N639AA

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,615 hrs · 24,864 cycles

FS FLOOR BEAM AT STATION 1661 & RBL 40 CORRODED. ACCOMPLISHED NESTED ANGLE REPAIR IAW EA B757-53-030895.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 70,615 hrs · 24,864 cycles

DAMAGE TO SKIN AT APPROXIMATELY STATION 1650 & STRINGERS 28 & 29 RT. REMOVED DAMAGE & INSTALLED REPAIR IAW SRM 53-00-01-2R.

Part: BEAM — CRACKED (FUSELAGE) · airframe 70,615 hrs · 24,864 cycles

THE PIN BEAM AFT END COMMON TO STATION 1720 WAS FOUND TO BE CRACKED. THE PIN BEAM IS CRACKED BETWEEN THE TWO AFT CENTER FASTENER HOLES & THE AFT EDGE OF THE PIN BEAM. ACCOMPLISHED COMPLEX REPAIR IAW EA B757-53-030938.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,616 hrs · 24,865 cycles

AFT DECK CORRODED FROM STATIONS 1680 TO 1700. REPLACED THE ENTIRE AFT DECK FLOOR IAW AARD 51-00-05-1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 70,615 hrs · 24,864 cycles

FRAME CHORD DAMAGE AT STATION 1640 JUST AFT OF STRINGER 8 RT. BLENDED DAMAGE & INSTALLED DOUBLER IAW B757-53-030942

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,615 hrs · 24,864 cycles

T CAP AT STATION 1640 AT RBL 55 CORRODED. SPLICED IN NEW T CAP IAW EA B757-53-030876.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,615 hrs · 24,864 cycles

T CAP AT STATION 1661 & RBL 55 CORRODED. SPLICED IN NEW T CAP IAW EA B757-53-030876.

Part: PUMP — OVERHEATED (HYDRAULIC SYS) · airframe 69,437 hrs · 24,410 cycles

DFW - CREW REPORTED OVERHEAT CONDITION ON LEFT WHEEL WELL. UPON RETURNING TO GATE RIGHT NUMBER 4 SLIDE WAS DEPLOYED DUE TO SMOKE IN CABIN. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ELECTRIC HYDRAULIC PUMP AND RIGHT NUMBER 4 SLIDE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 68,856 hrs · 24,192 cycles

SEAT MOUNTED EMERGENCY LIGHTS ON 4E INOPERATIVE. SECURED LOOSE WALL CONNECTOR. OPS CHECK NORMAL.

Part: SEAT — LOOSE (CABIN) · airframe 68,446 hrs · 24,044 cycles

JFK - CREW REPORTED DURING CLIMBOUT, SEAT ROW 14ABC CAME OUT OF ITS SEAT TRACK CAUSING THE SEAT TO PITCH BACK AND THE FRONT AND REAR LOCKS CAME OUT OF THEIR TRACKS. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED COMPLETE INSPECTION OF SEATS ONBOARD AND FOUND NUMEROUS SEATS NOT LOCKED DOWN PROPERLY. SECURED AND TIGHTENED ALL AFFECTED SEATS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,218 hrs · 23,225 cycles

DENT IN SKIN AT STATION 840 AND STRINGERS 1 TO 2 LEFT. INSTALLED DOUBLER PER EA B757-53-021104.

Part: UPLOCK SENSOR — INOPERATIVE (LANDING GEAR) · airframe 65,430 hrs · 22,932 cycles

DFW - CREW REPORTED AFTER TAKEOFF AND GEAR RETRACTION, GEAR WARNING ANNUNCIATOR LIGHT AND GEAR DISAGREE EICAS MESSAGE ILLUMINATED. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED RIGHT SYSTEM NUMBERS ONE AND TWO GEAR UPLOCK SENSORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,346 hrs · 22,536 cycles

PATHWAY EMERGENCY LIGHT AT SEAT 4EF FORWARD LIGHT IS INOPERATIVE. REPLACED LAMP FOR PATHWAY EMERGENCY LIGHT AT SEAT 4EF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,150 hrs · 22,458 cycles

1ST CLASS SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK FOR 1ST CLASS SEAT MOUNTED EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: ENGINE — FAILED (RIGHT) · airframe 63,849 hrs · 22,351 cycles

CUN - CREW REPORTED RIGHT ENGINE FIRE INDICATION ILLUMINATED IN FLIGHT WITH OVERHEAT AMBER EICAS MESSAGE. BOTH FIRE BOTTLES WERE DISCHARGED. RIGHT ENGINE SHUT DOWN (SINGLE ENGINE TIME 25 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED CUN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH FIRE BOTTLES. REPLACED RIGHT ENGINE ON 03/20/2011 AT CUN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,348 hrs · 22,182 cycles

BULLNOSE EMERGENCY LIGHT ABOVE 14D INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT ABOVE 14D. OPS CHECK NORMAL.

Part: GUARD — MISSING (CABIN) · airframe 61,893 hrs · 21,664 cycles

SEAT 19D MISSING ESCAPE PATH LIGHT GUARD. REPLACED GUARD FOR ESCAPE PATH LIGHT AT SEAT 19D. OPS CHECKED NORMAL.

Part: PLACARD — PEELING (CABIN) · airframe 61,893 hrs · 21,664 cycles

LEFT NUMBER 2 DOOR AFT EXIT MARKER STICKER PEELING. REMOVED AND REPLACED AFT LEFT NUMBER 2 DOOR EXIT STICKER.

Part: DOUBLER — MISINSTALLED (FUSELAGE) · airframe 61,382 hrs · 21,482 cycles

CABIN AFT DECK PLATE HAS DOUBLER THAT IS NOT INSTALLED UNDER AFT CAP FROM LEFT TO RIGHT SIDES. REPLACED DOUBLER ON AFT PRESSURE DECK PER SRM 53-60-51-2 R 2 AND EA B757-53-010811.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

CABIN AFT GALLEY CENTER SUPPORT CORRODED STATION 1705. REPLACED HAT CHANNEL PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

AFT CABIN AFT GALLEY CORRODED AT ZEE ANGLE AT STATION 1700 AND LEFT BUTTLINE 50. REPLACED ZEE ANGLE AT STATION 1700 AND LEFT BUTTLINE 50 PER SRM 51-10-02-0G.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

UPPER BATHTUB FITTING CORRODED AT STATION 1720 LEFT SIDE. REPLACED UPPER BATHTUB FITTING PER SRM 51-10-02-0G.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,382 hrs · 21,482 cycles

INTERIM REPAIR TO LEFT TRAILING EDGE FLAP UPPER SKIN PER ESO 90309 DATED 7-15-2008. REMOVED INTERIM REPAIR FROM BOTH SIDES OF TRAILING EDGE SKIN. BONDED IN CORE AND LOWER SKIN REPAIR FOR FIRST OF TWO STAGE PERMANENT REPAIR PER SRM 57-53-01-2R-1 AND SRM 51-70-07.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

CORROSION ON LEFT OUTBOARD T ANGLE IN LEFT AFT CORNER OF BLUE ROOM AT STRINGER 17 LEFT STATION 1720 LEFT BUTTLINE 57. CAN BE SEEN FROM BELOW CABIN FLOOR. REPLACED LEFT OUTBOARD T-ANGLE PER SRM 51-10-02-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

CORROSION ON CARGO SUPPORT WEB. REPLACED INTERCOSTAL PER SRM 53-60-04-2R.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

CORROSION ON FORWARD CARGO DOOR SILL FITTING AT STATION 612 STRINGER 27 RIGHT. REPLACED FITTING AT STATION 612 STRINGER 27 RIGHT PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,381 hrs · 21,482 cycles

CORROSION ON CLIP NUT ON CREASE ANGLE. ACCOMPLISHED SPLICE REPAIR PER AARD 53-30-13-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

RIGHT CREASE BEAM CORRODED FROM STATIONS 1380 TO 1400. REMOVED AND REPLACED DITCHING PANEL PER SRM 51-10-02-G8.

Part: SUPPORT — CORRODED (L4 DOOR) · corrosion level 2 · airframe 61,381 hrs · 21,482 cycles

LEFT NUMBER 4 DOOR SCUFF PLATE SUPPORT CORRODED. REPLACED SUPPORT PER SRM 51-10-02-0G.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

RIGHT CREASE BEAM CORRODED FROM STATIONS 1420 TO 1440. REPLACED CREASE BEAM (WEB/DITCHING PANEL) WITH SHOP FABRICATED REPLACEMENT DITCHING PANEL PER 757 SRM 51-30-01-0G.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,382 hrs · 21,482 cycles

BELOW THE CABIN FLOOR AT STATION 780 BUTTLINE 0 THE TOP OF THE VERTICAL LEG OF THE INTERCOSTAL HAS A 0.75 INCH CRACK IN IT. INSTALLED NEW WEBBING AT STATIONS 780 TO 800 IAW SRM 51-10-02-G8 AND SRM 53-00-51-2 R 4.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

FORWARD DRAIN SUPPORT CORRODED, FLOOR STRUCTURE OF RIGHT NUMBER 1 PASSENGER SERVICE ENTRY DOOR CUTOUT FLOOR STRUCTURE. INSTALLED SERVICEABLE DRAIN SUPPORT PER SRM 51-10-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

AFT DRAIN SUPPORT CORRODED, FLOOR STRUCTURE OF RIGHT NUMBER 1 PASSENGER SERVICE ENTRY DOOR CUTOUT FLOOR STRUCTURE. INSTALLED SERVICEABLE DRAIN SUPPORT PER SRM 51-10-02-0G.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,382 hrs · 21,482 cycles

CABIN FLOOR INTERCOSTAL STATIONS 780 TO 800 BUTTLINE 0 CRACKED. REPLACED INTERCOSTAL CAP AT STATIONS 780 TO 800 IAW SRM 51-10-02-G8 AND SRM 53-00-51-2 R4.

Part: SHIM — MIGRATED (PYLON) · airframe 61,382 hrs · 21,482 cycles

RIGHT ENGINE PYLON FORWARD OUTBOARD LOWER MID SPAR SHIM MIGRATED. REPAIRED IAW AARD 54-50-07-1.

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

CORROSION ON FLOORBOARD STRUCTURE RIGHT BUTTLINE 54 STATIONS 750 TO 770. COMPLETED INSTALLATION OF CHORD ANGLE AND SPLICE PER AARD 53-30-13-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

SEAT TRACK NUMBER 3 AT STATION 670 IS PITTED IN TRACK. INSTALLED NEW SEAT TRACK AT RIGHT BUTTLINE 25 STATIONS 640 TO 780 IAW SRM 51-10-02-G8.

Part: MOUNT BRACKET — DAMAGED (FUSELAGE) · airframe 61,382 hrs · 21,482 cycles

THE 5TH AFT THRESHOLD SCUFF PLATE MOUNTING BRACKET HAS OVERSIZED ELONGATED HOLES RIGHT NUMBER 1 DOOR THRESHOLD. REPLACED 5TH AFT THRESHOLD SCUFF PLATE MOUNTING BRACKET PER SRM 51-10-02-0G.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

CORROSION AROUND BLIND FASTENER AT OUTBOARD BOTTOM BLIND FASTENER. BLENDED CORRODED AREA AND INSTALLED STRAP-DOUBLER PER EA B757-27-010644.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,382 hrs · 21,482 cycles

NUMBER 9 SLAT, CORROSION ON SKIN AT DRIVE-TRACK. INSTALLED A FLUSH-DOUBLER PER SRM-57-43-01-2R.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,706 hrs · 21,228 cycles

CORROSION AROUND FASTENERS ON UPPER SKIN AT INBOARD DRIVE TRACK NUMBER 8 SLAT. REMOVED CORROSION INSTALLED DOUBLER PER AARD 57-43-00-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,132 hrs · 20,698 cycles

SFO - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22D.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,734 hrs

SFO - SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 25 TO 36 ARE DIM. REPLACED BATTERY PACK AT AFT GALLEY OVERHEAD.

Part: SPRING — INOPERATIVE (GIRT BAR) · airframe 57,267 hrs

JFK - L4 DOOR SLIDE ARM LIGHT WAS OUT BUT HANDLE NOT IN DISARM POSITION. REPLACED GIRT BAR SLIDER RIGHT LEAF SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 56,756 hrs

MIA EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. SECURED CONNECTOR PLUG FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS) · 56,470 cycles

SEA EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 WOULD NOT GO OUT WHEN POWER WAS REMOVED FROM ACFT. FOUND BAD LIGHT SOCKET AT SEAT 16D. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LENS — MISSING (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 28D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT LIGHTS AT LT AND RT NR 1 DOOR INOPERATIVE. REPLACED POWER SUPPLY FOR EMERGENCY EXIT LIGHTS AT LT AND RT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT SEATS 1E, 13D THROUGH 15D, AND 21D INOPERATIVE. REPLACED LAMPS FOR INOPERATIVE EMERGENCY LIGHTS AT SEATS 1E, 13D THROUGH 15D, AND 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (CABIN)

DFW - EMERGENCY LIGHTS AT SEAT 20D INOPERATIVE. REPAIRED CONNECTOR FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CIRCUIT BREAKER — INOPERATIVE (EMERGENCY LIGHT)

JFK - SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 16 AFT WOULD NOT TURN OFF FROM COCKPIT OR FLIGHT ATTENDANT STATION. LIGHT WENT OUT AFTER 45 MINUTES. RESET EMERGENCY LIGHT CHARGER CIRCUIT BREAKERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — FAILED (STALL WARNING)

TUL - FLT 535 - AIRCRAFT EN ROUTE TUL TO DFW, DURING ROTATION STICK SHAKER ACTIVATED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT NOT OVERWEIGHT. ACCOMPLISHED MCDP FAULT CHECK AND REPLACED ANGLE OF ATTACH SENSORS AND STALL WARNING CARDS. SYSTEM GROUND AND FCF CHECKED NORMAL OPERATION. (M)

Part: GIRT BAR — DAMAGED (ESCAPE SLIDE)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION. FOUND THE R1 DOOR GIRT BAR LEAF SPRINGS NOT WORKING PROPERLY. REPLACED GIRT BAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FOUND SEAT MOUNTED EMERGENCY LIGHT AT 32D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT GALLEY RIGHT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT AFT GALLEY RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (FS 317)

AFW - FLOOR BEAM AT STA 377, LBL 57, 55, 51, 35, 22, 18, AND RBL 10 HAD CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-666. TST, 15,327.4 HOURS. CYCLES, 5,762. (X)

Part: SKIN — DENTED (BS 502)

AT STA 502 AND BETWEEN S29L AND S28L, THE LOWER FUSELAGE SKIN HAS A DENT AND GOUGE 20 INCHES AFT OF MAIN E/E DOOR. THE PARENT MATERIAL REMAINING IN THE BLEND AREA OF GOUGE, 0.033 INCH. DAMAGE IS BEYOND SRM LIMITS, PER MRB 757-671. TST, 15,327.4 HOURS. CYCLES, 5,762. (X)

Part: DECK PLATE — CORRODED (BS 1681.8)

AFW - DECK PLATE HAS CORROSION REMOVED ON UPPER SURFACE AT VARIOUS LOCATIONS BEYOND SRM LIMITS PER MRB 757-668. TST, 15,327.4 HOURS, CYCLES, 5,762. (X)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STA 1640, RBL 50 AND RBL 53 HAD CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-667. TST, 15,327.4 HOURS. CYCLES, 5,762. (X)