N447FE

Part: SEALANT — LOOSE (SERVICE DOOR) · airframe 42,002 hrs · 29,718 cycles

FUSELAGE AT LAVATORY SERVICE PANEL, SEALANT LOOSE. NO CORROSION WAS FOUND AND VERIFIED WITH NDT.

Part: STRUCTURE — DAMAGED (ELEVATOR) · airframe 41,816 hrs · 29,533 cycles

HORIZ STAB - RT ELEVATOR T/E FRACTION NR 4 DAMAGED DUE TO ACCIDENTAL DAMAGE WITH A WORK STAND. RT ELEVATOR WAS INSPECTED AND REPAIRED IAW EA 6-5520-141545.

Part: SKIN — DAMAGED (ZONE 300) · airframe 41,816 hrs · 29,533 cycles

RT ELEVATOR T/E LOWER SKIN SURFACE WITH DEBONDING FROM 2500MM OF ER 40. RT ELEVATOR LOWER SKIN WAS REPAIRED IAW SRM 55-21-11 FIG 210.

Part: SKIN — DAMAGED (TE FLAP) · airframe 41,816 hrs · 29,533 cycles

LT WING - EXISTING REPAIR AT T/E OF FLAP INBD WITH DEBONDS. LT WING FLAP INBD WAS REPAIRED IAW SRM 57-52-12, FIG 204.

Part: SKIN — GOUGED (ZONE 500) · airframe 41,816 hrs · 29,533 cycles

LT WING - DETECTED NICK AT HOLE NR 63 -EO 6-5710-7-3322PT1. HOLE NR 63 REPAIRED IAW EA 6-5710-141544.

Part: SKIN — DAMAGED (ZONE 300) · airframe 41,816 hrs · 29,533 cycles

LT ELEVATOR - T/E LOWER SKIN SURFACE WITH DEBONDING AT ELEVATOR AT 3300MM FROM TOP INBD. LT ELEVATOR LOWER SKIN SURFACE WAS REPAIRED IAW SRM 55-21-11 FIG 210.

Part: SKIN — DAMAGED (ZONE 300) · airframe 41,816 hrs · 29,533 cycles

RT ELEVATOR - T/E LOWER SKIN SURFACE WITH DEBONDING (600MM X 100MM, SPANWISE X CORDWISE) AT 300MM FROM ER 40. RT ELEVATOR T/E LOWER SKIN WAS REPAIRED IAW EA 6-5520-141514A.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 41,816 hrs · 29,533 cycles

RT WING - FLAP OUTBD UPPER SKIN WITH 2 SCRATCHES BTW RIB 2 AND RIB 3. FLAP UPPERSKIN WAS REPAIRED IAW EA 6-5758-141543.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 41,816 hrs · 29,533 cycles

MDCC - CLS LOCATED AT FR54.2 BTW Y-450 AND Y-950 FOUND CRACKED. CLS REPLACED IAW SRM 51-72-10.

Part: SEAT TRACK — WORN (ZONE 100) · airframe 41,816 hrs · 29,533 cycles

CLS ADAPTER AT FR36 BTW SEAT TRACKS "D" AND "E" RT FOUND WORN AT LOCKS THE CLS WAS REPLACED IAW SRM 51-72-10.

Part: SEAT TRACK — WORN (ZONE 100) · airframe 41,816 hrs · 29,533 cycles

FWD CABIN - SEAT TRACK "D" LT WORN AT LOCKS BTW FR 36-37. SEAT-TRACK WAS REPAIRED IAW EA 6-5310-141513.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 41,816 hrs · 29,533 cycles

CLS LOCATED AT FR 54.3 AND BTW Y-450 AND Y-950 FOUND CRACKED. CLS WAS REPLACED IAW SRM 51-72-10.

Part: SEAT TRACK — WORN (ZONE 100) · airframe 41,816 hrs · 29,533 cycles

AFT - SEAT TRACK FOUND WORN AT LOCKS LOCATED AT FR79, Y 1450. SEAT TRACK REPLACED IAW THE SRM 51-72-10.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,816 hrs · 29,533 cycles

SUPERFICIAL CORROSION AT FR14RT BTW Z-80 AND S44R. THE CORROSION WAS FOUND TO BE OUTSIDE LIMITS, ACCORDINGLY THE FRAME WAS REPLACED IAW SRM 51-72-10.

Part: SEAT TRACK — WORN (ZONE 100) · airframe 41,816 hrs · 29,533 cycles

SEAT TRACK Y-450 WITH WEAR BTW FR 40/41 AND 42. SEAT TRACK WAS REPLACED IAW SRM 51-72-10.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 41,816 hrs · 29,533 cycles

AFT CARGO COMPT -BULK- LT INTERCOSTAL FOUND CRACKED BTW FR 68-69. THE AFFECTED PART WAS REPLACED IAW SRM 51-72-10.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 41,816 hrs · 29,533 cycles

RT WING - FLAP OTBD T/E SKIN SURFACE DEBONDED (1360MM LENGHT BY 190MM WIDTH) BETWEEN RIB 2 AND RIB 4. RT WING FLAP OTBD WAS REPAIRED IAW EA 6-5750-140260.

Part: SKIN — DENTED (NR 2 SLAT) · airframe 41,816 hrs · 29,533 cycles

LT WING - SLAT NR 2 WITH DENT ON EXTERIOR SKIN SURFACE BTW RIB 38 AND 39. SLAT WAS REPAIRED IAW SRM 57-43-11, FIG 202.

Part: FITTING — CRACKED (ZONE 500) · airframe 40,565 hrs · 28,495 cycles

LT WING, THREE CRACKS AT CENTRAL FITTING ATTACHMENT TO ACTUATOR AT NUMBER 4 LT SPOILER REPLACED FITTING IN ACCORDANCE WITH EA 6-5750-115315, SB A310-57-2057, IPC 57-73-11-01 AND SRM 57-73-11.

Part: BUSHING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

LT WING OUTB FLAP, FITTING WITH UPPER BUSHING ATTACHMENT TO NR 3 TRUNNION WITH SPOTS OF CORROSION. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5710-117224.

Part: FAILSAFE — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

FUSELAGE, CORROSION FOUND ON TOP SURFACE OF RT FWD PAX DOOR FAIL/SAFE RING, BETWEEN FR 14 AND 14B. FAIL/SAFE RING REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5310-117229 AND RAS/AS/023/2008 ISSUE A.

Part: TRUNNION — WORN (ZONE 600) · airframe 40,565 hrs · 28,495 cycles

RT WING NR 3 FLAP OUTBOARD TRUNNION WITH WEAR. TRUNNION NR 3 RT WAS REMOVED, REPAIRED PER CMM 57-53-12 AND INSTALLED PER AMM 27-54-37.

Part: TRUNNION — WORN (ZONE 600) · airframe 40,565 hrs · 28,495 cycles

RT WING NR 4 TRUNNION OF OUTBD FLAP WITH WEAR. TRUNNION NR 4 RT WAS REMOVED, REPAIRED PER CMM 57-53-12 AND INSTALLED PER AMM 27-54-37.

Part: TRUNNION — CORRODED (ZONE 500) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

LT WING, INBD FLAP NR 1 TRUNNION WITH CORRODED AREA AND EXCESSIVE WEAR. TRUNNION NR 1 LT WAS REPAIRED IN ACCORDANCE WITH CMM 57-52-15.

Part: FLOORBEAM — MISREPAIRED (BS 3514) · airframe 40,565 hrs · 28,495 cycles

N00529 LOWER FUSELAGE, PREVIOUS REPAIR FOUND LOCATED ON AFT CARGO FLOORBEAM OF FR 65, Y-950. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW BEAM P/N A5397422122451. INSTALLED IN ACCORDANCE WITH SRM 51-72-10.

Part: SKIN — DAMAGED (ZONE 500) · airframe 40,565 hrs · 28,495 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT (FLAP INBD UPPER SKIN) RIB 2/4 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIR WAS FOUND DAMAGED AND IT WAS REMOVED. NEW REPAIR WAS DONE PER SRM 57-52-12.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 40,565 hrs · 28,495 cycles

MDCC - SEAT TRACK Y-1970 BETWEEN FR60 AND FR61 FOUND CRACKED. THE ATA CHAPTER FOR THIS SDR IS IN FACT 5310, INSTEAD OF THE 5611 INSERTED ABOVE. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 40,565 hrs · 28,495 cycles

AFT CARGO COMPARTMENT, ATTACHMENT FITTING OF CROSSBEAM TO FR 64 AT Y-1400, FOUND CRACKED. THE FITTING WAS REPLACED IAW SRM 51-72-10 AND 51-40-21.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 40,565 hrs · 28,495 cycles

AFT CARGO COMPARTMENT, CROSSBEAM OF FR 61 WITH CORROSION AT Y 1004. CROSSBEAM REWORKED IAW EA 6-5310-115317.

Part: STRINGER — CORRODED (BS 3090-3143) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

AFT CARGO COMPARTMENT, SUPERFICIAL CORROSION BETWEEN FR 54.3 AND 55, STGR 52LH. CORROSION WAS REWORKED IN ACCORDANCE WITH SRM 51-74-10 WITH A MAXIMUM DEPTH OF 0.013". REWORK AUTHORIZED PER FEDEX EA 6-5310-115316.

Part: STRUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

TAIL CONE, SMALL SPOTS OF CORROSION AT LT AFT TRACK ATTACHMENT FITTING AT FRAME 87. STRUT-CROSS WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.

Part: STRINGER — CORRODED (BS 3143-3196) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

AFT CARGO COMPARTMENT, SUPERFICIAL CORROSION AT FR 58/59, STGR 56 LT. CORROSION WAS REMOVED IN ACCORDANCE WITH SRM 51-74-10 WITH A MAXIMUM DEPTH OF 0.008". REWORK AUTHORIZED PER FEDEX EA 6-5310-115316.

Part: TRUNNION — CORRODED (ZONE 500) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

LT WING, FLAP OUTBD NR 4 TRUNNION WITH SPOTS OF CORROSION AND EXCESSIVE WEAR. TRUNNION NR 4 LT WAS REPAIRED IN ACCORDANCE WITH CMM 57-53-12.

Part: STRINGER — CORRODED (BS 3249-3408) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

AT CARGO COMPARTMENT, SUPERFICIAL CORROSION AT FR 60/63, STGR 47 RT. CORROSION WAS REMOVED IN ACCORDANCE WITH SRM 51-74-10, WITH A MAXIMUM DEPTH OF 0.008". REWORK AUTHORIZED PER FEDEX EA 6-5310-115316.

Part: ATTACH FITTING — CRACKED (CARGO BAY) · airframe 40,565 hrs · 28,495 cycles

AFT CARGO COMPARTMENT FLOOR, AFTER AN HFEC INSPECTION NTM 52-32-04 PART6, CRACKS WERE FOUND ON FLANGE OF DOOR ACTUATOR ATTACH FITTING. THE FRAME WAS SPLICED IN ACCORDANCE WITH EA 6-5230-117223.

Part: RIB — DAMAGED (ZONE 100) · airframe 40,565 hrs · 28,495 cycles

TAIL CONE, RIBS BETWEEN FR 84 AND 86, AND STRINGER 32 LT DAMAGED, RIBS (SECTION-L) WERE REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.

Part: RIB — DAMAGED (ZONE 100) · airframe 40,565 hrs · 28,495 cycles

TAIL CONE, RIBS BETWEEN FRAME 85 TO 87 AND STRINGER 33 RT DAMAGED. THE RIBS (SECTION-L) WERE REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.

Part: STRUT — CORRODED (TAILCONE) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

TAIL CONE, SMALL SPOTS OF CORROSION AT TRACK LT, ATTACHMENT FITTING TO FR 86, STRUT-CROSS WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,565 hrs · 28,495 cycles

MDCC - ANGLE SUPPORT AT FR43 FLOOR LEVEL FOUND CRACKED AT Y 2860. THE ANGLE WAS REPLACED IAW SRM 51-72-10 AND EO51-40-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,565 hrs · 28,495 cycles

FLOORBEAM CRACKED AT FR 54.3 AND Y-680. FLOORBEAM REPAIRED IAW EA 6-5310-115317.

Part: STRUT — CORRODED (TAIL CONE) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

TAIL CONE, SMALL SPOTS OF CORROSION AT TRACK LT, ATTACHMENT FITTING TO FR 86. STRUT-CROSS WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 40,565 hrs · 28,495 cycles

CROSSBEAM OF FR 54.3 CRACKED AT Y-680.

Part: BEAM — CORRODED (ZONE 400) · corrosion level 2 · airframe 40,565 hrs · 28,495 cycles

NR 2 PYLON, AFT ATTACHMENT BEAM ASSEMBLY WITH CORROSION ON MATING FACE. CORROSION OUT OF LIMITS, REPLACED BEAM ASSEMBLY IAW SRM 54-51-81 AND AMM 54-51-85.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 40,565 hrs · 28,495 cycles

MDCC - SEAT-TRACK AT Y-2456 BETWEEN FR 38.2 AND FR40 WITH CRACK. SEAT-TRACK WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,565 hrs · 28,495 cycles

FUSELAGE LWR LOBE, FUSELAGE SKIN WITH SCRATCHES ON THE EDGE OF FR 20A - FWD CARGO COMPARTMENT DOOR FWD FRAME. FUSELAGE SKIN SURFACE REPAIRED IAW EA 6-5330-117222.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,565 hrs · 28,495 cycles

FOUND DENT ON FUSELAGE AT FR 49/50 AND STR 36/37 LT. THE DENT WAS REPAIRED IAW FEDEX EA 6-5330-115319.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 38,124 hrs · 27,036 cycles

COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT. INSPECTED IAW CFR 121.368. PREVIOUS REPAIR INSTALLED LEFT SIDE OF FUSELAGE AT FS 70 TO FS 71, STR 27LT TO 31LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. NEW REP ACCOMP PER SRM 53-10-12 FIG 225 SHEET 2. REP EVALUATED PER GMM 6-2-100 AND CLASSIFIED MAJOR.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 38,055 hrs · 26,993 cycles

ON T/O ROLL RW 36R AT TUL NOTED NO AIRSPEED INDICATION ON CAPTS PFD REJECTED TO BELOW 80 KTS. BLEW OUT CAPTS PITOT TUBE CHECKED GOOD WITH PITOT STATIC TESTER.

Part: OUTFLOW VALVE — FLUCTUATES (CABIN PRESSURE) · airframe 37,824 hrs · 26,834 cycles

A/C WOULD NOT PRESSURIZE ON CLIMB-OUT OF MEM. LEVELED OFF AT 9000. CABIN VSI CLIMBING AT SAME RATE AS A/C CLIMB. NR 2 FWD AND AFT VALVES DISPLAYED FULL OPEN AND AMBER IN COLOR. NR 1 FWD AND AFT OUTFLOW VALVES OSCILLATED VIOLENTLEY OPEN AND CLOSED THROUGH FLT. RETURNED AND LANDED IN MEMPHIS. NO ECAM FAULTS DISPLAYED THROUGH OUT WITH REGARD TO REG NR 1 OR NR 2. FOUND UNION WHERE AFT NR 2 JET PUMP HALVES CONNECT VERY LOOSE. TIGHTENED CONNECTION, ALSO REMOVED JET PUMP IAW A310 MM 21-31-00-5-01. PUMP WAS CLEAN OF ANY DIRT OR OTHER OBSTRUCTIONS. REINSTALLED IAW SAME REF. REMOVED REPLACED RELAYS 60GB (RLY-MLG) AND 45GB(RLY-MLG). PERFORMED ADJ/TEST IAW A310 MM 21-31-00-5-01. ALL TESTS PASSED.

Part: COALESCER BAG — CONTAMINATED (CABIN AIR) · airframe 37,779 hrs · 26,799 cycles

ON FINAL NR 2 TURBINE INLET TEMP AT 100C, ECAM ADVISORY FLASHING, SHORTLY THEREAFTER SMELLED FUMES IN COCKPIT. TURNED OFF NR 2 PACK. DECLARED EMERGENCY. COMPLIED WITH CFM PROCEDURES, LANDED UNEVENTFULLY. BITE CHECKED NR 2 PACK TEMP CONTROLLER (NO FAULTS FOUND). REPLACED NR 2 PACK WATER SEPARATOR COALESCER BAG IAW M/M 21-51-16-3. NR 2 PACK OPERATES NORMALLY, OK FOR SERVICE.

Part: DISPLAY — INTERMITTENT (COCKPIT) · airframe 37,599 hrs · 26,696 cycles

REJECTED TAKEOFF IND DUE TO F/O PFD & ND BLANKING AT ABOUT 95 KTS. DISPLAYS RETURNED BY THE TIME THE A/C STARTED SLOWING. BACK TO RAMP TO ALLOW BRAKES TEMPS TO COOL NO OTHER PROBLEM DEVELOPED WITH PFD/ND APPEARED NORMAL. SECOND TAKEOFF NORMAL. MALFUNCTION NOT VERIFIED ON GRD. F/O'S PFD & ND CK GOOD PER A310 AMM 34-71-00-5.

Part: THRUST REVERSER — INOPERATIVE (NR 1) · airframe 37,449 hrs · 26,591 cycles

PDIS 447 78-30 0007243 27OCT04 MCI OPEN U NR 1 REVERSER UNLOCK LITE ON T/O. REJECTED T/O AT 70 KNOTS. MEL 27OCT04 05:03 MCI U ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 06NOV04 (MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOPERATIVE, THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION.) MOCC CONTROL NR 212950, EXP DATE 11/06/04. C/0212950 ENT BY: 042537 RPT BY: 042537.

Part: VALVE — INOPERATIVE (THRUST REVERSER) · airframe 37,246 hrs · 26,454 cycles

PDIS 447, 78-30 0007040 05AUG04 CAE OPEN ON T/O AT 43 PERCENT N1,GOT REV UNLOCK LIGHT. MEL 05AUG04 05:40 CAE R ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 15AUG04 MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2)1. THRUST REVERSER, INOPERATIVE. THRUST REVERSER IS DEACTIVATED R&R MASTER ACTUATOR - NO HELP R & R RT FEEDBACK MECHANISM, PRESSER REG. VALVE FACT TUL 10 AUG 04

Part: THRUST REVERSER — INOPERATIVE (NR 1 ENGINE) · airframe 36,916 hrs · 26,236 cycles

NR 1 ENG REVERSER OPERATING LIGHT CAME ON (AMBER) AS TAKEOFF POWER WAS APPLIED AT ATL. THE LIGHT WENT OUT AFTER THE THROTTLE WAS BROUGHT BACK TO IDLE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 16MAR04 MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) 1 REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FWD THRUST POS.

Part: WINDOW — CRACKED (COCKPIT) · airframe 36,376 hrs · 25,859 cycles

AFT EDGE OF CAPT'S SIDE VIEW WINDOW GLOWED WHITE HOT IN TWO SPOTS. THERE WAS A NOTICABLE BURNING ODOR AND A SMALL AMOUNT OF SMOKE. TURNED OFF WINDOW HEAT AND BURNING STOPPED. RETURNEDTO MEMPHIS. FOUND CRACK IN WINDOW. REMOVED AND REPLACED LEFT FIXED SIDE WINDOW IAW M/M 56-11-12-4 OPS CK IAW M/M 30-42-00-5 GOOD OK FOR SERVICE PER MTSI WRI 56-10-6335 ALSO REMOVED AND REPLACED CONTROLLER 19DG AND PROTECTION UNIT 87DG ALSO CK GOOD PREMATURE REMOVAL/INSTALLATION OFF MFG NP175233-1 POS LT SRL 94168H8065 TAG 928284 ON MFG NP175233-1 SRL 03037H5905 TAG 830268.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 35,698 hrs · 25,487 cycles

ON TAKEOFF, POWER APPLICATION NR 1 REV UNLOCK LIGHT ILLUMINATED. REJECTED TAKE OFF AND RETURNED TO RAMP, WHEN POWER REDUCED, LIGHT WENT OUT. AC RELEASED FOR SERVICE IAW MEL/CDL 78-31-01 CATEGORY C. ENGINE NR 1 REV UNLK - INOPERATIVE. AFFECTED THRUST (1 OR 2) REVERSER DEACTIVATED.

Part: LINE — KINKED (NR 1 ENGINE)

NR 1 THROTTLE SPLIT 12 DEG TA MORE THAN NR 2, NR 1 NACELLE TEMP 35-45 DEG HOTTER THAN NR 2. REMOVED AND REPLACED PT2/TT2 SENSOR AND THE TT2 SENSOR. REMOVED AND REPLACED KINKED PT7 LINE AND RESEALED 1, 2, 3, 12, 13, 14 AND 16 FUEL NOZZLE PAD AIR LEAKS ALL ON NR 1 ENGINE.

Part: FUEL CONTROL — FAULTY (NR 1 ENGINE) · airframe 34,681 hrs · 24,964 cycles

ON TAKEOFF THROTTLES WERE 2 KNOB WIDTH APART ON CLIMB NR 1 ENG W/N REACH FULL PWR. DURING DESCENT NR 1 IDG ADVISORY ILLUM AND TEMP REACHED 144 DEG. REMOVED AND REPLACED PRSOV DIFFUSER CASE LINER REWORKED. REMOVED AND REPLACED AIR HEAT EXCHANGER SOV VALVE.

Part: REGULATOR — FAULTY (NR 1 ENGINE) · airframe 34,681 hrs · 22,964 cycles

ON TAKEOFF THROTTLE WERE 2 KNOB WIDTHS APART. NR 1 ENG W/N REACH FULL CLIMB PWR. DURING DESCENT NR 1 ENG IDG ADVISORY ILLUMINATED & TEMP REACHED 144 DEG. REMOVED AND REPLACED PRESS REGULATOR & SHUTOFF VALVE. TRIMMED HEATSHIELD, LEAK CHECK GOOD.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 34,453 hrs · 24,880 cycles

NR 1 ENGINE COMPRESSOR STALL AT FL 350. THIS WAS FOLLOWED BY COMPLETE LOSS OF OIL PRESS, FOLLOWED ECAM PREC ENGINE SHUTDOWN. ENG WIND MILLED FOR ABOUT 30 MIN. REMOVED AND REPLACED NR 1 ENGINE.

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG) · airframe 33,991 hrs · 24,572 cycles

AFT T/O GEAR WOULD NOT RETRACT SYS 1, SYS 2 OK. GOT WARNING, ATS PITCH TRIM PRESS AND PITOT HEAT FAULTS.

Part: COMPUTER — FAULTY (PROXIMITY BOX) · airframe 33,385 hrs · 24,095 cycles

AFT T/O BOTH CAPT AND F/O LOST FLT DIR. CAPT LOST ADC BOTH PITCH TRIMS AND YAW DAMPNERS TRIPPED OFF. REMOVED AND REPLACED PROX BOX COMPUTER AND PERF ALL OPS CK. ALL SYS CHECK GOOD.

Part: PROXIMITY SWITCH — FAILED (RT MLG) · airframe 33,385 hrs · 24,095 cycles

RT MLG DID NOT LOCK DOWN FOR SEVERAL MIN AFT GEAR HANDLE LOWERED. REMOVED AND REPLACED PROX UNIT COMPUTER AND PERF SEVERAL MORE EXT, AND RETRACTION WITH NO DEFECTS.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 32,884 hrs · 23,796 cycles

A/C HAD NR 2 BLEED FAULT.