N454FE

Part: PLATE — WORN (THRUST REVERSER) · airframe 32,212 hrs · 16,071 cycles

NR 2 ENG OTBD T/R COWL UPPER MID-SECTION INNER FACE FOUND ONE EACH PLATE WORN BY SPRING SEAL. ACCOMPLISHED THE WORK IAW EA 6-5410-T0208220.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,212 hrs · 16,071 cycles

FORWARD CARGO COMPARTMENT BILGE FRAME FOUND CORROSION AT FR 39, STRINGER 51R POSITION. CORROSION AREA CUT OUT & REINFORCED WITH REPAIR PART & FITTING TO INSTALLED IAW SRM 53-15-17. THE REPAIR CATEGORY B IAW 53-15-17-2-003-00.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,395 hrs · 15,546 cycles

IN CRUISE FL340, CAPTAIN'S WINDOW CRACKED IN TWO PLACES. CAPTAINS WINDOW HEAT FAULTED SHORTLY AFTER CRACK APPEARED. TURNED OFF WINDOW HEAT, NO FURTHER CRACKING. R & R CAPTAIN'S WINDSHIELD IAW MM 56-11-11-04.

Part: HINGE FITTING — GOUGED (RT NLG DOOR) · airframe 31,183 hrs · 15,400 cycles

RIGHT NLG AFT DOOR UPPER FWD HINGE FITTING HAS .2500" X .5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R RT NLG AFT DOOR UPPER FWD HINGE FITTING IAW SRM 51-72-10. REMOVED AND REINSTALLED FLOOR PANEL 122 PF IAW AMM 53-10-27-04. REMOVED AND REINSTALLED GROUND OPENING CONTROL ROD UPPER ATTACH HARDWARE AND BELLCRANK ATTACH HARDWARE IAW DWG A52810125 AND AMM 20-21-12. PERFORMED ADJUSTMENT OF RT AFT NLG DOOR IAW AMM 32-22-13-04.

Part: HINGE FITTING — GOUGED (LT NLG DOOR) · airframe 31,183 hrs · 15,400 cycles

LT NLG AFT DOOR UPPER FWD HINGE FITTING HAS .2500" X .5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R LT NLG AFT DOOR UPPER FWD HINGE FITTING IAW A310 SRM 51-72-10. REMOVED AND REINSTALLED FLOOR PANEL 121PF IAW A310-200 AMM 53-10-27-04. REMOVED AND REINSTALLED GROUND DOOR OPENING CONTROL ROD UPPER ATTACH HARDWARE AND BELL CRANK ATTACH HARDWARE IAW DWG A52810125 AND AMM 20-21-12. PERFORMED ADJUSTMENT OF LT AFT NLG DOOR IAW AMM 32-22-13-04, PARA 2.C.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 31,042 hrs · 15,303 cycles

NR 2 FUEL FLITER CLOG WOULD NOT GO AWAY AFTER QRH PROCEDURE. FOLLOWED ECAM AND QRH. DECLARED PRECAUTIONARY EMERGENCY. NR 2 ENG REMAINED AT IDLE REMAINDER OF FLIGHT. REF TSM 73-30-10, AMM 73-34-00-00, AMM 73-34-11-04, AND AMM 73-12-03-04: FOUND LIGHT STAYED ON AFTER ENGINE SHUTDOWN, WOULD EXTINGUISH WHEN DP SWITCH DISCONNECTED. R & R'D DP SWITCH, R &R D LP FUEL FILTER PRECAUTIONARY. LEAK CKS ACCOMPLISHED IAW JRH ACFT RELEASED FOR SVC THIS ITEM.

Part: COUPLING — LEAKING (E/E BAY) · airframe 30,782 hrs · 15,127 cycles

AFTER STARTING THE ENGINES DURING PUSHBACK THE COCKPIT FILLED WITH A LIGHT SMOKE WITH EYES AND THROAT BURNING. THERE WERE NO COCKPIT INDICATIONS OF ANY FIRE OR SMOKE. SMOKE STARTED TO DISSAPATE QUICKLY, DONNED OXYGEN MASKS. FOUND HYDRAULIC FLUID PUDDLED AND COVERING FLOOR AND DRIPPING FROM CEILING IN AVIONICS BAY. SOUND REDUCER AIR FILTER IS COVERED WITH HYD FLUID. FOUND THE STEERING CONTROL COUPLER LEAKING. R & R THE STEERING CONTROL COUPLER IAW AMM 32-51-14-04. OPS AND LEAK CHECKED GOOD. CLEANED DUCTS AND AREA OF HYD FLUID. RAN THE ENGINES AND PACKS IAW JRH. NO SMOKE OR ODORS DETECTED. OK FOR SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 30,652 hrs · 15,045 cycles

BLUE SYS HYD QUANTITY DECREASED IN FLIGHT SLOWLY UNTIL REACHED LO LEVEL WARNING, SECURED PUMP IAW ECAM AND QUANTITY STOPPED DECREASING, PRESSURE REMAINED ABOVE 3000 PSI UNTIL PUMP TURNED OFF. FOUND RETURN LINE TO BLUE MANIFOLD INSTALLATION SERVO CONTROL ACTUATOR LEAKING AT UNION, SEALS IN UNION DETERIORATED, REPLACED SEALS IAW AMM 29-12-34-04-0, NO LEAKS NOTED, OK FOR SERVICE. FINAL CLOSED.

Part: SIGNAL COND UNIT — FAILED (OIL PRESSURE) · airframe 30,596 hrs · 15,012 cycles

DURING T/O AT TYS AT 90 KNOTS - ECAM AND ENG 1 LIGHT - OIL HI PRESS - ILLUMINATED. CREW REJECTED T/O - LIGHT WENT OUT IMMEDIATLY. COMPLETED RTO CK LIST & QRH FOR OIL HI PRESS (NR 1 ENG) - ALL INDICATIONS WERE NORMAL. ALLOWED BRAKES TO COOL - THEN RAN UP ENGINES ON RUNWAY - ALL NORMAL- ALL INDICATIONS NORMAL. REPLACED ENG 1 SIGNAL CONDITIONER 11ES IAW AMM 79-33-31-04. ACCOMPLISHED IDLE ENG RUN, OIL PRESS INDICATIONS CHECK NORMAL IAW JRH. FINAL CLOSED.

Part: SKIN — CORRODED (ZONE 500) · airframe 30,267 hrs · 14,749 cycles

LEFT WING TOP SKIN HAS CORROSION AT REAR SPAR FASTENER, 6" OTBD OF RIB-4. LT WING CORROSION REMOVED BY BLENDING, NDT INSPECTED (NIL FINDINGS), NEW OVERSIZE TAPERLOCK FASTENERS INSTALLED AND SURFACE PROTECTION RESTORED. REF EA 6-5730- 145610.

Part: BRACKET — DAMAGED (NR 1 NACELLE) · airframe 30,267 hrs · 14,749 cycles

NR 1 ENGINE, NR 2 HYD SUCTION LINE HAS EXCESSIVE PLAY AT WING ATTACH POINT INSIDE NR 1 PYLON. LEFT WING, REWORKED HOLES 1,2,3,AND 4. R & R SUPPORT BRACKET BUSHING. REPAIR HOLES AND INSTALLED, NDT SKIN AND HOLES FOR CRACKS, NO CRACKS FOUND IAW EA 6-5720-145615.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 30,267 hrs · 14,749 cycles

AFTER SKIN REMOVED FOR REPAIR, FOUND FURTHER DELAMINATION APPROX. 8 SQ". REPAIRED RT ELEVATOR LOWER SURFACE EXISTING REPAIR DELAMINATED IAW SRM 55-21-11 PAR.5J PGS 257-262 AT RIB -14.

Part: SKIN — CHAFED (ZONE 600) · airframe 30,267 hrs · 14,749 cycles

RIGHT WING AFT SPAR ABOVE PYLON HYD LINE JAM NUT, LOOSE. REWORKED OVERSIZE HOLE IAW E-5720-145615. REWORKED AND INSTALLED NEW SUPPORT BRACKET BUSHING. REPAIRED HOLE IN BOTTOM WING SKIN IAW EA 6-5720-145615, NDT NR 2 PYLON SKIN AND HOLES FOR CRACKS-NO CRACK FOUND, RT WING AFT SPAR, PYLON.

Part: SKIN — CORRODED (LT ELEVATOR) · airframe 30,267 hrs · 14,749 cycles

LT ELEVATOR LOWER SURFACE AT RIB 9 HAS 6 SQ IN TOTAL AREA OF CORROSION. REPAIRED LT ELEVATOR LOWER SURFACE AT RIB 9 IAW SRM 55-21-11, PARA I, PGS 247-252 REF EA 6-5520-145621.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 30,267 hrs · 14,749 cycles

RT ELEVATOR LOWER SURFACE OTBD OF RIB 14 HAS 4 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION. REPAIRED RIGHT HAND ELEVATOR LOWER SURFACE IAW SRM 55-21-11,PARA 5I, DOUBLER REPAIR AT RIB 14 OF ELEVATOR. REFERENCE E.A. 6- 5520-145618.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 30,267 hrs · 14,749 cycles

RT ELEVATOR UPPER SURFACE AT RIB 17 HAS 2 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION. REPAIRED RT ELEVATOR UPPER SURFACE IAW SRM 55-21-11, PARA 5L PAGES 257-262. AND REFERENCE E.A. 6-5520-145618.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 30,267 hrs · 14,749 cycles

AFTER SKIN REMOVAL FOR REPAIR, FOUND FURTHER DELAMINATION APPROX 8 SQ IN. REPAIRED RT ELEVATOR LOWER SURFACE IAW SRM 55-21-11, PAR 5J, PGS 257-262 AT RIB 14 AND EA 6-5520-145618.

Part: SKIN — CORRODED (LT ELEVATOR) · airframe 30,267 hrs · 14,749 cycles

LOWER SURFACE LT ELEVATOR AT RIB 96 SQ IN CORROSION.

Part: COMPUTER — MALFUNCTIONED (ENG OIL PRESSURE) · airframe 28,367 hrs · 13,551 cycles

ENG 1 AFTER START, AMBER ECAM HI OIL PRESSURE IND (64 PSI), MOMENTARILY ON TAKEOFF ROLL AMBER ECAM-HI OIL PRESSURE, RTO. HI OIL PRESS (64PSI). LOWER OIL PRESSURE NR 1 (90C) REPLACED NR 1ENG OIL PRESSURE TRANSMITTER PER MM 79-33-11-04 AND NR 1FWC PER MM31-53-34-4. PERFORMED ENG 1 RUNUP AND ENHANCED THROTTLE PER A310 JRH. ALL PARAMETERS NORMAL AND OIL PRESSURE INDICATION NORMAL AND STABLE. LEAK CHK OK. CLOSED AND LATCHED NR 1 ENG COWLING PER MM71-10-00. ACFT OK FOR SVC.

Part: TRANSMITTER — MALFUNCTIONED (ENG OIL PRESSURE) · airframe 28,367 hrs · 13,551 cycles

ENG 1 AFTER START, AMBER ECAM HIGH OIL PRESSURE IND (64PSI), MOMENTARILY ON TAKEOFF ROLL AMBER ECAM-HIGH OIL PRESSURE, RTO. HIGH OIL PRESS (64PSI). LOWER OIL PRESSURE NR 1 (90C). REPLACED NR 1 ENG OIL PRESSURE TRANSMITTER PER MM 79-33-11-04 AND NR 1 FWC PER MM 31-53-34-4. PERFORMED ENG 1 RUNUP AND ENHANCED THROTTLE PER JRH. ALL PARAMETERS NORMAL AND OIL PRESSURE INDICATION NORMAL AND STABLE. LEAK CHK OK. CLOSED AND LATCHED NR 1ENG COWLING PER MM 71-10-00. ACFT OK FOR SVC.

Part: SIGNAL COND UNIT — MALFUNCTIONED (ENGINE OIL PRESS) · airframe 28,361 hrs · 13,548 cycles

REJECTED TAKEOFF. NR 1 ENGINE HIGH OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL APPROXIMATELY 85KTS. INDICATION DEFERRED PER MEL 79-33-01-02. REMOVED AND REPLACED NR 1 ENG OIL SIGNAL CONDITIONER P ER MM 79-33-31-4, PERFORMED OPERATIONAL TEST OF THE OIL PRESSURE AND LOP WARNING SYS SATI.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,170 hrs · 13,456 cycles

AFT CARGO DOOR CUTOUT FRAME 59A CORROSION AT LOWER END OF DOOR FRAME. PERFORMED REPAIR PER SRM 53-17 FIG 201 AND 202A AND EA NR 6-5320-125509.

Part: REGULATOR — FAILED (CABIN PRESSURE) · airframe 27,248 hrs · 13,038 cycles

DURING CLIMB-OUT WITH NR 1 REG DEFERRED, LOST NR 2 REG. USED MANUAL PRESSURIZATION FOR THE REST OF FLIGHT. ACN RELEASED FOR SERVICE PER MEL/CDL: 21-31-04-01-A. DEACTIVATED IN CLOSED POSITION. ENSURE CAB DIF PRESS IS ZERO PRIOR TO OPENING ANY DOOR." SWAPPED FWD TO AFT CABIN PRESSURE OUTFLOW VALVE AS PER WRI 21-30/7595. REMOVED AND REPLACED AFT OUTFLOW VALVE PER AMM 21-31-12-4 02. OPS TEST GOOD PER AMM 21-31-00-5 02. MEL CLEARED AND PLACARD REMOVED. A/C OK TO CONTINUE.

Part: AUTOPILOT SYS — UNKNOWN · airframe 25,810 hrs · 12,382 cycles

CLOSE R AP 1 AND 2 DO NOT ENGAGE. MTP FAULT REVIEW FOUND FCC 1/ FCC 2/FCU/TORQUE LIMIT RESET A/P 1 AND 2 BOTH FCC AND FCU. PERFORMED AFS/LAND ENGAGE TEST AS PER AMM 22-10-00-5 BOTH A/P CAN BE ENGAGED. A/C RETURNED TO SERVICE. MTP FAULT REVIEW FOUND FCC1/FCC2/FCU/TORQUE LIMITER, RESET A/P1 AND A/P2 BOTH FCC'S AND FCU, PERFORMED AFS/LAND ENGINE TEST AS PER AMM 22-10-00-5, BOTH A/P CAN BE ENGAGED, A/C RTN TO SERVICE. MTP FAULT REVIEW FOUND FCC1/FCC2/FCU/TORQUE LIMITER, RESET A/P1 AND A/P2 BOTH FCC'S AND FCU, PERFORMED AFS/LAND ENGINE TEST AS PER AMM 22-10-00-5, BOTH A/P CAN BE ENGAGED, A/C RTN TO SERVICE.

Part: UNKNOWN — WARNING LIGHT (CARGO DOOR) · airframe 25,736 hrs · 12,348 cycles

FWD CARGO DOOR UNLOCK INDICATION NUMEROUS TIMES AFTER TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01, CATEGORY: C EXPIRATION: 13JUL07.

Part: BULKHEAD — CORRODED (BS 808) · airframe 25,075 hrs · 11,999 cycles

FUSE AFT PRESSURE BULKHEAD LOWER RIM FWD SIDE FR 80/82 FROM STR 50L TO STR 51L. CORROSION REPAIRED IAW FEDEX EA6-5310-106280.

Part: BEARING — FROZEN (RUDDER) · airframe 25,075 hrs · 11,999 cycles

A FROZEN BEARING EXIST AT LT NR 3 RUDDER HINGE ARM COMPLIED WITH FEDEX EA6-5540-106279.

Part: HINGE — CORRODED (RT ELEVATOR) · airframe 25,075 hrs · 11,999 cycles

RT ELEVATOR T/E AT AT 4 HINGE ARM HAS LIGHT CORROSION TOP AND BOTTOM AS MARKED REPAIRED CORROSION ON RT, ELEVATOR AT NR 4 HINGE ON CORNER SKIN IAW A310/200 SRM 51-74-10 PARAGRAPH 6A. REPAIRED DAMAGED SKIN ON UPPER SKIN IAW EA6-5520-106303.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 25,075 hrs · 11,999 cycles

DUMMY TRACK FS 54 TO 54.2 LT NR 5 HAS SLOTTED HOLE ATTACHMENT POINT HAS WEAR MEASURING .051 IN. REMOVED AND INSTALLED FLOORBOARD IAW A310/200 AMM 53-10-254. ROUTED TO B/S FOR REPAIR IAW A310/200 SCP53-15-16. INSTALLED DUMMY TRACK IAW A310/200 SRM 53-15-18.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 25,075 hrs · 11,999 cycles

MDCC SEAT TRACK R1 AT FR 38.1 HAS (1) BROKEN SCALLOP AND (1) BENT SCALLOP. REMOVED AND INSTALLED REPAIR SEAT TRACK IAW A310-200 SRM 53-10-16 PB 201 FIG 208.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 25,075 hrs · 11,999 cycles

RT WING, INBD FLAP, LWR EXT SKIN AT MID T/E, (1)EA AREA OF DELAMINATION APPROX 6" * 6" DIA. REPAIRED (1EA) AREA OF DELAMINATION ON RT WING I/B FLAP LOWER SKIN IAW A310-200 SRM 57-52-12 FIG 204. THE REPAIR IS FOUND TO BE MAJOR IAW FED EX GMM 6-2-100.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 25,075 hrs · 11,999 cycles

PREVIOUS REPAIR, FUSELAGE SKIN RT SIDE HAS EXTERNAL REPAIR DOUBLE BETWEEN FR 54.1 TO 54.2, BETWEEN STR 38 RT TO STR 40 RT, MEASURES 6.3" BY 6.2" PREVIOUSLY INSTALLED REPAIR LOCATED AT RT SIDE FUSELAGE SKIN BETWEEN FRAMES 54.1- 54.2 STRINGERS 38 TO 40 RT DETERMINED NOT TO BE IAW FEDEX EA 6-5330-41795 DUE TO INCORRECT MATERIAL THICKNESS OF REPAIR DOUBLER, BASED ON VISUAL EVALUATION WITH THE REPAIR INSTALLED, VISUAL EVAL CONSIST OF CORRECT LOCATION, SHAPE, SIZE, FASTENER SPACING, AND EDGE MARGIN, FASTENER TYPE AND NUMBER, MAT THICKNESS, MAT TYPE AND GENERAL WORKMANSHIP OF PREVIOUS INSTALLATION. REMOVED EXISTING REPAIR AND REPAIRED FUSELAGE SKIN PER FED EX EA 6-5330-106290. MAJOR REPAIR IAW FED EX GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RUDDER) · airframe 25,075 hrs · 11,999 cycles

CORROSION EXIST AT VERT STAB REAR SPAR NR 3 RUDDER ATTACHMENT HINGE FITTING COMPLIED WITH EA NR 6-5540-106300. RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR REPAIR IAW FED EX GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RUDDER) · airframe 25,075 hrs · 11,999 cycles

VERT STAB REAR SPAR NR 2 RUDDER ATTACHMENT HINGE FITTING HAS CORROSION. COMPLIED WITH EA NR 6-5540-106300 RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR REPAIR IAW FED EX GMM 6-2-100.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 25,075 hrs · 11,999 cycles

MDCC SEAT TRACK L4 FR 54.2 - 58 GOUGED REMOVED AND REINSTALLED 4EA FLOORBOARDS IAW A310-200 SRM 53-10-25-4. REMOVED AND INSTALLED NEW SEAT TRACK IAW A310-200 DWG 16R532H1414. FABBED NEW SEATRACK PER A310-200 DWG 16R532H1414. REMOVED AND REINSTALLED 4 EA SEATRACK SPLICES IAW A310-200 SRM 51-72-10. SEALED FLOORBOARDS IAW A310-200 SRM 53-10-25-4. MAJOR REPAIR IAW FED EX GMM 6-2-100.

Part: REGULATOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 24,358 hrs · 11,687 cycles

ENGINE NR 1 REV UNLK ILLUMINATED ON TAKEOFF ROLL, REJECTED TAKEOFF, WHEN THROTTLES PULLED TO IDLE REV UNLK LIGHT ENGINE NR 1 EXTINGUISHED. REJECTED TAKEOFF AT APPROX 6O KTS. REMOVED AND REPLACED NR 1 ENGINE PRESSURE REGULATING AND SHUTOFF VALVE AS PER AMM 78-31-05-4-03. OPS TEST OK, 78-13-11 P BLOCK 501. MOVED A/C TO TAXIWAY PERFORMED HIGH POWER RAN PER JRH. NO REV UNLOCK ILLUMINATION OCCUR. A/C OK. PREMATURE REMOVAL/INSTALLATION OFF MFG 3214236-8, POS 1, SRL P-236C, TAG 0519A3, ON MFG 3214236-8, SRL 369C TAG 6A9488.

Part: SWITCH — FAULTY (THRUST REVERSER) · airframe 24,358 hrs · 11,687 cycles

ENGINE NR 1 REV UNLK ILLUMINATED ON TAKEOFF ROLL. REJECTED TAKEOFF APPROX 40 KTS REV UNLK LIGHT EXTINGUISHED WHEN THROTTLES PULLED TO IDLE. REMOVED AND REPLACED NR 1 ENGINE STOW SWITCH S303 AND PERFORMED RIGGING PER A310 AMM 78-31-00-5. OPS CHK COMPLETED. ALL INDICATION NORMAL.

Part: REGULATOR — MALFUNCTIONED (ENG OIL PRESS) · airframe 23,561 hrs · 11,329 cycles

NR 2 ENGINE INDICATED HIGH OIL PRESSURE, THEN FOLLOWED QRH & MONITORED PARAMETERS. OIL PRESS. WENT TO 20-32 PSI (LOW) FOLLOWED QRH AND SHUTDOWN ENGINE. DECLARED EMERGENCY AND LANDED RWY 32L. HIGH OIL PRESS. WAS 100, LOW OIL PRESS. WAS 22. PRESSURE VARIED ACCORDING TO THROTTLE POSITION. ALL OTHER ENGINE PARAMETERS WERE NORMAL EXCEPT RT OIL TEMP AT 130 DEG LEFT ENGINE OIL TEMP 120 DEG. REPLACED THE OIL PRESSURE REGULATOR AND OIL PRESSURE TRANSMITTER

Part: SKIN — DAMAGED (TE FLAP) · airframe 22,634 hrs · 10,773 cycles

NON-ROUTINE NR N00380. RT WING REPAIR ON INBD FLAP LWR SURFACE T/E. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-63790.

Part: SKIN — CORRODED (RT WING) · airframe 22,634 hrs · 10,773 cycles

RT WING CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,634 hrs · 10,773 cycles

FUSELAGE REPAIR AT APROX. FS 1 STR 56 LT. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5310-81826.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,634 hrs · 10,773 cycles

COMPLY WITH AGING 9-AGING-INSPECTION. NON-ROUTINE, FUSELAGE - REPAIR AT APPROX FS 69 STR 50 RT. *S/D* VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 225.

Part: RIB — CORRODED (LT WING) · airframe 22,634 hrs · 10,773 cycles

ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, LT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FEDEX EA 6-5710-81827. PERFORMED NDT INSPECTION 51-10-08 PT6. PAINTED IAW SRM 51-75-10-8.

Part: SKIN — CORRODED (LT WING) · airframe 22,634 hrs · 10,773 cycles

ACCOMPLISH MAINTENANCE C-CHECK, ORIGINAL PLAN DATE WAS ENTERED ON: 23JUL04. NON-ROUTINE LT WING - CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FEDEX EA 6-5710-81827. NDT INSP IAW 51-10-08 PT6. PAINTED IAW SRM 51-75-10-8.

Part: SKIN — DENTED (RT WING) · airframe 22,634 hrs · 10,773 cycles

ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, RT WING - DENTS AND DEBONDS AT LOWER SKIN SURFACE OF T/E OF FLAP INBOARD. REPAIRED IAW AIRBUS REF: 001-57-01-2005-A1B AND IAW EA 6-5750-81828. PAINTED IAW SRM 51-75-10-8.

Part: FAIRING — CRACKED (NR 2 PYLON) · airframe 22,634 hrs · 10,773 cycles

NR 2 PYLON, AFTER FIXED FAIRING WITH CRACK AT LT. REMOVED IAW AMM 54-55-00. REPAIRED IAW FEDEX EA 6-5480-81822. INSTALED IAW AMM 54-55-00.

Part: SKIN — CORRODED (RT WING) · airframe 22,634 hrs · 10,773 cycles

RT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,634 hrs · 10,773 cycles

FUSELAGE - REPAIR AT APROX. FS 63 STR 42 RT. REPAIRED IAW SRM 53-17-12, FIG 203.

Part: ENGINE — FAILED (NR 2) · airframe 22,024 hrs · 10,453 cycles

UNRECOVERABLE STALL ENG NR 2 DURING T/O AT 500 FT ATB. EGT WAS RAISING TO 670 DEG C, EGT LIGHT ON, PULLED BACK THE THROTTLE TO PREVENT FURTHER EGT INCREASE. FLAME NOTED BY ATC. AS PER MTSI 72-00/3790 REMOVED AND REPLACED NR 2 ENG VANE AND BLEED CONTROL PER MM 75-31-04-4A, FOR LEAK CHECK AND ENG TRIM RUN. PREMATURE REMOVAL/INSTALLATION OFF MFG 776555-7, ON MFG 776555-5.

Part: CONNECTOR — DAMAGED (DOOR WARNING) · airframe 21,603 hrs · 10,280 cycles

ON CLIMBOUT (APPROX 10,000 FT) ECAM WARNING OF FWD CARGO DOOR NOT CLOSED, RT ECAM DOOR PAGE ALL GREEN, PRESSURIZATION NORMAL. MEL 17MAR04 02:33 RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 27MAR04. MEL 52-71-01: (IDENTIFY) LWR FWD CARGO DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE INOP, LOWER FWD CARGO DOOR VISUALLY CHECKED CLOSED & LOCKED. FOUND LOT OF WATER IN C/P 14WS AND 16WS. FOUND PIN-A CRACKED JONC/P 14WS. REMOVED AND REPLACED 14WS PER MM 52-71-11. FWD CARGO INDICATION CHECKED NORMAL.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 17,947 hrs · 8,349 cycles

A/C ENCOUNTERED MODERATE TURBULENCE, CIRRUS CLOUDS AND STATIC ELECTRICITY. NR 1 ENG ROLLED BACK TO IDLE/OFF. EGT CLIMB TO GREATER THAN 600 DEG.

Part: ENGINE — MALFUNCTIONED (RT & LT)

ON T/O ROLL, THROTTLES ADV, EPR & N1 REACH TOGA THRUST, HAD LOUD BOOM FOLLOWED BY SLIGHT YAW 10 DEG TO RT. SUSPECT SIDE WIND. BOTH ENG RUN AT T/O PWR FOUND NORM. VISUALLY CHECK ENG TURBINES AND FANS, OK.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 16,541 hrs · 7,631 cycles

MANHOLE DOUBLER CORROSION FR 38 & 39 AT STR 50 RT. REPAIRED PER SRM 53-14-12 FIG 203, & 53-14-12 FIG 20.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,451 hrs · 7,631 cycles

FR 42-43, STR 10-11 LT KNIFE EDGE CONDITION IN THE SKIN PANEL. REMOVED AND REPLACED DOUBLER A538-70089-204 PER BEA 1402 6110, SH1.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 16,541 hrs · 7,631 cycles

FR 65, STR 28-29 RT SCRATCH IN OUTER SKIN. REMOVED AND REPLACED PER IAW DWT 14025J39.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,541 hrs · 7,631 cycles

FR 54.1 - 54.2, STR 39-41 RT EXTERNAL FUSELAGE SKIN. REMOVED AND REPLACED PER IAW DWG 16R539H0111.