N604AA

Part: HYDRAULIC LINE — DAMAGED (LT ENGINE) · airframe 57,472 hrs · 19,642 cycles

MIA, CREW REPORTED LT HYDRAULIC FAILURE. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HYDRAULIC LINE LOCATED ON LT ENGINE INBD SIDE OF COWL CASE DAMAGED. REPLACED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 3 · airframe 55,101 hrs · 18,797 cycles

CORROSION ON RIGHT OVERWING WALKWAY 10 INCHES FORWARD OF STRINGER 14 AT INBOARD SIDE OF THE WALKWAY. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 3 · airframe 55,101 hrs · 18,797 cycles

CORROSION ON RIGHT OVERWING WALKWAY AT OUTBOARD CORNER OF THE WALKWAY. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 3 · airframe 55,101 hrs · 18,797 cycles

CORROSION AROUND FASTENER ON OVERWING WALKWAY AREA FORWARD OF AFT SPAR. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 3 · airframe 55,101 hrs · 18,797 cycles

CORROSION ON THE RIGHT OVERWING WALKWAY APPROXIMATELY 18 INCHES FORWARD OF THE AFT SPAR. REMOVED CORROSION AND REPAIRED FOLLOWING PROCEDURES PER EA B757-57-027077.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 3 · airframe 55,101 hrs · 18,797 cycles

CORROSION ON OVERWING WALKWAY PANEL AROUND FASTENER 16 INCHES FORWARD OF STRINGER 14 AT THE INBOARD SIDE. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,504 hrs · 18,603 cycles

RIGHT AFT OVERWING EXIT AFT BULB INOPERATIVE. REPLACED AFT LAMP FOR RIGHT AFT OVERWING EXIT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,504 hrs · 18,603 cycles

LEFT FORWARD OVERWING EXIT AFT UPPER LAMP INOPERATIVE. REPLACED AFT UPPER LAMP FOR LEFT FORWARD OVERWING EXIT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,504 hrs · 18,603 cycles

LEFT AFT OVERWING EXIT AFT LAMP INOPERATIVE. REPLACED AFT LAMP FOR LEFT AFT OVERWING EXIT. OPS CHECK NORMAL.

Part: GENERATOR — FAILED (LEFT) · airframe 51,523 hrs · 17,493 cycles

DEN - INFLIGHT DFW-EGE. CREW REPORTED LEFT ENGINE GENERATOR FAILED WITH AUXILIARY POWER UNIT ON PLACARD. EMERGENCY DECLARED FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GENERATOR UNIT THAT WAS BAD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL MODULE — MALFUNCTIONED (SPOILER) · airframe 51,380 hrs · 17,442 cycles

DFW - CREW REPORTED DURING CLIMBOUT SPOILER EICAS MESSAGE AND OVERHEAD ANNUNCIATOR LIGHT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. UPON LANDING LEFT SIDE INSIDE SPOILER DID NOT DEPLOY AND MIDDLE SPOILER ONLY DEPLOYED HALFWAY. AIRCRAFT REMOVED FROM SERVICE. REPLACED WIRE BUNDLE W3305 AND W3405 AND L2 SPOLIER CONTROL MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PRESSURE PANEL — CORRODED (LT MLG WW) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

CORROSION ON PRESSURE DECK LEFT WHEEL WELL APPROXIMATE STATION 1140 INBOARD OF EXISTING DOUBLER. REPAIRED PER EA B757-53-01508.

Part: PRESSURE PANEL — CORRODED (RT MLG WW) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

CORROSION ON RIGHT WHEEL WELL PRESSURE DECK STATION 1100 RIGHT BUTTLINE 60. INSTALLED REPAIR DOUBLERS PER EA B757-53-015813.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

CORROSION - PRESSURE DECK-STATION 1128- RIGHT BUTTLINE 60. INSTALLED DOUBLER REPAIR PER EA B757-53-015810 AND BOEING DWG LOR5L53001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

STATION 1661 CORROSION ON FLOORBEAM CAP AT RIGHT BUTTLINE 57. REPAIRED FLOORBEAM CAP AT STATION 1661 AT RIGHT BUTTLINE 57 IAW BOEING DRAWING LOR5L53005, AND EA 757-53-015670.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

CORROSION ON AFT FLANGE BOTTOM SIDE OF FLOORBEAM AT STATION 377 LEFT BUTTLINE 60. INSTALLED T-CAP AND DOUBLERS PER SRM 53-00-51-2R 3 AND AARD 53-00-51-01.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

NUMBER 1 CARGO DOOR CORRSION ON INTERCOSTAL AT BOTTOM CENTER OF DOOR. REPLACED INTERCOSTAL ON BOTTOM OF FORWARD CARGO DOOR IAW ESO 90114.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

RIGHT NUMBER 4 DOOR FORWARD DRAIN SUPPORT HAS CORRISION FROM 1640 TO 1661. REMOVED CORRODED AND INSTALLED NEW RIGHT NUMBER 4 FORWARD DRAIN SUPPORT IAW 757 SRM 51-10-02-OG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,352 hrs · 17,076 cycles

FLOORBOARD SUPPORT STATIONS 1661 TO 1681 CORRODED. REPAIRED PER SRM 51-10-02 0G.

Part: PIN — DEFECTIVE (CABIN) · airframe 49,433 hrs · 16,728 cycles

SEAT 18 EMERGENCY LIGHT INOPERATIVE. REPLACED PINS AT SIDEWALL. OPS CHECKS NORMAL.

Part: PUMP — FAILED (LT ENGINE) · airframe 49,112 hrs · 16,619 cycles

SJU - INFLIGHT CCS-MIA. CREW REPORTED LEFT HYDRAULIC PRESSURE LOSS. EMERGENCY DECLARED DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN PUMP, CASE DRAIN FILTER, PRESSURE FILTER AND POWER TRANSFER UNIT FILTERS.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 48,984 hrs · 16,575 cycles

ANC - CREW REPORTED SMOKE ODOR IN CABIN COMING FROM FORWARD GALLEY OVEN. EMERGENCY DECLARED RETURNED ANC LANDED WITHOUT INCIDENT. REPLACED FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,589 hrs · 16,431 cycles

FORWARD OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT FORWARD OVERWING. OPS CHECKED NORMAL.

Part: TERMINAL — BROKEN (EXTERIOR) · airframe 48,589 hrs · 16,431 cycles

RIGHT NUMBER 3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPAIRED TERMINAL END OF LIGHT BASE. OPS CHECKED NORMAL.

Part: WATER HEATER — OVERHEATED (LAVATORY) · airframe 46,400 hrs · 15,629 cycles

INFLIGHT ORD TO SNA. CREW REPORTED FUMES AROUND RIGHT AFT LAVATORY AREA AND SMOKE DETECTOR SOUNDED. MAINTENANCE FOUND RIGHT AFT LAV WATER HEATER OVERHEATED AND CIRCUIT BREAKER POPPED. LANDED DEN WITHOUT INCIDENT. RESET RIGHT AFT LAVATORY WATER HEATER. NO FURTHER ODOR NOTICED.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 23DEF DAMAGED. REPLACED SHROUD AT SEAT ROW 23DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 43,913 hrs

MIA - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT SEAT ROW 9E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 43,913 hrs

MIA - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT SEAT ROW 19E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

PRESSURE DECK CORRODED 11 INCHES TO 21 INCHES OUTBOARD OF CENTER LINE. REPAIRED PRESSURE DECK IAW EA B757-53-004896.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

AFT MAIN DECK PLATE DOUBLER CORRODED. INSTALLED NEW DOUBLER IAW SRM 53-60-51-2R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

LT OUTBOARD SEAT TRACK CORRODED, REPLACED SEAT TRACK IAW SRM 51-10-02.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

AFT MAIN DECK PLATE CORRODED. INSTALLED REPAIR DOUBLER IAW SRM 53-60-51-2R.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

LT OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW SRM 51-10-02.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R 2.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

LT INBOARD SEAT TRACK CORRODED, REPLACED SEAT TRACK IAW SRM 51-10-02.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,723 hrs · 14,666 cycles

AFT OUTBOARD RIGHT SIDE GALLEY FITTING CORRODED. REPLACED FITTING IAW SRM 53-00-51.

Part: PSEU — FAILED (LANDING GEAR) · airframe 42,566 hrs

SJU INFLIGHT T1312/16JUN. CREW REPORTED GEAR INDICATION AFTER RETRACTION. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,190 hrs

DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 23 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS FROM SEAT ROW 15 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROW 15 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY)

JFK INFLIGHT - NUMBER ONE OVEN IN FIRST CLASS SMOKING WHILE IN USE. OVEN WAS TURNED OFF AND SMALL PATCH CONTINUE TO GLOW AT LEFT SIDE OF HEATING ELEMENT. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. CLEANED BURNED DEBRIS AND GREASE ON HEATING ELEMENT FOR NUMBER ONE OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - SEAT PATH EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT PATH EMERGENCY LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — TORN (OIL CAP)

BOS - INFLIGHT, RIGHT ENGINE IN FLIGHT SHUT DOWN DUE TO OIL QUANTITY LOSS. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 25 MINUTES. FOUND O-RING FOR OIL CAP TORN. FOUND DEBRIS UNDER OIL TANK CHECK VALVE. REMOVED DEBRIS AND REPLACED OIL CAP O-RING. REPLACED SCAVENGE AND PRESSURE FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

MIA - OVERHEAD EMERGENCY LIGHT AT SEAT 20C HAS LENS MISSING. REPLACED LENS FOR OVERHEAD EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHTS AT SEAT 16D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (MLG)

JFK INFLIGHT T1015/30 RIGHT SYSTEM HYDRAULIC QUANTITY EICAS STATUS PAGE INDICATED .42 QUANTITY. RETURNED TO JFK AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION WITH NO DAMAGE NOTED. SERVICED RIGHT HYDRAULIC SYSTEM TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. REPLACED RIGHT HAND ANTI SKID SHUTTLE VALVE MODULE AND ALTERNATE BRAKE SELECTOR VALVE. JACKED AIRCRAFT AND CHECKED ALL BRAKES FOR PROPER RELEASE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) PROPER RELEASE.

Part: BRAKE — DRAGGING (MLG)

MIA - T1550 NEAR THE V1 SPEED THE AIRCRAFT YAWED TO THE LEFT ABOUT 5 DEGREES. THE TAKEOFF WAS CONTINUED AND A NORMAL ROTATION WAS ACCOMPLISHED. LANDED AT MIA WITHOUT INCIDENT. ACCOMPLISHED SPIN CHECK OF LEFT HAND MAIN GEAR AND FOUND NUMBER ONE BRAKE DRAGGING. REPLACED NUMBER ONE BRAKE ASSEMBLY. 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. REPLACE ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SLIDE LIGHT AT R4 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT SLIDE LIGHT LAMP SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT ILGHT AT SEAT 1ABC INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 1ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 24D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (SEAT 20)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 20D INOPERATIVE. RESEATED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)