N630AA

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 72,596 hrs · 25,819 cycles

JFK CREW REPORTED MAIN BATTERY CHARGER STATUS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. REPLACED MAIN BATTERY CHARGER. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 72,013 hrs · 25,610 cycles

ON CLIMB OUT FROM DFW THE CREW REPORTED LT AFT FUEL BOOST PUMP FAILED. EMERGENCY WAS & THE CREW ACCOMPLISHED QRH PROCEDURES. THE FLIGHT DIVERTED MSY WITH A REPORTED 1900 LB FUEL IMBALANCE. PLACARDED LT AFT FUEL BOOST PUMP IAW MEL, REFUEL & DISPATCHED THE FLIGHT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,966 hrs · 25,586 cycles

FOUND 2 LIGHTNING STRIKES THAT SHOWED CRACKS ON FUSELAGE AT STATION 1500 AT STRINGER 3 LT. REMOVED DAMAGE & INSTALLED SKIN DOUBLER & STRINGER REPAIR.

Part: SKIN — DEBONDED (TE FLAP) · airframe 71,966 hrs · 25,586 cycles

LT HAND INBD MAIN FLAP LOWER SKIN DISBONDED. THE DAMAGE IS LOCATED JUST OTBD OF THE NR 3 FLAP FAIRING. REPAIRED DAMAGE UP TO 6 INCHES IN DIAMETER ON THE FLAP LOWER SKIN IAW SRM 51-70-10-2R & EA B757-57-032253 USING THE HF ALODINE SURFACE PREPARATION WITH PASTE ADHESIVES AS GIVEN IN THE SRM.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 71,966 hrs · 25,586 cycles

LOWER FWD CORNER OF AFT CARGO DOOR. INSTALLED PERMANENT REPAIR IAW SRM 52-30-01 & AARD 52-30-01.

Part: BULKHEAD — CORRODED (NLG WW) · corrosion level 3 · airframe 71,966 hrs · 25,586 cycles

NOSE GEAR BULKHEAD AT STATION 263 OUTER CHORD CORRODED. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-53-032297.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,714 hrs · 24,822 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK M10568. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,714 hrs · 24,822 cycles

LIGHTNING STRIKE AT FORWARD ATG ANTENNA. ACCOMPLISHED BORE REWORK PER EA B757-53-028744.

Part: STRAP — OUT OF POSITION (EVAC SLIDE) · airframe 69,714 hrs · 24,822 cycles

RELEASE STRAP DOES NOT GO THROUGH GUIDE RING ON RIGHT NUMBER 2 SLIDE. INSTALLED RELEASE STRAP THROUGH GUIDE RING ON RIGHT NUMBER 2 SLIDE.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 68,789 hrs · 24,495 cycles

EMERGENCY EXIT LIGHT LOCATED IN OVERHEAD BIN AREA AT ROW 13ABC INOPERATIVE. REPLACED LIGHT HOUSING ASSEMBLY AT ROW 13ABC. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,789 hrs · 24,495 cycles

EMERGENCY EXIT LIGHTS LOCATED IN OVERHEAD BIN AREA AT ROWS 13ABC, 16ABC AND 18ABC INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

CORROSION ON STRINGER 30 RIGHT AT STATION 1700. REPLACED STRINGER PER SRM 53-00-03-2R 1.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

CORROSION ON AFT DECK STATION 1720 AT LEFT AND RIGHT BUTTLINE 54. INSTALLED NEW DOUBLER PER AARD 51-00-05-1.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

CORROSION AT STATION 1681 AT LEFT BUTTLINE 48. INSTALLED T-CAP REPAIR PER EA B757-53-023767.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 68,160 hrs · 24,262 cycles

BELLFRAME IS CUT AT STATION 1681 AFT OF RIGHT NUMBER 4 DOOR AT TOP OF 1681 FLOORBEAM. INSTALLED BELLFRAME DOUBLER REPAIR PER EA B757-53-023825 AND SRM 51-70-11-OG.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

LEFT NUMBER 4 DOOR, STATIONS 1640 TO 1660 DOOR DRAIN SUPPORT HAS CORROSION. INSTALLED FORWARD DRAIN SUPPORT OF LEFT NUMBER 4 DOOR PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

STATION 1660 TO 1681 BUTTLINE 0 INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

LEFT NUMBER 4 DOOR, STATIONS 1660 TO 1681 DOOR DRAIN SUPPORT HAS CORROSION. INSTALLED AFT DRAIN SUPPORT OF LEFT NUMBER 4 DOOR PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

WHEN INSTALLING LEFT NUMBER 4 DOOR THRESHOLD CORROSION WAS FOUND APPROXIMATELY LEFT BUTTLINE 58 AT STATION 1640. INSTALLED T-CAP, EXISTING STRAPS AND DOUBLERS PER SRM 53-00-51-2R.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,160 hrs · 24,262 cycles

RIGHT NUMBER 1 FORWARD DRAIN PAN SUPPORT CORRODED AT STATION 345. INSTALLED FORWARD DRAIN PAN SUPPORT FOR THE RIGHT NUMBER 1 SERVICE/PASSENGER ENTRY DOOR PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 65,471 hrs · 23,268 cycles

LAX - INFLIGHT ORD-SNA. CREW REPORTED TRAILING EDGE FLAP DISAGREE EICAS MESSAGE AFTER SELECTION OF 15 DEGREE FLAP ON DESCENT. FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP CONTROL LEVEL POSITION TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,883 hrs · 22,705 cycles

SEAT ESCAPE PATH LIGHT AT 35D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR ESCAPE PATH LIGHT AT 35D. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,883 hrs · 22,705 cycles

RIGHT NUMBER 2 EXTERIOR ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP AT RIGHT NUMBER 2 EXTERIOR ESCAPE PATH LIGHT. OPS CHECKS GOOD.

Part: PLACARD — PEELING (CABIN) · airframe 63,883 hrs · 22,705 cycles

RIGHT FORWARD OVERWING HATCH ESCAPE PATH LIGHT EXIT STICKER PEELING. REMOVED AND REPLACED EXIT STICKER AT RIGHT FORWARD OVERWING HATCH. OPS CHECK NORMAL.

Part: PLACARD — PEELING (CABIN) · airframe 63,883 hrs · 22,705 cycles

LEFT AFT OVERWING HATCH ESCAPE PATH LIGHT EXIT MARKER PEELING. REMOVED AND REPLACED EXIT STICKER AT LEFT AFT OVERWING HATCH. OPS CHECK NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 63,370 hrs · 22,518 cycles

CORROSION AT NUMBER 10 SLAT LEADING EDGE SKIN AT RIVET ROW APPROXIMATELY 2.5 FEET OUTBOARD LEADING EDGE. CORROSION REMOVED AND DOUBLERS INSTALLED PER AARD 57-43-00-1.

Part: MODULE — INOPERATIVE (RUDDER) · airframe 62,771 hrs · 22,304 cycles

RDU - INFLIGHT LGA-MIA. CREW REPORTED RUDDER TRIM STUCK AT 3.5 UNITS ON CLIMBOUT FROM LGA REQUIRED 3 TO FOUR UNITS OF AILERON TO FLY LEVEL. EMERGENCY DECLARED LANDED RDU WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT RUDDER RATIO MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN) · airframe 60,078 hrs · 21,335 cycles

EMERGENCY LIGHT AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED EMERGENCY BATTERY MODULE AT STATION 705.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,184 hrs

JFK - EMERGENCY LIGHT AT OVERHEAD LT NR TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD LT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,184 hrs

JFK - EMERGENCY LIGHT AT MID LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT MID LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: TUBE — BROKEN (P1 SENSE) · airframe 56,005 hrs

MCO INFLIGHT T1247/28MAY MIA TO ORD. NR TWO ENGINE ENGINE PRESSURE RATIO REMAINED AT CLIMB. ALL OTHER INDICATIONS DROPPED LOWER AS ALTITUDE INCREASED. LANDED MCO WITHOUT INCIDENT. REPLACED NR TWO ENGINE BROKEN P1 SENSE LINE AT FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: ACTUATOR — INOPERATIVE (MLG) · airframe 55,962 hrs

ORD INFLIGHT T1740/22MAY LT HYDRAULIC QUANTITY INDICATION FOLLOWED BY LOSS OF LT SYSTEM HYDRAULIC PRESSURE. RUDDER TRIM DID NOT WORK DURING INITIAL APPROACH. AFTER TWO ATTEMPS RUDDER TRIM WORKED NORMALLY. LANDED ORD WITHOUT INCIDENT. REPLACED LT MAIN LANDING GEAR DOWN LOCK ACTUATOR AND LEFT MAIN LANDING GEAR DOWN LOCK ACTUATOR HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,836 hrs

MIA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 54,836 hrs

MIA - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY PATH LIGHT AT RIGHT SEAT 12A INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT SEAT 12A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCYLIGHT)

BOS - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED WIRE CONTACT SOCKET FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT)

SFO EMERGENCY ESCAPE PATH LIGHT AT 20D INOPERATIVE. REPAIRED BROKEN CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: WIRE — LOOSE (LT GENERATOR)

LEFT GENERATOR FAILED IN FLIGHT. AIRCRAFT RETURNED ANC AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT GENERATOR GROUND WIRE LOOSE AT IDG TERMINAL BLOCK. RE-TORQUED WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPRING — OUT OF ADJUST (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RELIEF VALVE — MALFUNCTIONED (HYD SYSTEM)

DFW - FLT 389 - EN ROUTE SAT-DFW - DURING DESCENT, LEFT HYDRAULIC QUANTITY EICAS MESSAGE CAME ON. LEFT RESERVOIR LIGHT ALSO CAME WITH ZERO PRESSURE SHOWING. AIRCRAFT LANDED AT DFW WITHOUT INCIDENT. INSPECTION OF AIRCRAFT FOUND NO LEAKS. REPLACED LEFT RESERVOIR PRESSURIZATION MODULE FILTER. REPLACED LEFT HYDRAULIC RESERVOIR PRESSURE RELIEF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 1681)

AFW - FLOORBEAM AT STATION 1681 HAS CORROSION REMOVED. A .080 THICK 7075-T6 REPAIR ANGLE WILL BE INSTALLED UNDER FORWRD FLANGE OF FLOORBEAM. A .071 THICK 7075-T6 FILLER WILL BE ADDED IN THE AREA OF THE REMOVED DECK PLATE. A .080 THICK 7075-T6 DOUBLER WAS FASTENED OVER THE FILLER AND DECK PLATE. (M)

Part: WIRE — BROKEN (EMER EXIT)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE ON LEFT SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 345)

AFW - CORROSION BLENDED ON FLOOR BEAM AT STATION 345, LBL 12, IS BEYOND SRM LIMITS, PER MRB 757-589. (M)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - CORROSION BLENDED ON FLOOR BEAM AT STATION 324, RBL 61 IS BEYOND SRM LIMITS, REPAIRED PER MRB. (M)

Part: DECK — CORRODED (BS 1681/1716)

AFW - PRESSURE DECK HAS CORROSION REMOVAL AT STATION 1716 AND STATION 1681 AT VARIOUS BL LOCATIONS, MATERIAL REMAINING IS BEYOND SRM LIMITS, PER MRB 757-587. (M)

Part: DOOR FRAME — CRACKED (BS 338)

AFW - FRAME AT STATION 338, WL 263 AND LBL IS CRACKED, PER MRB 757-585. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-586. (M)

Part: EEL CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATAIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)