N642AA

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 70,525 hrs · 24,975 cycles

NR 1 PYLON, INBD MID BULKHEAD HALF WAS BEING REPLACED DUE TO CRACK. THE FWD FASTENER HOLE COMMON TO THE MID BULKHEAD & THE LOWER SPAR CHORD WAS FOUND TO BE AT .415 INCHES WHICH IS BEYOND THE LIMITS SPECIFIED IN SB 757-54A0039 OF .3911INCHES MAXIMUM. ENGINEERING AUTHORIZATION B757-54-033265 DATED 01/17/2014 WAS ISSUED TO INCREASE THE HOLE SIZE TO .4990 INCHES. INSTALLED A FREEZE PLUG IN THE LOWER SPAR CHORD & INSTALLED FASTENER.

Part: DOOR — CRACKED (CABIN) · airframe 70,525 hrs · 24,975 cycles

LT NR 2 DOOR UPPER HINGE CUT OUT IS CRACKED. INSTALLED DOUBLER REPAIR IAW SRM 52-10-02-2R-1 & EA COMP 52-033189.

Part: FITTING — WORN (LT WING) · airframe 70,525 hrs · 24,975 cycles

BOTH LT HAND SIDE LOAD FITTINGS, INBD & OTBD FACES, HAD WEAR FROM THE MID STRUT BUSHINGS AT THE PYLON ATTACH POINT. REWORKED & BLENDED AREAS IAW EA B757-57-033230.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 67,560 hrs · 23,893 cycles

ROW 18DEF EMERGENCY LIGHTS INOPERATIVE. INSTALLED SERVICEABLE SIDEWALL CONNECTOR, OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,202 hrs · 23,411 cycles

REPLACED EXISTING REPAIR AT STATION 400 AND STRINGER 15 RIGHT. REPLACED WITH NEW DOUBLER REPAIR PER SRM 53-00-01-2R2 AND EA B757-53-023792.

Part: FSEU — INOPERATIVE (TE FLAP) · airframe 65,033 hrs · 22,968 cycles

CREW REPORTED ON APPROACH WHEN FLAPS WERE MOVED TO 25 FROM 20 TRAILING EDGE FLAP 95YM MESSAGE. ACCOMPLISHED GO AROUND. WHEN FLAPS WERE MOVED BACK 20 MESSAGE DISSAPEARED. FLIGHT LANDED MIA WITHOUT INCIDENT. FOUND NUMBER 1 CONTROLLER AT FAULT. REPLACED NUMBER 1 FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — LOOSE (CABIN) · airframe 64,654 hrs · 22,824 cycles

EMERGENCY LIGHT WIRE AT SEAT 28D NOT SECURE. SECURED WIRE FOR EMERGENCY LIGHT AT SEAT 28D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,654 hrs · 22,824 cycles

EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 1ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 1ABC.

Part: LIGHT — MISSING (CABIN) · airframe 64,654 hrs · 22,824 cycles

PROXIMITY EMERGENCY LIGHT IS MISSING LAMP. REPLACED LAMP FOR PROXIMITY EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,654 hrs · 22,824 cycles

EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 13ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 13ABC.

Part: WIRE — LOOSE (CABIN) · airframe 64,654 hrs · 22,824 cycles

EMERGENCY LIGHT WIRE AT SEAT 19B NOT SECURE. SECURED WIRE FOR EMERGENCY LIGHT AT SEAT 19B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,534 hrs · 22,775 cycles

SEAT 20D EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 20D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 64,534 hrs · 22,775 cycles

SEAT 24D EMERGENCY LIGHT MISSING LENS. REPLACED LENS FOR SEAT 24D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,888 hrs · 21,811 cycles

LOWER FUSELAGE SKIN HAS DEEPLY BLENDED AREA STATION 490 AT 29 LEFT. INSTALLED DOUBLER LOWER FUSELAGE STATION 490 STRINGER 29L LEFT PER SRM 53-00-01-2R 3 AND EA B757-53-014368.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,888 hrs · 21,811 cycles

FRAME STATION 700 LEFT BUTTLINES 0 TO 70.5 CRACKED. REPLACED BEAM PER SRM 53-00-51-2, REPAIR NUMBER 3, WITH AARD 53-30-51-2 REPAIR 2, BY THE COMPLETING OF TASK CARD 53-98-01, STEPS 1 THROUGH 76.

Part: PAN — GOUGED (R2 DOOR) · airframe 61,888 hrs · 21,811 cycles

RIGHT NUMBER 2 DOOR HANDLE PAN GOUGED. RIGHT NUMBER 2 DOOR NEW HANDLE PAN INSTALLED PER ESO 90282.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,888 hrs · 21,811 cycles

FLOORBEAM CORRODED AT STATION 377.7 AND RIGHT BUTTLINE 54. REPAIRED LATERAL FLOORBEAM AT STATION 377.7 AT RIGHT BUTTLINE 47 TO RIGHT BUTTLINE 70 PER IAW SRM 53-00-51-2R 3.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,888 hrs · 21,811 cycles

BETWEEN STATIONS 1420 TO 1440 BELOW THE CABIN FLOOR THE INTERCOSTAL AT BUTTLINE 0 TOP "L" ANGLE IS CRACKED OUT. INSTALLED SERVICEABLE INTERCOSTAL TOP ANGLE A STATIONS 1420 TO 1440 BUTTLINE 0, WATERLINE 208, PER IAW SRM 51-10-02-0G PARAGRAPH 9 AND 10.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,888 hrs · 21,811 cycles

CORROSION ON CREASE ANGLE AT APROXIMATELY STATION 757 LEFT BUTTLINE 67. INSTALLED SPLICE REPAIR TO CREASE ANGLE PER AARD 53-30-13-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,888 hrs · 21,811 cycles

CORROSION AT CREASE ANGLE ON RIGHT SIDE AT STATION 440. REPLACED CREASE ANGLE ON RIGHT SIDE AT STATION 440 PER AARD 51-10-05 REPAIR NUMBER 1 BOEING REF DRAWING NUMBER 141N8322.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,888 hrs · 21,811 cycles

CORROSION ON CREASE ANGLE AT LEFT NUMBER 2 DOOR THRESHOLD, FRAME STATIONS 690 TO 760, LEFT BUTTLINES 63 TO 65, WATERLINE 208, STRINGER 17 LEFT. REMOVED AND REPLACED CREASE ANGLE LOCATED AT FRAME STATIONS 690 TO 760, LEFT BUTTLINES 63 TO 65, WATERLINE 208, STRINGER 17 LEFT PER SRM 51-10-02-0G, PARAGRAPH 10.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,888 hrs · 21,811 cycles

LARGE AREA OF CORROSION JUST FORWARD OF STATION 760, RIGHT SIDE, INNER CHORD OF CREASE BEAM. INSTALLED CREASE BEAM AND SPLICE STATIONS 756 TO 810 PER AARD 53-30-13-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,888 hrs · 21,811 cycles

TEMPORARY REPAIR INSTALLED BELOW FIRST WINDOW CUT-OUT STRINGER 16 RIGHT SIDE BETWEEN STATIONS 400 AND 420. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-00-01-2R AND SRM 51-40-02-0G.

Part: PLACARD — DAMAGED (CABIN) · airframe 61,860 hrs · 21,800 cycles

RIGHT SIDE OVERWING EXIT MARKER DECALS DAMAGED. REPLACED DECALS. OPS CHECK NORMAL.

Part: PIN — BROKEN (CABIN) · airframe 61,860 hrs · 21,800 cycles

SEAT 27D EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN PIN. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 61,860 hrs · 21,800 cycles

LEFT SIDE OVERWING EXIT MARKER DECAL DAMAGED. REPLACED DECALS. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,527 hrs · 21,677 cycles

BULLNOSE EMERGENCY LIGHT AT 12ABC. REPLACED LAMP FOR BULL NOSE EMERGENCY LIGHT AT 10ABC. OPS CHECKS NORMAL.

Part: SWITCH — FAULTY (APU DOOR) · airframe 61,304 hrs · 21,592 cycles

JFK - INFLIGHT EWR-MIA. CREW REPORTED AUXILIARY POWER UNIT FAILED IN FLIGHT WITH LEFT GENERATOR ON PLACARD. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GENERATOR AND AUXILIARY POWER UNIT DOOR SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — SHORTED (CABIN) · airframe 60,877 hrs · 21,448 cycles

RIGHT NUMBER 4 FORWARD LIGHT WIRE FOUND SHORTED TO GROUND. CORRECTED SHORT IN WIRING. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,797 hrs · 21,418 cycles

FROM 26D SEAT TO AFT DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK FOR 26D SEAT AND AFT DOORS.

Part: ACOUSTIC PANEL — DEFECTIVE (LT ENGINE) · airframe 59,959 hrs · 21,118 cycles

MIA - CAPTAIN REPORTED LOUD NOISE FROM LEFT ENGINE AND VIBRATIONS AT LEFT NUMBER 2 DOOR ON TAKEOFF NO ANOMALIES WITH GAUGES OR AIRCRAFT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ACOUSTIC PANEL AND ADJUSTED DOOR LATCH AT MID LAV SERVICE DOOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FUSE — FAILED (RT MLG) · airframe 59,532 hrs · 20,946 cycles

RIGHT MAIN GEAR DOOR WOULD NOT RETRACT WHEN GEAR WAS UP. RECYCLED GEAR STILL WOULD NOT RETRACT. NORMAL GEAR AND DOOR INDICATION UPON LANDING. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED EXTENSION AND RETRACT FUSE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,690 hrs · 20,646 cycles

EMERGENCY BATTERY PACK AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED EMERGENCY BATTERY PACK AT RIGHT NUMBER TWO DOOR. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS ON ROW 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS ON ROW 9 TO 15.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT)

DFW - 21DEF EMERGENCY LIGHT HARNESS LOOSE. RESECURED 21DEF EMERGENCY LIGHT HARNESS.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT)

DFW - 27DEF EMERGENCY LIGHT HARNESS LOOSE. RESECURED 27DEF EMERGENCY LIGHT HARNESS.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT HARNESS AT LIGHT ASSEMBLY AT SEAT 32D LOOSE. RESECURED EMERGENCY LIGHT HARNESS AT LIGHT ASSEMBLY AT SEAT 32D.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHTS)

DFW - 18DEF EMERGENCY LIGHT HARNESS LOOSE. RESECURED 18DEF EMERGENCY LIGHT HARNESS.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT)

DFW - SEAT 29F EMERGENCY LIGHT HARNESS LOOSE AT WALL. RESECURED SEAT 29F EMERGENCY LIGHT HARNESS.

Part: BULB — MISSING (EMERGENCY LIGHT)

TPA - EMERGENCY LIGHT AT SEAT 17D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

TPA - EMERGENCY LIGHT AT SEAT 17D MISSING LENS. REPLACED RED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — LEAKING

ORD INFLIGHT T313 - FLIGHT ATTENDANTS REPORTED ELECTRICAL SMELL MIXED WITH SMELL OF BURNED PLASTIC. DECK NEAR AFT FLIGHT ATTENDANT JUMPSEAT SLIGHTLY WARM. BOTH AFT LAVATORY SMOKE ALARMS SOUNDED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED AUXILLIARY POWER UNIT DUE TO LOW OIL QUANTITY INDICATIONS AND OIL LEAK AND RAN AIR CONDITIONING PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT RT AFT OVERWING EXIT INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT RT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (CLOSED)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT LT NR 1 DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

AFW - LEFT WING FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT WING FORWARD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFW - EMERGENCY LIGHT AT STATION 985 LEFT WING FORWARD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT STATION 985 LEFT WING FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

EMERGENCY LIGHT ON SIDE OF SEAT 21D INOPERATIVE. FOUND CONNECTOR LOOSE AT SIDEWALL. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 10 THROUGH 14. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TECHNICIAN OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROW 15D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (CABIN)

EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 26DEF. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - CEILING EXIT LOCATOR SIGN AT ROW 17 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (APU)

DFW - FLT 745 - EN ROUTE DFW-SNA, DETECTED APU FLAME OUT WHILE LEFT GENERATOR ON MEL. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU DOOR OPEN SENSOR WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRANSMITTER — LEAKING (LT WING)

JFK - FLT 1397 - EN ROUTE JFK-MIA - DURING TAKEOFF ROLL, DETECTED LEFT SIDE FUEL FLOW DROP TO ZERO. RETURNED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED AFT FUEL FLOW TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — MALFUNCTIONED (NLG)

DFW - FLT 1904 - EN ROUTE SNA-DFW, ON TAKEOFF DURING GEAR RETRACTION, MAIN GEAR HUNG UP WITH AN ACCOMPANYING AMBER DISAGREE AND AMBER DOOR STATUS. ALERT LIGHT ILLUMINATED UPPER EICAS AND AUDIBLE ALERT CAME ON IN COCKPIT. AFTER APPROXIMATELY ONE MINUTE WITH GEAR HANDLING THE UP POSITION CESSNA AIRCRAFT REPORTED MAIN LANDING GEAR IN THE UP POSITION AND NOSE LANDING GEAR IN THE DOWN POSITION. AT AN ALTITUDE OF ABOUT 1000 FEET, THE NOSE GEAR CAME UP. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING GEAR ACTUATOR. PERFORMED GEAR SWING PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM ROW 1 TO ROW 14 FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT ROW 1. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: PAN — GOUGED (R4 DOOR)

AFW - R-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS. E58 NR 1803569. REPAIRED PER MRB NR 757-1053. TST: 14,920.38 HOURS. CYCLES, 5,447. (X)

Part: CONNECTORS — LOOSE (CABIN)

BOS - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTING FROM LAST ROW FIRST CLASS CABIN TO OVERWING EXIT, L2 DOOR EMERGENCY EXIT SIGN, R2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. RESEATED CONNECTIONS AT MID GALLEY FLOOR AND RIGHT FORWARD OVERWING DOOR, CLEANED CONNECTORS AT DOOR SIGNS. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M)

Part: DECK PLATE — CORRODED (BS 1680)

AFW - DECK PLATE HAS CORROSION REMOVED IN VARIOUS LOCATIONS. MATERIAL REMOVED IS BEYOND SRM LIMITS, PER MRB 757-735. TST: 15,758.46. CYCLES: 5,958. (X)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FLOOR BEAM AT STA 365 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-734. TST: 15,758.46 HRS. CYCLES: 5,958. (X)

Part: HANDLE PAN — GOUGED (R4 DOOR)

AFW - R4 DOOR HANDLE PAN HAS A SMALL GOUGE AFTER BLENDING IS BEYOND SRM LIMITS, PER MRB 757-740. TST: 15,758.46. CYCLES: 5,958. (X)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STA 1640 HAS CORROSION REMOVED ON UPPER SURFACE BEYOND SRM LIMITS, PER MRB 757-756. TST: 15,758.46 HRS. CYCLES: 5,958. (X)

Part: FLOOR BEAM — CORRODED (FS 377.7)

AFW - FLOOR BEAM AT STA 377.7 HAS CORROSION REMOVED ON UPPER SURFACE BEYOND SRM LIMITS, PER MRB 757-737. TST: 15,758.46 HRS. CYCLES: 5,958. (X)

Part: SILL — CORRODED (BS 1398-1440)

AFW - T-CHORD (INNER) HAS CORROSION REMOVED BEYOND SRM LIMITS ON UPPER SURFACE. T-CHORD (OUTER) HAS CORROSION REMOVED BEYOND SRM LIMITS ON OUTER SURFACE OF VERTICAL LEG, PER MRB 757-743. TST: 15,758.46 HRS. CYCLES: 5,958. (X)

Part: FLOOR BEAM — CORRODED (BS 345)

AFW - FLOOR BEAM AT STA 345 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-733. TST: 15,758.46 HRS. CYCLES: 5,958. (X)

Part: EEL WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRING IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)