRUCK — FAILED (LT MLG)

ON TAXI OUT, LEFT MAIN LANDING GEAR BOGIE TRUCK FAILED. AIRCRAFT UNABLE TO MOVE FROM TAXIWAY. NO EMERGENCY DECLARED. REPLACED BOGIE ASSEMBLY FOR LEFT MLG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 17 INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT ASSEMBLY AT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 17D BROKEN. REPLACED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LEAD — CORRODED (CABIN)

SFO - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CORROSION OFF OF GROUND LEAD OF LAMP HOUSING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (R2 DOOR)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COOLING FAN — FAILED (E/E BAY)

TPA - FLT 2199 - AT FL390 IN CRUISE STRONG ELECTRICAL ODOR OCCURRED IN COCKPIT AND CABIN. DECLARED AN EMERGENCY DIVERTED TO TAMPA. ACCOMPLISHED APPROPRIATE EMERGENCY PROCEDURES AT FIRST SIGN OF SMELL. LANDED NORMALLY IN TPA. REPLACED NR 2 AFT EQUIP COOLING FAN. OPS CHECK NORMAL.

Part: SOLENOID — DEFECTIVE (MLG)

DFW - FLT 2030 - EN ROUTE DFW-GSO, AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED ANTI-RETRACTION SOLENOIDS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DEFECTIVE (R1 DOOR)

SJC - WHILE ON GROUND, R1 DOOR INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS AT FORWARD PART OF MAIN CABIN INOPERATIVE.