N413FE

Part: SKIN — MISREPAIRED (NR 2 SLAT) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS FLUSH REPAIR FOUND LOCATED ON LEADING EDGE OF NR 2 SLAT BETWEEN SLAT TRACKS 6-7, WS 1057 AND RIB 17. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND NEW REPAIR PER SRM 57-43-11 FIG 202 SHEET 12. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: STRUCTURE — MISREPAIRED · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE LT CROSSBEAM FS 2082, FR 38 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND NEW REPAIR PER FEDEX EA 6-5310-105652. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (LT WING) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE OUTBD OF NR 7 SPOILER, WS 1604 AND RIB 26. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR, NEW REPAIR ACCOMPLISHED IAW FEDEX ENGINEERING AUTHORIZATION 6-5730-105650 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: CROSSBEAM — MISREPAIRED (FUSLEAGE) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT CROSSBEAM FS 1870, FS 34 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND REPAIRED PER SRM 53-10-15 FIG 201 (SHEET 2). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: CROSSBEAM — MISREPAIRED (FUSELAGE) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT CROSSBEAM FS 3143, FR 55/58 AND Y120- Y197. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX EA 6-5310-105658. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 31,911 hrs · 22,168 cycles

DURING ACCESS OPENING ON MAIN CARGO DECK CROSSBEAM FS 44,Y1456/Y1956, P/N R538D1048-200-00, WAS FOUND CRACK AND NEED TO BE REPLACED TRACK REPLACED PER SRM 51-40-00. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON AFT CARGO DOOR SKIN FWD LWR SIDE, FS 3249, AND FR 60. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO AN EXISTING SRM REPAIR. ACCOMPLISHED PER FEDEX EA 6-5230-105654 PART 2. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (LT ELEVATOR) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE LT ELEVATOR UPPER SURFACE L/E OUTBD OF NR 7 HINGE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND NEW REPAIRED PER SRM 55-24-11. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: CROSSBEAM — MISREPAIRED (BS 1976) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT CROSSBEAM FS 1976, FR 36 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND NEW REPAIR PER SRM 53-10-15 FIG 201 SHEET 2. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 31,911 hrs · 22,168 cycles

DURING ACCESS OPENING ON MAIN CARGO DECK CROSS TRACK FR 50,-Y450/-Y953, P/N A53812934-200-00, WAS FOUND CRACKED AND NEEDED TO BE REPLACED. TRACK REPLACED PER SRM 51-40-00.

Part: SKIN — MISREPAIRED (LT WING) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT LOWER WING SURFACE CORNER OF ACCESS PANEL 581 AB, WS 663 AND RIB 11. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX EA 6-5710-105661. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (FUSLEAGE) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE LT INBOARD FLAP LOWER SURFACE FWD OF T/E SECTION WS 139 AND RIB 3. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR, NEW REPAIR ACCOMPLISHED PER SRM 57-52-12 FIG 205. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (BS 2135-2188) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED FS 2135-2188, FR 38.1-38.2 EXTERNAL TRIPLER FWD LEFT SIDE OF MANHOLE ACCESS PANEL 136AR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND REPAIRED PER SRM 53-15-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: STRUCTURE — MISREPAIRED (HORIZONTAL STAB) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LT HORIZONTAL STABILIZER L/E EDGE SECTION 341CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR/MAJOR".

Part: STRUCTURE — MISREPAIRED (BS 1870) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT CROSSBEAM FS 1870, FR 34 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND REPAIRED PER SRM 53-10-15 FIG 201 SHEET 2. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF FWD CARGO DOOR SKIN, FS 1605, AND FR 23-23A. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX E.A. 6-5230-105654 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR"

Part: CROSSBEAM — MISREPAIRED (FUSELAGE) · airframe 31,911 hrs · 22,168 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT CROSSBEAM FS 3249, FR 60 AND Y120- Y197. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX EA 6-5310-105658. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,911 hrs · 22,168 cycles

DURING ACCESS OPENING ON MAIN CARGO DECK SOME CROSS TRACKS OF FRAME 43 P/N R538D1048-200-00 WAS FOUND CRACK AND NEED TO BE REPLACED. TRACKS REPLACED PER SRM 51-40-00 ON FR43 Y1456/Y1956. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 30,569 hrs · 21,451 cycles

PASSING 11,000 FT ON CLIMB-OUT, GOT EXCESSIVE CABIN ALTITUDE ECAM WARNING. CABIN ALT WAS 10170. FOLLOWED ECAM AND QRH. NO FAULT LIGHTS COULD GET OUTFLOW VALVES TO CLOSE IN AUTO OR MANUAL. AIR TURN BACK TO KMEM NO DEFECTS NOTED. AS PRECAUTIONARY SUGGEST CHANGING BOTH CABIN PRESSURE CONTROLLERS. REMOVED AND REPLACED NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS IN REFERENCE TO A310-200 M/M 21-31-11-4. TESTED IN REFERENCE TO A310-200 M/M 21-31-00-5-01 NO DEFECTS NOTED.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 30,569 hrs · 21,451 cycles

PASSING 11,000 FT ON CLIMB-OUT, GOT EXCESSIVE CABIN ALTITUDE ECAM WARNING. CABIN ALT WAS 10170. FOLLOWED ECAM AND QRH. NO FAULT LIGHTS COULD GET OUTFLOW VALVES TO CLOSE IN AUTO OR MANUAL. AIR TURN BACK TO KME.

Part: PANEL — DAMAGED (RT WING) · airframe 29,786 hrs · 20,962 cycles

PANEL LAND ON RIGHT WING ACCESS HOLE 650JB HAS 1 EACH ELONGATED HOLE. COMPLIED WITH EA 6-5710-85600 BY INSTALLING REPAIR BUSHING.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 29,786 hrs · 20,962 cycles

PANEL 550JB HAS 2 EACH ELONGATED HOLES. COMLIED WITH EA 6-5710-85600 BY INSTALLING 2 EACH REPAIR BUSHINGS.

Part: PANEL — DAMAGED (LT WING) · airframe 29,786 hrs · 20,962 cycles

PANEL 550GB HAS 1 EACH ELONGATED HOLE ON PANEL LAND, LEFT WING. COMPLIED WITH EA 6-5710-85600 BY INSTALLING REPAIR BUSHING.

Part: SEQUENCE VALVE — MALFUNCTIONED (ZONE 700) · airframe 29,102 hrs · 20,495 cycles

ON DEPARTURE AFTER GEAR RETRACTION THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. AS PER THE QRH, DID NOT RECYCLE BUT PUT THE HANDLE TO OFF. AT THAT POINT, LOTS OF NOISE AND SOME VIBRATION. RETURNED TO KMEM AND THE SPEED NEVER EXCEEDED (270K/M.65). REF THE AIRBUS A310 07-11-00-0, JACKED AIRCRAFT ANY FAULTS NOTED, SIX TIMES IN BOTH SYSTEMS 1 AND 2. REF THE AIRBUS A310 M/M 32-00-00-5, INSTALLED TEST BOX NR 97A32602004201-1 TO AIDE IN THE CYCLING OF THE NOSE GEAR. FURTHER TROUBLESHOOTING REQUIRED. PER MAINTENANCE CONTROL REMOVED AND REPLACED NOSE GEAR DOOR LEFT AND RIGHT SEQUENCE VALVES IAW A310-200MM 32-31-18-4. NOSE GEAR DOOR, RIGG AND OPS CHECK.

Part: ADC — INOPERATIVE (NR 1) · airframe 28,267 hrs · 20,014 cycles

AFTER T/O F/O PFD AIRSPEED WAS SLOW TO RESPOND 80 ON CAPT SIDE 50 ON F/O'S SWITCHED TO ADC NR 1 ON F/O SIDE, AT 1000AGL GOT FLAP HIGH SPEED WARNING OVER- SPEED WARNING, SPEED OF A/C WAS 160 KTS IND. FACT 28MAY03 22:03 MEM R REMOVED AND REPLACED NR 2 ADC PER A310 MM 34-11-34 SYSTEM OPS CHECKS GOOD. 34-10/6446 PURGED SYS AND PUMP DOWN ACCOMPLISHED PREMATURE REMOVAL/INSTALLATION.

Part: LANDING GEAR — MALFUNCTIONED (LANDING GEAR) · airframe 26,350 hrs · 545 cycles

01-342 LANDING GEAR DID NOT LEAVE THE WELLS.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 26,141 hrs · 18,906 cycles

RDU GREEN HYD LOW LEVEL. ACCOMPLISH CKLIST AND DECLARED EMERGENCY.

Part: RELAY — FAILED (NR 2 CABIN PRESS)

NR 2 CABIN PRESS REG FAULT. COULD NOT RESET, CABIN WOULD NOT PRESSURIZE. NOSE RELAY FAILED DURING LAST FLT ON AFS TEST PNL. ATS TRIP OFF. NR 2 CABIN PRESS SYSTEM CHECK OK. REMOVED AND REPLACED PSEU, RELAY 96GB AND 141GB OF FLT/GROUND SYS, OPS OK.

Part: CONTROLLER — FAILED (NR 1)

AT 10,000 FT ON DEPARTURE, CABIN ALTITUDE WARNING APPEARED ON ECAM, NO DOOR OR WINDOWS INDICATED OPEN. CABIN PRESSURE WAS VERIFIED ABOVE 10,000 FT, MANUAL PRESSURIZATION CONTROLLER WOULD NOT CONTROL CABIN ALTITUDE. T/S PER TSM 21-30-00 FOUND NR 1 PRESSURE CONTROLLER BAD. REPLACED THE SAME AND TESTED OK. BOTH CABIN PRESS TESTED SYS 1 AND 2 TESTED OK.

Part: SWITCH — LACK OF LUBE (CARGO DOOR)

CARGO DOOR OPEN WARNING WITH ASSOCIATED ECAM EVERY 5 SECONDS. CLEANED AND LUBED SWITCHES 14 AND 16WS, CKS OK.

Part: HYD TUBE — LEAKING (NR 2 ENGINE)

SIN - ON CLIMBOUT OF WSSS, LOST YELLOW FLUID TO STAND PIPE AND RETURNED TO WSSS. ON NR 2 ENG TUBE ASSY TO PRESSURE SWITCH FOUND LEAKING. REMOVED AND REPLACED SAME, (P/N 224-5-12-507). SERVICED YELLOW HYD SYS, LEAK CHECK BY ENG RUN OK.

Part: SMOKE DET — MALFUNCTIONED (COCKPIT)

SIN - AVIONICS SMOKE WARNING ON FINAL, WITH ECAM WARNING. PILOT CONFIRMED NO SMOKE WITH SNIFFER FAN AND NO WARN ON OVERHEAD. REMOVED AND REPLACED COCKPIT SMOKE DET 13WA AND OPS CHECKS GOOD PER 310 TSM 26-15-00.

Part: O-RING — FAILED (GREEN HYD SYST)

WRI 29-10-287 ON DEPARTURE FROM SJC, GREEN SYSTEM HYDRAULIC QUANTITY WAS LOST. REPLACED O-RING ON GREEN SYSTEM HIGH PRESSURE MANIFOLD, RESERVICED HYD SYS PER MM 12-12-28, OK FOR SERVICE.