N332AA

Part: LENS — MISSING (CABIN) · airframe 96,699 hrs · 19,222 cycles

EMERGENCY LIGHT COVER MISSING (BI-DIRECTIONAL ARROWS) AT BASE OF AISLE BY AFT LEFT LAVATORY. REPLACED MISSING LENS COVER.

Part: EXHAUST VALVE — DEFECTIVE (E&E BAY) · airframe 94,691 hrs · 18,812 cycles

LAX - CREW REPORTED UNABLE TO PRESSURIZE AICRAFT AFTER TAKEOFF. SWITCHED TO AUTO CONTROLLER NUMBER 2 AND THEN TO MANUAL BUT UNABLE TO CONTROL CABIN ALTITUDE. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED E AND E EQUIPMENT COOLING OVERBOARD EXHAUST VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 93,993 hrs · 18,666 cycles

RIGHT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT EXTERIOR EMERGENCY EXIT LIGHT.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,895 hrs · 18,442 cycles

STATION 1153 J-CAP HAS CORROSION UNDER ROLLER TRAYS AT LEFT BUTTLINE 8 TO 12 AND RIGHT BUTTLINE 8 TO 12. INSTALLED REPAIR ANGLE PER FLANGE NOTE M BAC1503-100018 7075-T6. INSTALLED 3 TAPPERED SHIMS FOR FW STIFFENERS AND 2 RADUIS BLOCKS FOR 1/4 IN NUT PLATES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,895 hrs · 18,442 cycles

DISCOVERED THAT STRINGER 34 RIGHT BETWEEN STATIONS 434 TO 456 HAS AREA OF CORROSION AROUND FASTENER. REMOVED CORROSION PER SRM 51-10-02. CUT AND REMOVED DAMAGE SECTION OF STRINGER. NO CORROSION NOTED ON SKIN. FABRICATED REPAIR PARTS PER SRM 53-30-03-2R. INSTALLED STRINGER 34R PER SRM 53-30-03-2R.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,895 hrs · 18,442 cycles

DISCOVERED STRINGER 37 RIGHT BETWEEN STASTIONS 434 TO 456 HAS AN AREA OF CORROSION JUST AFT OF STRINGER SPLICE REPAIR., REMOVED DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS PER SRM 53-00-03-2R 2. INSTALLED STRINGER 37R PER SRM 53-00-03.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,895 hrs · 18,442 cycles

STRINGER 37 LEFT BETWEEN STATIONS 434 TO 456 AND STATIONS 412 TO 434 HAS CORROSION ON OUTBOAD SIDE. CUT AND REMOVED DAMAGED SECTION OF STRINGER PER SRM 53-00-03-2R. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03-2R.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,895 hrs · 18,442 cycles

DISCOVERED THAT STRINGER SPLICE REPAIR ON STRINGER 39 RIGHT BETWEEN STATIONS 434 TO 456 AND STATIONS 412 TO 434 HAS AREAS OF CORROSION ON FLANGES. REMOVED LIGHT SURFACE CORROSION BETWEEN STATIONS 412 AND 434 WITHIN LIMITS PER SRM 53-00-03-1A. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03-2R.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,895 hrs · 18,442 cycles

CORROSION FOUND AT STRINGER 35 LEFT BETWEEN STATIONS 412-434. CUT OUT AND REMOVED DAMAGED AREA. ACCOMPLISHED SPLICE REPAIR PER AARD 51-20-00-02 AND SRM 53-00-03.

Part: CONNECTOR — BROKEN (CABIN) · airframe 89,750 hrs · 17,812 cycles

FOUND ALL EMERGENCY EXIT LIGHTS INOPERATIVE ON LEFT SIDE FROM ROW 31 AFT. FOUND BROKEN CONNECTOR FOR EMERGENCY PATH LIGHTING BY SEATS 37 A AND B. REPLACED BROKEN CONNECTOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,750 hrs · 17,812 cycles

FOUND ALL EMERGENCY EXIT LIGHTS INOPERATIVE ON LEFT SIDE FROM ROW 31 AFT. REPLACED BATTERY PACK BY SEATS 36 A AND B. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,371 hrs · 17,734 cycles

LEFT NUMBER 4 DOOR AND LEFT SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY M738. OPS CHECKED NORMAL.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 84,648 hrs · 16,748 cycles

JFK - CAPTAIN REPORTED WHEN CHANGING FLAPS FROM 20 TO 25 DEGREES , RECEIVED A TRAILING EDGE DISAGREE LIGHT AND FLAPS STUCK MESSAGE ON GAUGE. EMERGENCY DECLARED, LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED FIM 27-51-00 AND FIM 27-58-00. CYCLED FLAPS SEVERAL TIMES, NO BITE FAULTS NOTED. ALL OPS CHECKS OK. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — FAILED (APU) · airframe 84,268 hrs · 16,669 cycles

LAX - AUXILIARY POWER UNIT FAILED AND LEFT ENGINE GENERATOR WAS ON PLACARD. EMERGENCY DECLARED, RETURNED TO LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY POWER UNIT OIL SENSOR AND NUMBER 1 ENGINE INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: IDG — FAILED (NR 1 GENERATOR) · airframe 83,420 hrs

DFW - NUMBER ONE GENERATOR ON PLACARD AND APU SHUT DOWN TWICE. APU WAS RUNNING BUT CAPTAIN ELECTED TO DIVERT. REPLACED NUMBER ONE ENGINE INTEGRATED DRIVE GENERATOR. REPLACED SENSOR FOR APU. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHTS AT SEATS 10B TO 17B INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — AUTO SHUTDOWN (ZONE 100)

SFO INFLIGHT - DURING CLIMB AUXILLIARY POWER UNIT (APU) AUTO SHUT DOWN WITH LEFT INTEGRATED DRIVE GENERATOR ON MEL. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED APU ON 20 NOV AT SFO. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,568 hrs · 16,313 cycles

AFW FUSELAGE SKIN AT STATION 1084 TO 1088 BETWEEN STRINGER 37 LT AND 38 LT HAD CORROSION ON THE OUTER SKIN SURFACE. AREA OF DISCREPANCY IS 2.4 INCHES BY 4.6 INCHES. REPAIRED PER MRB 767 3274.

Part: SKIN — DAMAGED (BS 532 S32R) · airframe 82,568 hrs · 16,313 cycles

AFW FUSELAGE SKIN APPROXIMATELY 10 INCHES FORWARD OF FORWARD CARGO DOOR AT STRINGER 32 RT HAD A GOUGE BLENDED BEYOND SRM LIMITS. AREA OF DISCREPANCY IS 2 INCHES BY 1 INCH WITH A DEPTH OF .050 INCH. MATERIAL REMAINING IS .156 INCH. HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS WITH NO FINDINGS. REPAIRED PER SRM 53-00-01-1A WITH EXCEPTIONS PER MRB 767 3276.

Part: STRINGER — CORRODED (BS 434-456) · corrosion level 2 · airframe 82,568 hrs · 16,313 cycles

AFW STRINGER WAS CORRODED AT STATION 451 DUE TO PREVIOUS REPAIR AT STATION 434. STATION 434 WILL NEED TO BE REPLACED TO ALLOW A REPAIR AT STATION 451. REPAIRED PER SRM 53-00-03-2R2 WITH EXCEPTIONS PER MRB 767 3278.

Part: STRINGER — CORRODED (BS 424-446) · corrosion level 2 · airframe 82,568 hrs · 16,313 cycles

AFW STRINGER WAS CORRODED FROM STATION 424 TO 446. REPAIRED PER SRM 53-00-03-2R2 WITH EXCEPTIONS PER MRB 767 3281.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,568 hrs · 16,313 cycles

AFW STRINGER WAS CORRODED FROM STATION 425 TO 443. REPAIRED PER SRM 53-00-03-2R2 WITH EXCEPTIONS PER MRB 767 3272.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,568 hrs · 16,313 cycles

AFW WHILE ACCOMPLISHING MX NDT FOUND INDICATIONS OF CRACKING AT RT OUTER CHORD AT LOWER AFT FASTENER AT 12A. HOLE REAMED TO .2807 INCH TO REMOVE CRACKING. REPLACED WITH OVERSIZED FASTENER PER MRB 767 3273.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,342 hrs · 82,342 cycles

JFK - EMERGENCY EXIT SIGN LIGHTS AT LT AND RT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHTS AT LT AND RT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,342 hrs · 82,342 cycles

JFK - EMERGENCY LIGHTS AT OVERHEAD MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: LENS — MISSING (CABIN) · airframe 81,751 hrs

JFK - EMERGENCY FLOOD LIGHT AT FORWARD GALLEY NEAR RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY FLOOD LIGHT AT FORWARD GALLEY NEAR RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (BS 434)

MCI - LEFT SKIN PANEL HAS CORROSION ON SURFACE OF PANEL AT LOWER AFT CORNER UNDER LAP SEAM AT STATION 434 LEFT STRINGER 37. AREA OF DISCREPANCY IS 1.75 INCHES BY 3.75 INCHES WITH A DEPTH OF APPROXIMATELY 50 PERCENT OF PANEL THICKNESS. TRIMMED DISCREPANT AREA OF SKIN PANEL TO REMOVE DAMAGE. INSTALLED EXTERNAL DOUBLER REPAIR AT LOCATION OF TRIM OUT PER MRB 767 2913 AND 2914.

Part: SKIN — DAMAGED (LT PYLON)

AFW - LEFT HAND PYLON INBOARD AND OUTBOARD SKIN AT STATION 250 HAS GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. AREA OF DISCREPANCY FOR INBOARD IS THREE INCHES BY 0.9 INCH WITH A DEPTH OF 0.055 INCH. AREA OF DISCREPANCY FOR OUTBOARD IS 2.5 INCHES BY 1 INCH WITH A DEPTH OF 0.058 INCH. REPAIRED PER MRB 767 2871 DATED 23 AUGUST 2006. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — FAILED (NR 2)

JFK - ON CLIMBOUT RIGHT HAND ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS. SLIGHT BANG HEARD AT 27000 FEET. FDR DOWNLOADED. FOUND METAL IN SCREEN. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EGRESS EMERGENCY LIGHT ON RIGHT SIDE OF ROWS 10 TO 30 AND TWO EACH LOWER EMERGENCY EXIT SIGNS AT RIGHT SIDE MID OVERWING ESCAPE LIGHTING INOPERATIVE. REPLACED CONTROL MODULES AND BATTERIES FOR EGRESS EMERGENCY LIGHT ON RIGHT SIDE OF ROWS 10 TO 30 AND TWO EACH LOWER EMERGENCY EXIT SIGNS AT RIGHT SIDE MID OVERWING ESCAPE LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RETAINER — WORN (PYLON SEAL)

MCI - NUMBER ONE AND TWO ENGINE THRUST REVERSER SEAL RETAINER RUBBED INTO PYLON STRUCTURE AT TOP AFT SIDE OF BOTH INBOARD AND OUTBOARD REVERSERS FOR NUMBER TWO ENGINE AND AT TOP AFT SIDE OF INBOARD THRUST REVERSERS FOR NUMBER ONE ENGINE. BLENDED WEAR AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION. CHECKED AREA FOR MATERIAL LOSS AND CRACKS. TRIMMED REVERSER SEAL RETAINER AND RIGGED REVERSER CLEARANCE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM 31H TO 37H TEST CIRCUIT ONLY. REPLACED EMERGENCY LIGHTS CONTROL MODULE BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTS FROM 31H TO 37H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (347)

FOUND FLOORBEAM UPPER FLANGE AT STATION 347 RBL 45.5 HAD CORROSION BLENDED BEYOND SRM LIMITS. REQ ENGINEERING APPROVAL TO REPAIR PER ATTACHED DRAWING. FLOORBEAM REPAIRED AT STATION 347 PER MRB 767-2428. (M)

Part: SKIN — DELAMINATED (HORIZ STAB)

AFW - LEFT OUTBOARD LOWER L/E AT STATION 160 ULTRA SOUND INSPECTION FOND A DELAMINATION INDICATION. TAP TEST GOOD REQUEST ENGINEERING APPROVAL TO CONTINUE AS IS. REPEAT INSPECTION EACH MBV TO RFS NR KK02-0021.

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE EMERGENCY EXIT LIGHT AT SEATS 1 THROUGH 9 INOPERATIVE. REPAIRED WIRING AT RIGHT SIDE EMERGENCY EXIT LIGHT CONNECTOR. (M)

Part: SIGN — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY BIDIRECTIONAL EMERGENCY EXIT SIGN ON FORWARD GALLEY INOPERATIVE. REPLACED BIDIRECTIONAL EMERGENCY EXIT FORWARD GALLEY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 20F INOPERATIVE. RESET EMERGENCY EXIT SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

SFO - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 28HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 28HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — LOOSE (CONNECTOR)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28H INOPERATIVE. RESECURED LOOSE PIN AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COFFEEMAKER — SPARKS (GALLEY)

LHR - DURING OVERNIGHT MAINTENANCE, AFT GALLEY COFFEEMAKER WHEN FIRST TURNED ON SPARKS APPEARED. REPLACED AFT GALLEY COFFEEMAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FIRE DETECTOR — DEFECTIVE (NR 2 ENGINE)

JFK - FLT 45 - EN ROUTE JFK-SFO - DETECTED FAILURE OF BOTH RIGHT SIDE ENGINE FIRE LOOP WARNING SYSTEM. AIR INTERUPTED, RETURNED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ENGINE LP 2 DETECTOR. PERFORMED LOOP RESISTANT CHECK. ACCOMPLISHED FIRE WARNING TEST PER THE MM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25J INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 25J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (ROW 2B)

ORD - FLT 83 - DURING MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROWS 2B THROUGH 9B INOPERATIVE. REPAIRED SHORT IN EMERGENCY EXIT WIRING AT AFT END OF E/E COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 33C INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 33C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DETECTOR — DEFECTIVE (CABIN)

LHR - FLT 46 - DURING CRUISE, FORWARD MID CABIN LAVATORY SMOKE DETECTOR CHIMED CONTINUOUSLY. REPLACED FORWARD MID CABIN LAVATORY SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP HOLDER — LOOSE (CABIN)

LHR - DURING MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 31B WOULD NOT ILLUMINATE. RECONNECTED LAMP HOLDER AND RESECURED WIRES AT SEAT ROW 31B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (LT ENGINE)

BRU - FLT 0088 - EICAS LEFT GENERATOR DRIVE MESSAGE AT LIFT-OFF ACCOMPANIED WITH AN OVERHEAD GENERATOR DRIVE LIGHT. STEADY INDICATIONS. DISCONNECTED LEFT GENERATOR DRIVE PER CHECKLIST. REMOVED AND REPLACED LEFT ENG IDG PER MM 20703. PERFORMED IDG. OPS CHECK AND LEAK CHECK ALL CHECKED GOOD. REMOVED PLACARD, CLEARED MIC. 33224F7C2/1419.05JAN.BRU. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 26A/B FOUND INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 26A/B. SYSTEM FOUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 32J INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT 32J. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ON PASSENGER SEAT 33F FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT 33F. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHORD — CORRODED (BS 1270)

AFW - INNER CHORD HAS CORROSION. REMOVED ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. ENSURE ALL CORROSION HAS BEEN REMOVED. BLEND OUT AREA OF CORROSION ON THE UPPER SURFACE OF THE INNER CHORD. TST: 42,915.43 HOURS. CYCLES: 8,368. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT WIRE FOUND PULLED OUT ON PAX SEAT 32H. REPLACED EMERGENCY EXIT LIGHT WIRE CONNECTOR ON PAX SEAT 32H AND RESECURED WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 23H INOPERATIVE. REPAIRED WIRES PULLED FROM EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)