N622AA

Part: TRANSMITTER — INOPERATIVE (TE FLAP) · airframe 71,658 hrs · 24,788 cycles

DFW CREW REPORTED SPLIT FLAP INDICATION ON THE FLIGHT DESK. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT OTBD FLAP POSITION TRANSMITTER. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: MODULE — LEAKING (ANTI-SKID SYS) · airframe 71,587 hrs · 24,764 cycles

DFW INFLIGHT SFO-MIA. CREW REPORTED RT HYD QUANTITY LOSS INFLIGHT. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT & RT ANTI SKID SHUTTLE VLV MODULES. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 70,663 hrs · 24,419 cycles

RSW CREW REPORTED ELECTRICAL ODOR IN AFT CABIN. EMERGENCY DECLARED, FLIGHT RETURNED RSW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SEVERAL LEAKS IN AUXILIARY POWER UNIT BLEED DUCT IN AFT CARGO. REPLACED DUCT AT STATION 1520. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 70,189 hrs · 24,243 cycles

LEFT NR 3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 3 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: FITTING — DAMAGED (NR 3 PYLON) · airframe 69,236 hrs · 23,907 cycles

NUMBER 1 ENGINE PYLON, 3 SHEARED FASTENERS ON INBOARD AFT HINGE THRUST REVERSER FITTING. INSTALLED DOUBLER PER EA B757-54-027263.

Part: INDICATOR — FAILED (COCKPIT) · airframe 68,530 hrs · 23,659 cycles

MIA - CREW REPORTED STANDBY ATTITUDE INDICATION FAILED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED STANDBY ATTITUDE INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 67,471 hrs · 23,274 cycles

LEFT OVERWING EMERGENCY INOPERATIVE. REPLACED LAMP FOR LEFT OVERWING EMERGENCY. OPS CHECK NORMAL.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 66,524 hrs · 22,939 cycles

LIGHTNING STRIKES STATIONS 297 TO 310. ACCOMPLISHED DOUBLER REPAIR PER EA 020861.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,524 hrs · 22,939 cycles

AFT G4 GALLEY - RIGHT AFT FLOOR MOUNT CORRODED. INSTALLED NEW MOUNT PER SRM 51-10-02-0G.

Part: TRUSS — DAMAGED (FUSELAGE) · airframe 66,524 hrs · 22,939 cycles

HOLE DRILLED IN RADIUS OF TRUSS ON LEFT SIDE JUST AFT OF LEFT NUMBER 1 DOOR WAY. INSTALLED TRUSS ON LEFT SIDE STATIONS 380 TO 400 LEFT BUTTLINE 65 PER SRM 51-10-02-0G AND 51-40-02-0G.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,524 hrs · 22,939 cycles

AFT G4 GALLEY - AFT LEFT FLOOR MOUNT CORRODED. REPLACED MOUNT PER SMR 51-10-02-0G.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,524 hrs · 22,939 cycles

AFT G4 GALLEY - CENTER FLOOR MOUNT CORRODED. REPLACED CENTER MOUNT PER SRM 51-10-02-0G.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,524 hrs · 22,939 cycles

CABIN, BETWEEN STATIONS 395 AND 418, LEFT SIDE CREASE ANGLE CRACKED. INSTALLED CREASE ANGLE SPLICE REPAIR AT STATIONS 395 TO 418 PER AARD 53-10-13-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,524 hrs · 22,939 cycles

AFT MAIN DECK Z-ANGLE CORRODED AT RIGHT BUTTLINE 60 BETWEEN STATIONS 1700 TO 1720. INSTALLED NEW Z-ANGLE PER SRM 51-10-02-0G.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 66,524 hrs · 22,939 cycles

AFT MAIN DECK REPAIR DOUBLER DOES NOT CONTINUE UNDER THE 1720 LEFT ANGLE BETWEEN LEFT BUTTLINE TO RIGHT BUTTLINE 64. DOUBLER INSTALLED PER SRM 53-60-51-2 REPAIR 2 AND EA B757-53-020644.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 66,524 hrs · 22,939 cycles

AT STATION 330, OUTBOARD VERTICAL SIDE OF FLOORBEAM HAS TOOLING DAMAGE. REMOVED OF DAMAGED WEB AND INSTALLED OF NEW WEB PER SRM 51-40-02-0G.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 66,524 hrs · 22,939 cycles

APPROXIMATE STATION 1715 LEFT BUTTLINE 34, T-ANGLE DAMAGED. INSTALLED NEW SUPPORT T-ANGLE PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,524 hrs · 22,939 cycles

AFT MAIN DECK Z-ANGLE CORRODED AT STATIONS 1700 TO 1720 AND LEFT BUTTLINE 60 WATERLINE 208. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02-0G.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 66,524 hrs · 22,939 cycles

RIGHT NUMBER 2 DOOR INNER CHORD AT THE UPPER HINGE CUTOUT IS CRACKED. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 52-10-02-2R 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,524 hrs · 22,939 cycles

FLOORBOARD SUPPORT CORRODED FROM STATIONS 1661 TO 1681 LEFT BUTTLINE 2. REPLACED FLOORBOARD SUPPORT PER SRM 51-10-02-0G.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 66,524 hrs · 22,939 cycles

EXCESSIVE BLEND OUT ON FLOORBOARD SUPPORT AT SEAT TRACK NUMBER 3 AND STATION 330. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-40-02-0G AND EA B757-53-020744.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,524 hrs · 22,939 cycles

CORROSION ON 1640 FLOORBEAM FROM LEFT BUTTLINE 30 TO RIGHT BUTTLINE 12. ACCOMPLISHED NESTED ANGLES REPAIR PER SRM 53-00-51-2R AND EA 020601.

Part: HOUSING — DISCONNECTED (CABIN) · airframe 63,747 hrs · 21,935 cycles

FORWARD ENTRY AREA CENTER EMERGENCY LIGHT L26 INOPERATIVE. RESTORED CONNECTION ON BACK OF HOUSING ASSEMBLY. OPS CHECK NORMAL

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,747 hrs · 21,935 cycles

AFT RIGHT ENTRY DOOR EXTERIOR EMERGENCY LIGHT L6O IS INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER 4 DOOR. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 63,747 hrs · 21,935 cycles

LEFT AFT OVERWING EXIT MARKER, EMERGENCY LIGHT, DECAL IS DAMAGED. REPLACED AFT OVERWING LEFT SIDE EXIT MARKER DECAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,747 hrs · 21,935 cycles

AFT CARGO DOOR, EXTERIOR EMERGENCY LIGHT L569 IS INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT CARGO DOOR. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,747 hrs · 21,935 cycles

FORWARD ENTRY AREA, CENTER EMERGENCY LIGHT L26, LOWER ROW OF LAMPS ARE INOPERATIVE. REPLACED LAMPS. OPS CHECK NORMAL.

Part: PROBE — FAULTY (RT ENGINE) · airframe 63,220 hrs · 21,750 cycles

MIA - CREW REPORTED RIGHT ENGINE PROBE HEAT MESSAGE ON LOWER EICAS. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE RIGHT ENGINE PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SERVO — LEAKING (AILERON) · airframe 59,248 hrs · 20,332 cycles

CENTER HYDRAULIC RESERVOIR LIGHT AND CENTER HYDRAULIC QUANTITY EICAS MESSAGE WITH AN INDICATION OF .38RF CENTER QUANTITY. PRESSURE WAS STABLE AT 2890 TO 2910 POUNDS PER SQUARE INCH. BOTH QUANTITY AND PRESSURE REMAINED UNCHANGED THROUGHOUT APPROACH AND LANDING ON SHORT FINAL. THERE WAS A PRONOUNCED ROLL TO THE RIGHT. ALL FLIGHT CONTROL INDICATIONS WERE NORMAL. LEFT AILERON WAS REQUIRED UNTIL LANDING. LANDED DFW WITHOUT INCIDENT. REPLACED CENTER SYSTEM PILOT AILERON SERVO. SERVICED CENTER HYDRAULIC SYSTEM WITH NO LEAKS FOUND. REPLACED CENTER HYDRAULIC FLUID QUANTITY TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: TRANSMITTER — FAULTED (LE SLAT) · airframe 59,248 hrs · 20,332 cycles

RNO - ON APPROACH FLIGHT RECEIVED INDICATION OF TRAILING EDGE FLAP ASYMMETRY PROBLEM. ACCOMPLISHED A GO AROUND. LANDED RNO WITHOUT INCIDENT. REPLACED NUMBER ONE SLAT TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DIRTY (FLAP TRANSMITTER) · airframe 59,137 hrs · 20,292 cycles

JFK - PILOT REPORTED ON APPROACH FLAP INDICATOR FAILED. AIRCRAFT ABORTED APPROACH AND COMPLETED GO-AROUND. LANDED JFK WITHOUT INCIDENT. INSPECTED AIRCRAFT AND DETERMINED FAULT WAS AN INDICATION ISSUE. CLEANED RIGHT FLAP TRANSMITTER CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,141 hrs · 20,293 cycles

LEFT CREASE BEAM FLOORBOARD SUPPORT CORRODED. REPAIRED IAW AARD 53-30-13 AND EA B757-53-005221.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,047 hrs · 19,901 cycles

DENT IN FUSELAGE AFT OF LEFT NR 4 PASSENGER/SERVICE DOOR AND ABOVE STRINGER 15 LEFT. REPAIRED IAW SRM 53-00-01-2R IN CONJUNCTION WITH EA B757-53-005160, DOUBLER INSTALLED.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 18DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 18DEF BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT EXIT PLACARD AT AFT LEFT OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT AT AFT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 2EF BULLNOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 2EF BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT EXIT PLACARD AT FORWARD LEFT OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT AT FORWARD LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 36D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DISCHARGED (L4 DOOR)

SFO LT NR 4 DOOR EMERGENCY SLIDE BOTTLE PRESSURE NOT IN GREEN ZONE. REPLACED EMERGENCY SLIDE FOR LT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

DFW SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 9D AND FORWARD INOPERATIVE. REPLACED THE FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — NOT SEATED (CABIN)

SFO - EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RESEATED CONNECTOR FOR INSEAT EMERGENCY ESCAPE PATH LIGHT AT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — CRACKED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT CRACKED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (LT WING)

TUL - FOUND 3 INCH BY 15 FT OF CORROSION ON LEFT WING SKIN SURFACE (UPPER) 1 INCH OUTBOARD OF WING TO BODY FAIRING ALONG BLACK STRIPE. SEE ESO 90309 DATED 5/16/2001. (M)

Part: SPAR — CORRODED (RT WING)

TUL - FOUND CORROSION AT RIGHT WING AFT SPAR BOOST PUMP LOWER BOND JUMPER AREA. REPAIR PER ESO 90309 DATED 05-15-2001. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON HORIZONTAL CHORD ANGLE AT STATION 1180 LEFT W/W. REPAIR PER SRM 51-70-11-0 AND ESO90309 DATED 5-15-2001. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN DAMAGE EITHER SIDE OF STRINGER 17 AND STATION 1720 TO 1730. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-00-01-2. (M)

Part: LIGHT — INOPERATIVE (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DEFECTIVE (L1 DOOR)

LGA- WHILE ON GROUND L1 DOOR INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAL — LEAKING (ENTRY DOOR)

SJU - FLT 674 - EN ROUTE SJU-EWR, DETECTED AIR LEAK AT FORWARD ENTRY DOOR. RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT. RE-SECURED COSMETIC SEAL AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (SEAT 9B)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 9B INOPERATIVE. RECONNECTED CONNECTOR UNDER SEAT 9B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SOCKET — CORRODED (R4 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, R4 EXTERIOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTNEANCE FOUND COROSION ON LIGHT SOCKET. CLEANED CORRODED SOCKET AND RELAMPED BULB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SOCKET — CORRODED (EMERGENCY EXIT)

DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE FOUND CORROSION ON LIGHT SOCKET. CLEANED CORRODED SOCKET. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIPS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EXHAUST FAN — DEFECTIVE (E/E COMPT)

SJU - FLT T0672 - EN ROUTE STT/MIA DURING CRUISE, CABIN CREW REPORTED ELECTRICAL FUME SMELL IN CABIN. SMOKE DETECTORS IN FORWARD, MID, AND AFT CABIN LAVATORIES SOUNDED. AIRCRAFT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 AFT EQUIPMENT VENTILATION FAN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)