N655AA

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 68,355 hrs · 23,564 cycles

MCO CREW REPORTED CAPTAIN`S FRONT OUTER WINDSHIELD CRACKED. EMERGENCY DECLARED. FLIGHT LANDED MCO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT NR 1 WINDOW ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,177 hrs · 23,500 cycles

LT NR 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: O-RING — WORN (HYDRAULIC SYS) · airframe 67,649 hrs · 23,320 cycles

SJU INFLIGHT MIA-BGI CREW REPORTED CENTER HYDRAULIC SYSTEM QUANTITY SLOWLY DECREASING. FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HYDRAULIC PUMP B-NUT LEAKING. REPLACED 0-RING. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SIGN — BROKEN (CABIN) · airframe 67,647 hrs · 23,319 cycles

RT NR 4 DOOR EMERGENCY EXIT SIGN LIGHT ASSEMBLY BROKEN OFF WALL. REPLACED EMERGENCY EXIT LIGHT SIGN ASSEMBLY AFT OF RT NR 4 DOOR. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — DEFECTIVE (LT GENERATOR) · airframe 63,300 hrs · 21,735 cycles

JFK - CREW REPORTED LEFT GENERATOR TRIPPED AND CAUSED MULTIPLE STATUS MESSAGES. LEFT INTEGRATED DRIVE GENERATOR UNABLE TO BE RESET BY FLIGHT CREW. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONNECTOR D1116P AND LEFT GENERATOR FEEDER CABLE FROM INTEGRATED DRIVE GENERATOR TO D1016J. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — DENTED (FUSELAGE) · airframe 61,408 hrs · 21,034 cycles

DENT IN FRAME STATION 1580 LOWER CARGO AREA. INSTALLED DOUBLER PER SRM 53-00-07-2R.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

NUMBER 10 SLAT HAS CORROSION AROUND FASTENER HEAD APPROXIMATELY 2 INCHES FROM INBOARD END AT TOP OF OUTER SKIN. CUT OUT CORROSION, FABRICATED DOUBLER AND DRILLED HOLES FOR FASTENERS PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

RIGHT WING NUMBER 10 SLAT HAS CORROSION AROUND A FASTERNER HEAD APPROXIMATELY 42 INCHES FROM INBOARD END AT TOP OF OUTER SKIN. INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

RIGHT WING NUMBER 10 SLAT HAS CORROSION AROUND A FASTENER HEAD APPROXIMATELY 64 INCHES FROM OUTBOARD END AT TOP OF OUTER SKIN. CUT OUT CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

NUMBER 2 SLAT SKIN CORRODED AT OUTBOARD MAIN TRACK 2 PLACES. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

LEFT WING NUMBER 2 SLAT HAS CORROSION AROUND FASTENERS HEADS AT THE / INBOARD MAIN TRACK APPROXIMATELY 44 INCHES FROM INBOARD END OF THE OUTER SKIN. REMOVED CORROSION INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

CORROSION AROUND RIVET ON LEADING EGDE OF NUMBER 7 SLAT. REMOVED CORRODED AREA OF SKIN AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

FRAME AT STATION 686 RIGHT SIDE 3 INCHES ABOVE FLOORLINE CORRODED. INSTALLED FRAME REPAIR DOUBLER PER SRM 51-70-11-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

INBOARD CHORD OF CREASE ANGLE CORRODED STATIONS 742 TO 746 RIGHT SIDE. REPLACED INBOARD CHORD OF CREASE ANGLE PER SRM 51-10-02-0G.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

STATION 1635 RIGHT BUTTLINE 47 AFT OUTBOARD LAVATORY MOUNTS CORRODED. REPLACED LAVATORY MOUNTS PER SRM 51-10-02-0G.

Part: SKIN — GOUGED (FUSELAGE) · airframe 61,408 hrs · 21,034 cycles

GOUGE IN FUSELAGE SKIN, STATIONS 1080 TO 1100 BETWEEN STRINGERS 1 AND 2 RIGHT. AREA BLENDED AND POLISHED TO REMOVE DAMAGE PER SRM 53-00-01-1A1 AND PER EA B757-53-016919.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 61,408 hrs · 21,034 cycles

NUMBER 2 CARGO DOOR AFT LOWER CORNER SEAL LANDING IS DAMAGED. REMOVED AND REPLACED AFT LOWER CORNER SEAL LANDING PER ESO 90121.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

CREASE ANGLE AT STATION 780 LEFT SIDE CORRODED. REMOVED AND REPLACED CREASE ANGLE LEFT SIDE STATION 780 PER SRM 53-30-13-1.

Part: DOOR FRAME — CORRODED (L4 DOOR) · corrosion level 2 · airframe 61,408 hrs · 21,034 cycles

CORROSION ON LOWER FORWARD CORNER VERTICAL FRAME OF LEFT NUMBER 4 DOOR. INSTALLED DOUBLER AND FILLER PER EA 757-53-017328.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 61,047 hrs · 20,900 cycles

AFT RIGHT FLIGHT ATTENDANT JUMPSEAT RIGHT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,534 hrs · 20,387 cycles

EMERGENCY LIGHTS FROM SEAT 26D AT AFT DOOR TOO DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT 26D AT AFT DOOR. OPS CHECKED NORMAL.

Part: ENGINE — OIL CONSUMPTION (LEFT) · airframe 58,730 hrs · 20,099 cycles

IAD - INFLIGHT MIA-LGA. CREW REPORTED LEFT ENGINE OIL QUANTITY WAS STEADILY DECREASING. FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DUE TO REPEATS OF HIGH OIL CONSUMPTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 57,622 hrs · 19,706 cycles

RIGHT WING NUMBER 8 SLAT FASTENER 45 INCHES OUTBOARD FROM INBOARD END HAS CORROSION AROUND HEAD. INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.

Part: COVER — MISSING (CABIN) · airframe 56,576 hrs

JFK - EXIT SIGN AT AFT OF RIGHT NUMBER ONE DOOR MISSING COVER. REPLACED COVER FOR EXIT SIGN AT AFT OF RIGHT NUMBER ONE DOOR.

Part: LENS — BROKEN (CABIN)

DFW EMERGENCY LIGHT AT SEAT 28D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED BATTERY PACK AT MID CABIN OVERHEAD FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BOTTLE — INOPERATIVE (SLIDE)

LAS LEFT NUMBER ONE SLIDE WAS NOT DISARMED AND DOOR WAS OPEN FROM INSIDE. SLIDE DID NOT DEPLOY. FELL ON AIR STAIRS. DOOR ASSIST BOTTLE EXPENDED. REINSTALLED SLIDE WITH NEW DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GENERATOR — INOPERATIVE (RT ENGINE)

MIA INFLIGHT T687/03SEP - RIGHT ENGINE SPEED CARD STATUS MESSAGE ILLUMINATED. RIGHT CENTER FUEL LOW PRESSURE AND RIGHT N3 FLUCTUATING 60 TO 80 WITH RIGHT ENGINE BLEED OFF LIGHT. REPLACED N2 SPEED CARD AND N3 TACH GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT OVERHEAD BIN BETWEEN SEAT ROWS 12ABC AND 13ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD BIN BETWEEN SEAT ROWS 12ABC AND 13ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: EEC — INOPERATIVE (RT ENGINE)

BDA - POWER ON RIGHT HAND ENGINE. ENGINE PRESSURE RATIO GAUGE RISING AND N1, N2, AND N3 FUEL LOW DECREASING. ENGINE PRESSURE RATIO WENT BLANK N1, N2, AND N3 STILL RECORDING BUT NOT PRODUCING. REPLACED ENGINE PRESSURE RATIO TRANSMITTER. REPLACED RIGHT HAND ENGINE ELECTRONIC ENGINE CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PANEL — INOPERATIVE (COCKPIT)

MEX - PREFLIGHT INSPECTION FOUND EMERGENCY -DISARMED- LIGHT INOPERATIVE. FERRIED FLIGHT FROM MEX TO MIA FOR REPAIR OF EMERGENCY LIGHT SWITCH. REPLACED EMERGENCY LIGHT PANEL ON COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (WING)

TUL - FOUND UPPER WING SKIN CORRODED IN BLACK PAINTED AREA AT EMERGENCY EXIT PATH. BLENDED AREA. FLAPPER PEEN, REINSTALLED FASTENERS. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FOUND AFTER CORROSION REMOVAL, BEAM THICKNESS LESS THAN SRM LIMITS. REPAIR PER MRB 757-901. (M)

Part: DECK PLATE — CORRODED (BS 1701)

AFW - AFTER CORROSION REMOVAL, REMAINING THICKNESS BEYOND SRM LIMITS. REPAIR PER MRB 757-902. (M)

Part: BUSHING — WORN (RT MLG)

AFW - INSPECT RIGHT MLG BUSHING FOR MIGRATION. INSPECTION PER MRB 757-900. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - AFTER CORROSION REMOVAL, REMAINING THICKNESS IS BEYOND SRM LIMITS. REPAIR PER MRB 757-907. (M)

Part: FLOOR STRUCTURE — CORRODED (BS 370)

AFW - AFTER REMOVING CORROSION, REMAINING THICKNESS BEYOND SRM LIMITS. REPAIR PER MRB 757-903. (M)

Part: DOOR PAN — GOUGED (R4 DOOR)

AFW - FOUND DOOR HANDLE PAN GOUGED BEYOND SRM LIMITS. REPAIR PER MRB 757 909. (M)

Part: STRUT BUSHING — ROTATED (RT MLG GEAR)

AFW - RIGHT MLG LOWER SIDE STRUT SWIVEL UPPER BUSHING HAS ROTATED SLIGHTLY. TST: 13,691. CYCLES: 4,900. (X)