N442FE

Part: CONVERTER — FAILED (DATA ANALOG) · airframe 44,779 hrs · 19,642 cycles

SDAC FAILURE, BOTH ECAMS, CFM 8-3-1-13. CAPT ECAM SAID "SYSTEM DATA NOT AVAIL" FO ECAM SAID "NO DISCRETE AVAIL". REMOVED AND REPLACED SYSTEM DATA ANALOG CONVERTER PER M/M 31-55-22-4. CHECKS GOOD AT THIS TIME. R&I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 66501-005-1.

Part: REPAIR — NONE (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

THERE WAS NO DOCUMENTED RECORD OF APPROVED DATA FOUND. IN ADDITION ,THERE WAS NO RECORD THAT THE REPAIR HAS BEEN EMBODIED ON THE AIRCRAFT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED TO CONFORM AS PER SRM 53-17-18 FIGURE 204 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (HORIZONTAL STAB) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT HS683-696. 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 SRM 55-12-12 FIGURE 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT HS683-696. 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 SRM 55-12-12 FIGURE 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

THERE IS NO DOCUMENT RECORD THAT THIS REPAIR HAS BEEN EMBODIED ON THE AIRPLANE. REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR IN ACCORDANCE BY REF:RAS DA/HAM -1357-96. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (LT WING) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT WS222-232. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS REMOVED FOUND SMALL DENT PERFORMED NDT INSPECTION , NO CRACKS FOUND DENT WAS FILLED AS PER SRM 51-73-10 AND RIVETS INSTALLED PER SRM 51-40-21 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LEFT HS683-696. 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 SRM 55-12-12 FIGURE 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (LT ELEVATOR) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT ES327-336. 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 PERFORMED IAW SRM 55-21-11 FIG 1 PAGE 212. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (HORIZONTAL STAB) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED AT LT HS 330-350 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 SRM 55-12-12 FIG 203 AND SRM 51-73-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED AT LEFT HS330-350 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 SRM 55-12-12 FIG 203 AND SRM 51-73-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

THERE IS NO DOCUMENT RECORD THAT THIS REPAIR HAS BEEN EMBODIED ON THE AIRPLANE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM REF:RAS DA/ BRE503/92 AND DRAWING KLM2H-17390. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

THERE IS NO DOCUMENT RECORD THAT THIS REPAIR HAS BEEN EMBODIED ON THE AIRPLANE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM REF:RAS DA/ BRE503/92 AND DRAWING KLM2H-17390. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (LT ELEVATOR) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT ES327-336. 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 PERFORMED IAW SRM 55-21-11 FIG 1 PAGE 212. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT HS683-696. 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 SRM 55-12-12 FIGURE 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (LT WING) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT WS270-280. 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 EXISTING REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-42-11 FIG 202 SHEET 4 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — MISINSTALLED (LT ELEVATOR) · airframe 43,849 hrs · 19,161 cycles

FOUND REPAIR LOCATED LT ES327-336. 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 PERFORMED IAW SRM 55-21-11 FIG 1 PAGE 212. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (T/E FLAP) · airframe 43,840 hrs · 19,159 cycles

FOUND REPAIR LOCATED RT WS 1574-1604. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPAIR RT FLAP OUTBOARD REPAIRED PER SRM 57-53-12. REPAIR EVALUATED PER GMM 6-2-100 CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (T/E FLAP) · airframe 43,840 hrs · 19,159 cycles

FOUND REPAIR LOCATED RT WS 1372-1372. 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 EXISTING SRM REPAIR RIGHT WING OUTBOARD FLAP LOWER T/E WAS REPAIRED PER SRM 57-53-12. REPAIR EVALUATED PER GMM 6-2-100 CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 43,840 hrs · 19,159 cycles

AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0329): FOUND REPAIR LOCATED LT; FS 3514 AND FS 3567, FR 65 AND FR 66 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 EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 53-10-21. REPAIR EVALUATED PER GMM 6-2-100 CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 43,840 hrs · 19,159 cycles

FOUND REPAIR LOCATED LT FS 4100 AND FS 4120 , FR 76. 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 EXISTING SRM REPAIR. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5330-94671. REPAIR EVALUATED PER GMM 6-2-100 CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 43,840 hrs · 19,159 cycles

FOUND REPAIR LOCATED RT WS 339-339. 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 EXISTING SRM REPAIR RIGHT WING INBOARD FLAP REPAIRED PER EA FEDEX 6-5710-94674. REPAIR EVALUATED PER GMM 6-2-100 CLASSIFIED AS MINOR.

Part: PLACARD — CORRECT (DATA PLATE) · airframe 43,840 hrs · 19,159 cycles

A/C DATA PLATE SHOWS DATE OF MFG AS 9 JAN 1985. RECORDS SHOW DATE F MFG AS 26 OCT 1984 THERE APPEARS TO BE A CONFLICT. VERIFIED AIRCRAFT DATAPLATE DAY OF MFG TO BE 9 JAN 1985. AIRCRAFT RECORDS NOTIFIED.

Part: REPAIR — CORRECT (FUSELAGE) · airframe 43,840 hrs · 19,159 cycles

SMIS 442 51-00 0007189 03NOV05 MC1 OPEN R WS-C 00031301 MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0324 FOUND REPAIR LOCATED LT FS1067AND FS1091 FR 12 AND FR12A EXT DOUBLER REPAIR HAS EA 6-5310-54506 CLASSIFIED MINOR BY ENGINEERING . THIS REPAIRS REQUIRES RE-EVALUATION BY OPERATOR TO DETERMINE MAJOR OR MINOR DUE TO THE SIZE AND LOCATION OF THE REPAIR. REPAIR EVALUATED AND CONFORMS TO EXISTING EA 6-5310-54506 REPAIR EVALUATED IAW GMM 6-2-100.

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 43,840 hrs · 19,159 cycles

SMIS 442 51-00 0007189 03NOV05 MC1 OPEN R WS-C 00031301 MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0328): FOUND REPAIR LOCATED RT FS 1605-1658 FR23-24. REPAIRS REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APROVED DATA. PREVIOUS REPAIR REPLACED IAW SRM 51-40-21 AND 51-40-44 AND 51-72-10. REPAIR EVALUATED IAW GMM 6-2-100 CLASSIFIED AS MAJOR.

Part: SEQUENCE VALVE — MALFUNCTIONED (MLG) · airframe 42,495 hrs · 18,382 cycles

ON INITIAL TAKEOFF RETRACTED GEAR AND LT MLG REMAINED DOWN AND LOCKED WITH RED UNLOCK LIGHT ILLUMINATED ON BOTH LANDING GEAR PANELS. PLACED GEAR HANDLE DOWN AND GOT 3 GREEN NO RED LANDED UNEVENTFUL SYSTEM 1 SELECTED. PER FLIGHT CREW DEBRIEF, THE DOOR OPEN LIGHT WAS NOT ILLUMINATED AT ANY POINT DURING THE ATTEMPTED GEAR RETRACTION OR THE SUBSEQUENT GEAR EXTENSION. PERFORMED MEMORY RECALL TEST ON PROXIMITY DETECTOR UNIT WITH NO FAULTS RECORDED. ALSO PERFORMED SYSTEM TEST ON SAME UNIT WITH RESULTS COMING BACK NORMAL. TROUBLESHOOTING TO CONTINUE. PERFORMED GENERAL ADJ/TEST PER A310-200 COMPLETED MAIN GEAR SEQUENCE VALVE PER A310-200 MM 32-31-37-4. PERFORMED GEAR SWING INDICATIONS NORMAL.

Part: CONNECTOR — CORRODED (MLG UPLOCK) · airframe 42,495 hrs · 18,381 cycles

NR 1 MLG DOOR WOULD NOT CLOSE ON GEAR RETRACTION. PUT GEAR DOWN IAW ECAM, RETURNED FOR LANDING. PERFORMED BITE CHECK OF PROX DET UNIT REF A310 M/M 32-31-71-4, RECEIVED BOX FAULT CODE (BOX LIGHT ON) CODE 64= 28VDC POWER SUPPLY NR 4 OR NR 3,SEE A310 TSM 32-61-00 FAULT ISOLATION PAGE 104.A310 TSM 32-61-00 PAGE 117 SUGGESTS TO CHECK C/B 1GB. FOUND SYS 1 MLG DOOR UPLOCK CONNECTOR CORRODED, REPLACED CONNECTOR AND REPINNED REMOVED AND REPLACED LT MLG UPLOCK ASSY OPS CHECK NORMAL. REMOVED AND REPLACED MLG DOOR ACTUATOR, WITH SERVICEABLE ACTUATOR, OPS CHECK NORMAL IAW MM 32-31-00 P. BLOCK 501. JACKED AC IAE MM 07-11-00-0 THRU STEP C 4. SWUNG GEAR SUCCESSFULLY, NO DEFECTS NOTED.

Part: ANGLE — MISMANUFACTURED (ZONE 100) · airframe 41,624 hrs · 17,866 cycles

RIGHT WING FRAME NR 40 HAS NUMEROUS HOLES DRILLED THRU FUSELAGE SKIN ONLY. THAT IS OUT OF ROUND/ELONGATED. ACCOMPLISHED WORK CARD EA6-5310-7-5003 02 PT4 AND EA6-5310-73419A AT CWF BY DRILLING FASTENER HOLES TO CORRECT SIZE AND INSTALLING PICKUP ANGLE TO ENGINEERS FASTENER INSTALLATION SHEET.

Part: SKIN — CRACKED (ZONE 500) · airframe 41,624 hrs · 17,866 cycles

MEM MX REPORTS A .8 CRACK IN THE LT LOWER WING SKIN AT RIB 11. COMPLIED WITH WORK CARD T6-5710-66977 WRI 57105494 AT CWF BY INSTALLING NEW DOUBLER PER EA6-5710-66977 PT3 AND AIRBUS DRAWING R57249152 AND EA6-5710-73414A AND NRC S00002.

Part: SKIN — CRACKED (ZONE 600) · airframe 41,624 hrs · 17,866 cycles

MEM MX REPORTS A 1.9 INCH CRACK IN THE RT LOWER WING SKIN AT RIB 11. ACCOMPLISHED WORK CARD T6-5610-66979 A PT3 AT CWF BY INSTALLING DOUBLER AT RIB 11 PER EA 6-571066979 PT 3 AND EA6-5710-73414A AND NRC S00025.

Part: ANGLE — MISREPAIRED (ZONE 100) · airframe 41,624 hrs · 17,866 cycles

LEFT WING RIB NR 40 HAS 24 EA EXISTING HOLES THAT IS ( 2-AND) OVERSIZE IN FRAME 40. PICKUP ANGLE C/T FUEL TANK EO6-5310-7-5003 WORK INSTRUCTION - DRILL HOLES TO THE (1ST) OVERSIZE. COMPLIED WITH WORK CARD (EA6-5310-7-5003 02 PT3) , EA6-5310-73418, EA6-5310-73418A, EA6-5310-73418B AND NRC (SOOO24) AT CWF. BY DRILLING ALL FASTENER HOLES AND PICKUP ANGLE TO CORRECT SIZE AND INSTALLING ON A/C, AND INSTALLING ALL NEW FASTENERS IAW ENGINEER FASTENER CALLOUT SHEET REVISION (C).

Part: SEQUENCE VALVE — MALFUNCTIONED (RT MLG) · airframe 39,977 hrs · 17,023 cycles

AFTER T/O FROM LGB THE GEAR WAS RAISED AND WAS CONFIRMED UP AND LOCKED UNTIL SLATS WERE RETRACTED AT WHICH TIME A THUMP AND SLIGHT SHUDDER WAS FELT AND L MAIN GEAR INDICATED UNSAFE. GEAR HANDLE WAS PLACED IN THE DOWN POSITION WITH ALL GEAR INDICATING DOWN AND LOCKED. UNABLE TO DUPLICATED, SUSPECTED BAD UPLOCK ACTUATOR. WHEN PERFORMING GEAR SWING PER M/M 32-31-00-516, PUT GEAR HANDLE IN NEUTRAL POSITION W/GEAR UP, AND HYD MULE PRESS WAS ABLE TO DUPLICATE PROBLEM ON ANOTHER A310 W/SAME PROBLEM. IT WAS T/S TO OPPOSITE SIDE MLG SEQ VALVE.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 39,730 hrs · 16,899 cycles

DURING CLIMB NR 1 ENGINE FLUCTUATED. REMOVED AND REPLACED NR 1 CIT SENSOR & T2 SENSOR PER 73-21-02-4, 73-23-07-4. ALL OK.

Part: WINDSHIELD — CRACKED · airframe 39,386 hrs · 16,695 cycles

1-381 CAPT'S WINDSHIELD CRACKED OUTER LAYER. REPLACD WINDSHIELD, CONTROLLER & REGULATOR.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 38,752 hrs · 16,302 cycles

TRANSVERSE LOAD FITTING HAS INTERGRANULAR CORROSION, TOP LT AND RT ATTACH POINT TO FWD VERTICAL STAB FRONT SPAR.

Part: COMPUTER — FAILED (COCKPIT FLT DIR) · airframe 38,446 hrs · 16,157 cycles

00-335 BOTH FLIGHT DIRECTORS FAILED.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 38,446 hrs · 16,167 cycles

00-334 NR 1 ENGINE ROLLED BACK WITH A ENG TRIM FAULT LIGHT ON.

Part: CONTROLLER — FAILED (SLATS)

STUCK SLATS AFT TO SLATS REMAIN AT 15'' BOTH SYS 1 AND 2 FAULT LIGHTS AND SLATS LIGHTS ON SPFC ON. REMOVED AND REPLACED NR 1 SFCC PER MM 27-5-18-4. PERF BITE TEST AND OPS CK OF FLAPS AND SLATS, NO FAULTS NOTED. AC OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 37,805 hrs · 15,852 cycles

DURING CLIMB, NR 2 ENGINE REDUCED TO IDLE WOULD NOT RESPOND TO THROTTLE MOVEMENT.