N625AA

Part: FITTING — CRACKED (RT PYLON) · airframe 70,196 hrs · 25,054 cycles

RIGHT PYLON: SHEARED OUTBOARD LOWER FASTENER THROUGH THE VERTICAL FLANGE OF THE DIAGONAL BRACE FITTING OF THE AFT BULKHEAD. HFEC INSPECTION OF THE FASTENER HOLE INDICATED EVIDENCE OF A CRACK. REAMED HOLE. HFEC REINSPECTION CONFIRMED NO CRACK. REINSTALLED FASTENER. REPAIRS ACCOMPLISHED PER EA B757-54-028696.

Part: SPLICE PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 70,196 hrs · 25,054 cycles

CORROSION ON THE HORIZONTAL STABILIZER - RIGHT LOWER PIVOT SPLICE PLATE. REMOVED CORROSION AND ACCOMPLISHED REPAIRED PER EA B757-55-028640.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,956 hrs · 24,959 cycles

SEAT EMERGENCY EVACUATING LIGHTS FROM ROWS 1 TO 6 INOPERATIVE. REPLACED BATTERY PACK M10798. OPS CHECK NORMAL.

Part: SHUTTLE VALVE — INOPERATIVE (ANTI-SKID SYS) · airframe 68,254 hrs · 24,368 cycles

MIA - CREW REPORTED LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY FOLLOWED BY LOSS OF RIGHT HYDRAULIC SYSTEM PRESSURE. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT ANTI SKID SHUTTLE VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 66,281 hrs · 23,612 cycles

DOME SEALANT MISSING ON FASTENERS AT PP STATION 172 NUMBER 2 PYLON, VERTICAL FASTENER THROUGH UPPER SPAR AT STATION 172 OUTBOARD SIDE SHOWS SIGN OF ROTATION. INSTALLED FREEZE PLUG REPAIR PER EA 757-54-019893.

Part: BULKHEAD — CRACKED (LT PYLON) · airframe 66,281 hrs · 23,612 cycles

LEFT PYLON MID BULKHEAD OUTBOARD FOWARD LOWER MOUNT CRACKED AT BOLT HOLE. REPAIRED PER EA B757-54-019860.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

IN THE CABIN THE LATERAL FLOORBEAM AT STATION 310 IS CORRODED BETWEEN RIGHT BUTTLINES 40 AND 43. INSTALLED NEW UPPER CHORD AND STIFFENER PER SRM 53-00-51-2, R3 AND EA B757-53-019839.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

IN THE CABIN BETWEEN STATIONS 1640 TO 1661 AT BUTTLINE 0 THE LONGITUDAL FLOORBOARD SUPPORT IS CORRODED BY THE NUT PLATE HOLES. REMOVED AND REPLACED THE LONGITUDAL FLOORBOARD SUPPORT AT STATIONS 1640 TO 1661 AT BUTTLINE 0 PER SRM 51-40-02-0G.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

DOUBLER AT STATION 1720 CORRODED. INSTALLED REPAIR DOUBLER AND BOTTOM DOUBLERS PER SRM 53-60-51-2R 2 AND EA B757-53-019771.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

IN THE CABIN AT STATION 1640 THE LATERAL FLOORBEAM IS CORRODED AROUND THE NUT PLATE HOLE ON THE FORWARD SIDE BOTTOM SURFACE RIGHT BUTTLINE 8.5. REMOVED CORROSION, AND REINFORCED LATERAL "I" BEAM "T" CAP PER SRM 53-00-51-2R, REPAIR 3.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

IN THE CABIN AT STATION 1681 THE AFT GALLEY DECK PLATE DOUBLER IS CORRODED BETWEEN LEFT BUTTLINES 48 AND 50. INSTALLED DOUBLER AT STATION 1681 BETWEEN LEFT BUTTLINES 48 AND 50 PER SRM 53-60-51-2R 2.

Part: SKIN — DAMAGED (LE SLAT) · airframe 66,281 hrs · 23,612 cycles

LEFT WING WORN AREA ON UPPER TRAILING EDGE OF NUMBER 3 SLAT BOTTOM SIDE FROM CONTACT WITH HIGH SPOT IN FIXED LEADING EDGE. INSTALLED FLUSH DOUBLER PER SRM 51-70-10-2R.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

AFT GALLEY Z ANGLE MOUNT IS CORRODED AT STATION 1684 AND RIGHT BUTTLINE 50. INSTALLED NEW Z ANGLE PER SRM 51-40-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

CABIN AFT GALLEY Z ANGLE CORRODED AT STATIONS 1703 TO 1716 AND RIGHT BUTTLINE 50. REPLACED Z ANGLE PER SRM 51-10-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

CORROSION ON STATION 1640 FLOORBEAM AT RIGHT BUTTLINE 3. REPAIRED FLOORBEAM PER EA B757-53-019779.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

CABIN AFT GALLEY CENTER MOUNT HAT CHANNEL IS CORRODED AT STATION 1714 AND LEFT BUTTLINE 1. INSTALLED NEW AFT GALLEY CENTER HAT CHANNEL FROM STATIONS 1689 TO 1714 PER SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,281 hrs · 23,612 cycles

CORROSION ON FLOORBOARD SUPPORT AT STATION 1675 AT LEFT BUTTLINE 1. REPLACED FLOORBOARD SUPPORT PER SRM 51-10-02-G9.

Part: TRIM PANEL — DEFECTIVE (RUDDER) · airframe 65,487 hrs · 23,306 cycles

MIA - CREW REPORTED RUDDER TRIM FAILED DURING CLIMBOUT. NO INDICATIONS OR RUDDER MOVEMENT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED RUDDER AILERON TRIM PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 65,212 hrs · 23,205 cycles

SEAT 33D EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTOR FOR SEAT 33D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 64,119 hrs · 22,816 cycles

CREW REPORTED THAT THE AFT LEFT LAV SMOKE DETECTOR WAS CHIMING IN FLIGHT. NO SMOKE OR FIRE OBSERVED. CREW REPORTED AN ALERT 8 UPON SCHEDULED ARRIVAL INTO JFK. INSPECTED AND FOUND SMOKE DETECTOR FAULTY. REPLACED SMOKE DETECTOR AND ALL CHECKED NORMAL. NO SMOKE OR EVIDENCE OF FIRE PRESENT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (LT ENGINE) · airframe 64,081 hrs · 22,800 cycles

MBJ - INFLIGHT UIO-MIA - CREW REPORTED LEFT ENGINE PRESSURE RATIO TRANSMITTER FAILURE CAUSING FALSE ENGINE INDICATIONS. EMERGENCY DECLARED FLIGHT DIVERTED MBJ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE PRESSURE RATIO TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT) · airframe 62,339 hrs · 22,175 cycles

PUJ - LEFT ENGINE FAILURE ON 4 MILE FINAL (SINGLE ENGINE TIME 2 MINUTES). NO FIRE WARNING. EMERGENCY DECLARED LANDED PUJ WITHOUT INCIDENT. A SMALL FIRE WAS REPORTED ON ENGINE UPON LANDING. LEFT FIRE BOTTLE USED ON LEFT ENGINE. AIRCRAFT REMOVED FROM SERVICE. FOUND TEMPERATURE EXCEEDANCE 945 AND ENGINE CHANGE DECLARED. REPLACED LEFT ENGINE ON 05/09/2010 AT PUJ. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 62,240 hrs · 22,136 cycles

TRAILING AFT INBOARD UPPER HOLE INDICATES A CRACK AND OUTBOARD UPPER AFT HOLE INDICATES A CRACK. ACCOMPLISHED DOUBLER REPAIR IN ACCORDANCE WITH EA B757-54-010091 AND FAA-AD CARD F1566AC.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,240 hrs · 22,136 cycles

CRACKS IN FLOORBEAM STATION 700 AT LEFT BUTTLINE 24 AND LEFT BUTTLINE 45.5. INSTALLED DOUBLERS ON FLOORBEAM PER AARD 53-30-51-2 REPAIR 2 AND CARD 53-98-01.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 62,240 hrs · 22,136 cycles

AREAS OF CORROSION ON LEADING EDGE OF NUMBER 3 SLAT. REPAIRED PER AARD 57-43-00-1 AND AARD 57-43-00-3.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,240 hrs · 22,136 cycles

ONE FASTENER ON NUMBER 3 SLAT BOTTOM SKIN 30 INCHES FROM INBOARD END HAS CORROSION AROUND IT. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: BATTERY PACK — WEAK (CABIN) · airframe 61,542 hrs · 21,882 cycles

EMERGENCY LIGHT AT SEAT 25D AFT DOORS DIM. REPLACED BATTERY PACK.

Part: SPLICE — BROKEN (CABIN) · airframe 61,281 hrs · 21,800 cycles

EMERGENCY LIGHT AT MID LAVATORY WALL INOPERATIVE. FOUND WIRE SPLICE BROKEN AT LOWER WALL. REPLACED SPLICE.

Part: SHROUD — DAMAGED (CABIN) · airframe 60,809 hrs · 21,650 cycles

EMERGENCY LIGHT AT SEAT 18D SHROUD DAMAGED. REPLACED SHROUD AT SEAT 18D.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,809 hrs · 21,650 cycles

SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS ARE DIM. REPLACED BATTERY PACK M10798.

Part: CONNECTOR — LOOSE (CABIN) · airframe 60,193 hrs · 21,444 cycles

SJU - EMERGENCY LIGHT FOR SEAT 36D INOPERATIVE. REINSTALLED LOOSE CONNECTOR AT 36F SIDEWALL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 57,302 hrs

SFO - EMERGENCY LIGHT AT RT NR ONE DOOR INTERIOR AND EXTERIOR AND EXIT SIGN NEXT TO MID LAVATORY INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHTS AT RT NR ONE DOOR INTERIOR AND EXTERIOR AND EXIT SIGN NEXT TO MID LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: SHROUD — BROKEN (EMERGENCY LIGHTS) · airframe 56,246 hrs

DFW - EMERGENCY LIGHT AT SEAT 1E HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,246 hrs

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 14D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

MIA - SEAT MOUNTED EMERGENCY ESCAPE LIGHTS FROM SEAT 25 TO AFT GALLEY INOPERATIVE. REPLACED AFT BATTERY CHARGER AND BATTERY FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEATS 25 TO AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HARNESS — FAULTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT HARNESS AND LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED WIRE TO FLIGHT DECK EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, L3 DOOR EMERGENCY EXIT AFT SIDE SIGN WAS FOUND BROKEN. REPLACED L3 DOOR AFT SIDE EMERGENCY EXIT SIGN LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — SHORTED (CABIN)

DFW - DUIRNG OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. REPAIRED SHORTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM FIRST CLASS CABIN TO FORWARD GALLEY INOPERATIVE. REPLACED TWO BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INDICATOR — REQ RESET (LT TE FLAPS)

LAX - FLT 649 - DURING DESCENT INTO SNA, FLAP ASYMMETRY WARNING CAME ON AFTER SELECTING 1 DEGREE FLAP. ACCOMPLISHED EMERGENCY CHECKLIST AND LOWERED FLAPS BY ALTERNATE METHOD TO 20 DEGREES. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. RESET LEFT INBOARD FLAP TRANSMISSION OVER TORQUE INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — GOUGED (BS 376)

AFW - FOUND FUSELAGE SKIN AT STATION 376 AND STRINGER 20R HAS GOUGE BLENDED BEYOND SRM. DYE CHECKED, FOUND NO CRACK, BLENDED GOUGE PER SRM 53-00-01-1. DIGITAL THICKNESS PARENT .080 PERFORMED EDDY CURRENT INSPECTION, NO CRACKS NOTED. (M)