N634AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,308 hrs · 25,838 cycles

RIGHT NR 4 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK M00736, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,308 hrs · 25,838 cycles

EMERGENCY LIGHT AT SEAT 31D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31D, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,308 hrs · 25,838 cycles

EMERGENCY LIGHTS AT SEAT 29D, 33D, 36D & 16C INOPERATIVE. REPLACED BATTERY PACK M00737, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,097 hrs · 25,757 cycles

RT NR 3 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RT NR 3 DOOR, OPERATIONS CHECKED NORMAL.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,857 hrs · 25,325 cycles

AFT CARGO DOOR CORRODED ON THIRD "T" ANGLE AFT OF FORWARD DOOR FRAME AT LOWER EDGE BEAM. INSTALLED NEW "T" ANGLE IAW AARD 51-00-05-1.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,857 hrs · 25,325 cycles

AFT CARGO DOOR, FOURTH "T" ANGLE AFT OF FORWARD DOOR FRAME BEAM CORRODED. R&R FOURTH "T" ANGLE IAW AARD 51-00-05-1.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,857 hrs · 25,325 cycles

AFT CARGO DOOR, FIRST "T" ANGLE AFT OF DOOR FRAME AT LOWER EDGE BEAM CORRODED. R&R "T" ANGLE IAW AARD 51-00-05.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,857 hrs · 25,325 cycles

AFT CARGO DOOR, CORRODED ON THIRD WEB AFT OF DOOR FRAME AT LOWER EDGE BEAM. INSTALLED NEW WEB IAW 51-00-05-1.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,857 hrs · 25,325 cycles

AFT CARGO DOOR, CORRODED ON FIRST WEB AFT OF FORWARD DOOR FRAME AT LOWER EDGE BEAM. INSTALLED NEW WEB IAW AARD 51-00-05-1.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,857 hrs · 25,325 cycles

AFT CARGO DOOR, FOURTH WEB AFT OF FORWARD DOOR FRAME AT LOWER EDGE BEAM CORRODED. INSTALLED NEW WEB IAW AARD 51-00-05-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,975 hrs · 24,647 cycles

EMERGENCY EXIT SPOT LIGHT AT ROW 18ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SPOT LIGHT AT ROW 18ABC. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,975 hrs · 24,647 cycles

EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER 4 DOOR INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 68,937 hrs · 24,262 cycles

CORROSION ON NUMBER 9 SLAT UPPER SKIN AT MID SPAN. REMOVED DAMAGED AREA AND INSTALLED DOUBLERS PER AARD 57-43-00-1. INSTALLED COVE SKIN PER ESO 90249.

Part: DOOR — CRACKED (L2) · airframe 68,937 hrs · 24,262 cycles

LEFT NUMBER 2 DOOR UPPER HINGE CUTOUT CRACKED. INSTALLED REPAIR DOUBLER PER SRM 52-10-02R 1 AND EA COMP-52-024976.

Part: DOOR — CRACKED (R2) · airframe 68,937 hrs · 24,262 cycles

RIGHT NUMBER 2 DOOR HAS CRACK AT UPPER HINGE IN RADIUS. INSTALLED DOUBLER PER SRM 52-10-02-2R 1 AND EA COMP-52-024975.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 68,087 hrs · 23,949 cycles

FIRST CLASS CLOSET BULLNOSE OVERHEAD LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED NORMAL

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 68,087 hrs · 23,949 cycles

L4 DOOR ENTRY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 68,087 hrs · 23,949 cycles

R4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR. OPS CHECKED NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,237 hrs · 22,552 cycles

MAIN E&E CEILING INTERCOSTAL CRACKED AT T-CAP STATION 418 AT BUTTLINE 0. INSTALLED INTERCOSTAL TOP CAP AND SPLICE IAW SRM 51-70-12 AND EA B 757-53-015050, DATED 1/26/11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,058 hrs · 21,773 cycles

EMERGENCY LIGHT AT 34D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY AT SEAT 34D, OPS CHECKED NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,098 hrs · 21,066 cycles

CORROSION ON UPPER SURFACE OF SKIN 30 INCHES FROM INBOARD END. INSTALLED DOUBLER ON UPPER SURFACE PER SRM 57-43-01 AND AARD 57-43-00-1 MRT 022536.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 60,098 hrs · 21,066 cycles

SLAT NUMBER 4 DELAMINATED ON TRAILING EDGE WEDGE. REMOVED FOR REPAIR. INSTALLED NEW CORE AND DOUBLER UNDER SRM 51-70-10-2R.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,098 hrs · 21,066 cycles

CORROSION ON NUMBER 10 SLAT, 41 INCHES FROM OUTBOARD UPPER SURFACE. INSTALLED DOUBLER UNDER SRM 57-43-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,098 hrs · 21,066 cycles

CORROSION ON NUMBER 10 SLAT 30 INCHES FROM INBOARD BOTTOM SURFACE. INSTALLED DOUBLER UNDER SRM 57-43-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,098 hrs · 21,066 cycles

CORROSION ON NUMBER 10 SLAT, 30 INCHES FROM INBOARD UPPER SURFACE. INSTALLED DOUBLER UNDER SRM 57-43-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,098 hrs · 21,066 cycles

RIGHT WING NUMBER 10 SLAT HAS CORROSION ON UPPER SURFACE/REF E-58 5999524/FMR-63457FFAA. REMOVED CORROSION AND INSTALLED FLUSH-DOUBLER UNDER SRM-57-43-01-2 AT OUTBOARD SLAT-TRACK FITTING AREA.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,098 hrs · 21,066 cycles

NUMBER 7 SLAT HAS 2 CRACKS ON UPPER SKIN. REMOVED CORROSION INSTALLED DOUBLER UNDER SRM 57-43-01, MRT 022493 DWMS 1215532.

Part: DOOR — CRACKED (LE SLAT) · airframe 60,098 hrs · 21,066 cycles

NUMBER 9 SLAT INBOARD DRIVE TRACK DOOR IS CRACKED. REMOVED AND REPLACED TRACK DOOR PER ESO 90249. MRT 022468 MRR/SDR ACCOMP DWMS 1213681.

Part: SKIN — CRACKED (LE SLAT) · corrosion level 2 · airframe 60,098 hrs · 21,066 cycles

NUMBER 9 SLAT AT INBOARD DRIVE TRACK SKIN IS CRACKED AT FASTENER. MARKED, BLENDED PRIMED AND PAINTED PER ESO 90249. MRT 022470 AND MRR/SDR ACCOMP. DWMS1213690.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,098 hrs · 21,066 cycles

RIGHT WING NUMBER 9 SLAT HAS CORROSION ON UPPER SURFACE, REF: E58 5999523. REMOVED CORROSION, INSTALLED DOUBLER UNDER SRM 57-43-01.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,098 hrs · 21,066 cycles

NUMBER 9 SLAT AT OUTBOARD DRIVE TRACK SKIN IS CRACKED AT FASTENER. INSTALLED DOUBLER PER AARD 57-43-4. MRT 022467 MRR/SDR ACCOMP. DWMS 1213686.

Part: PAN — CRACKED (PAX DOOR) · airframe 60,098 hrs · 21,066 cycles

CRACK IN DOOR HANDLE BOX MRT 022447 DWMS1214553. INSTALLED NEW HANDLE BOX UNDER ESO 90283.

Part: TORQUE BOX — CRACKED (L4 DOOR) · airframe 60,098 hrs · 21,066 cycles

LEFT NUMBER FOUR PASSENGER ENTRY DOOR HANDLE TORQUE BOX CRACKED AT CAM BASKET MOUNT HOLE. REMOVED AND REPLACED HANDLE TORQUE BOX UNDER ESO 90108.

Part: TORQUE BOX — CRACKED (PAX DOOR) · airframe 60,098 hrs · 21,066 cycles

RIGHT NUMBER ONE PASSENGER ENTRY DOOR TORQUE BOX IS CRACKED AT CAM BASKET MOUNT HOLES. REMOVED AND REPLACED TORQUE BOX UNDER ESO 90284.

Part: PAN — CRACKED (R4 DOOR) · airframe 60,098 hrs · 21,066 cycles

RIGHT NUMBER FOUR PASSENGER ENTRY DOOR HANDLE BOX CRACKED. REMOVED AND REPLACED DOOR HANDLE BOX UNDER ESO 90108.

Part: PAN — DAMAGED (L2 DOOR) · airframe 60,098 hrs · 21,066 cycles

LEFT NUMBER 2 DOOR PASSENGER ENTRY OUTER HANDLE PAN HAS GROOVE WORN IN IT. REMOVED AND REPLACED PAN UNDER ESO 90282.

Part: PAN — GOUGED (L4 DOOR) · airframe 60,098 hrs · 21,066 cycles

LEFT NUMBER 4 PASSENGER ENTRY DOOR HANDLE PAN GOUGED. REMOVED AND REPLACED PAN PER ESO 90108.

Part: PRESSURE SWITCH — FAILED (HYDRAULIC SYS) · airframe 59,805 hrs · 20,965 cycles

AIRCRAFT AIR INTERUPT WITH LEFT HAND ENGINE HYDRAULIC PUMP LOW PRESS INDICATION. REPLACED HYDRAULIC LOW PRESS SWITCH AND HYDRAULIC FILTER. ACP OVERWEIGHT LANDING SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: PRESSURE SWITCH — DEFECTIVE (HYDRAULIC SYS) · airframe 59,802 hrs · 20,964 cycles

MIA - RIGHT ENGINE HYDRAULIC PRESSURE INDICATION ERRATIC. EMERGENCY DECLARED RETURNED MIA WITHOUT INCIDENT. REMOVED AND REPLACED LEFT HYDRAULIC SYSTEM PRESSURE SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,553 hrs

BOS - SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 26 AND AFT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON SEATS 26 AND AFT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,553 hrs

BOS - SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS.

Part: LIGHT — BROKEN (CABIN) · airframe 59,027 hrs

JFK - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 18D BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 18D.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,027 hrs

JFK - SEAT MOUNTED LIGHTS FROM SEATS 16D TO 26D INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED LIGHTS FROM SEATS 16D TO 26D.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 58,841 hrs

DFW - SEAT MOUNTED EMERGENCY PATH LIGHTING AT ROW 32DEF INOPERATIVE. REPAIRED CONNECTOR FOR SEAT MOUNTED EMERGENCY PATH LIGHTING AT ROW 32DEF.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 58,841 hrs

DFW - OVERWING AFT POSITION EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. REPLACED LAMP AT OVERWING AFT POSITION FOR EMERGENCY LIGHT.

Part: COVER — MISSING (EMERGENCY LIGHTS)

JFK - LEFT NUMBER FOUR DOOR EXIT SIGN COVER MISSING. REPLACED LENS ON LEFT NUMBER FOUR DOOR EXIT SIGN.

Part: CIRCUIT CARD — INOPERATIVE (FIRE DETECTION) · airframe 55,745 hrs

SJU INFLIGHT T809/09APR - CREW REPORTED NUMBER TWO ENGINE FIRE LOOP ONE STATUS MESSAGE DURING CLIMB. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. NO FIRE. REPLACED NUMBER TWO ENGINE FIRE LOOP ONE DETECTOR CARD M683. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ECU — INOPERATIVE (LT ENGINE)

MIA INFLIGHT T1047/16OCT - NUMBER ONE ENGINE GENERATOR FAILED AND CREW WAS UNABLE TO ESTABLISH POWER WITH AUXILLIARY POWER UNIT (APU). LANDED MIA WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ELECTRONIC CONTROL UNIT AND SERVICED INTEGRATED DRIVE GENERATOR. PLACARDED APU. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: CONTACT — DIRTY (CABIN)

MIA - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SJU - EMERGENCY LIGHTS AFT OF OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AFT OF OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - EMERGENCY LIGHTS FROM SEAT ROW 26 AFT INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS FROM SEAT ROW 26 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (HYD SYSTEM)

SJU - INFLIGHT T790/01 TWO MINUTES AFTER TAKEOFF LOST LEFT HYDRAULIC SYSTEM QUANTITY. MANUALLY EXTENDED GEAR AND FLAPS AND TURNED LEFT HYDRAULIC PUMPS OFF WHEN PRESSURE LIGHT ILLUMINATED. LANDED SJU WITHOUT INCIDENT. FOUND BRAKE METERING VALVE DAMPED. REPLACED RIGHT BRAKE METERING VALVE ASSEMBLY AND CHECKED LEFT SYSTEM HYDRAULIC FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — BROKEN (EMERGENCY LIGHT)

SFO - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 8DEF BROKEN. REPLACED LIGHT SOCKET FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 8DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

SFO EMERGENCY EXIT LIGHTS FROM AISLE SEAT 24D TO 34D INOPERATIVE. REPLACED BATTERY ABOVE RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

SFO EMERGENCY EXIT LIGHTS INOPERATIVE AT L4 AND R4. REPLACED BATTERY ABOVE RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY LIGHTS SEAT 24D AND AFT INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — DAMAGED (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING NEEDING REPLACED. REPLACED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — INOPERATIVE (COCKPIT)

DFW - COCKPIT EMERGENCY LIGHT UNARMED LIGHT INDICATION INOPERATIVE. REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT UNARMED SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING WIRE AT SEAT 23D IS PULLED LOOSE. REPLACED SEAT MOUNTED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — MALFUNCTIONED (ACM BAY)

LIT - FLT 405 - EN ROUTE BOS-DFW, DETECTED STRONG ELECTRICAL SMELL FROM SEAT ROW 4 THROUGH SEAT ROW 12. AIR INTERRUPTED, DIVERTED LIT AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE RECIRCULATION FAN. ACCOMPLISHED PACK BURNOUT PER THE MM. NO SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 1640)

AFW - FLOORBEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND LIMITS. BLEND OUT CORROSON AND REFINISH THE SRM. FILL BLENDS ON THE UPPER HORIZONTAL FLANGE SURFACE WITH BM55-95 SEALANT. (M)

Part: SILL — CORRODED (BS 1420)

AFW - AFT CARGO DOOR LOWR SILL T-CHORD HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT THE CORROSION AND RE-FINISHED THE SURFACE FILLED BLENDS ON THE UPPER HORIZONTAL FLANGE SURFACE WITH BMS 5-95 SEALANT. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FLOOR BEAM AT STATION 377 HAS CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-625. (M)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - FLOOR BEAM AT STATION 324, HAS CORROSION REMOVED ON UPPER SURFACE, MATERIAL REMAINING IS BEYOND SRM LIMITS. PER MRB 757-623. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STATION 1640 HAS 3 AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-620. (M)

Part: DECK PLATE — CORRODED (BS 1681)

AFW - SEVERAL AREAS OF DECK PLATE HAS CORROSION BEYOND SRM LIMITS. PER MRB 757-619. (M)

Part: ANGLE — CORRODED (CABIN)

AFW - CORROSION REMOVED FROM ANGLE AT L-1 DOOR FLOOR BEYOND LIMITS. PER MRB 757-622. (M)