Airbus A310

Service difficulty reports · 606

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A310'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 06FDEA0533Repair · misinstalledFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 347-349. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALUAFeb 3, 2006 · N430FE · Airbus A310 · Trailing Edge FlapsSDR 06FDEA0532Repair · misinstalledFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 110-119. REPAIR REQUIRES EVALUATION FOR MAJOR OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALUFeb 3, 2006 · N430FE · Airbus A310 · Trailing Edge FlapsSDR 06FDEA0531Repair · unknownFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 359-409. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 AND RAS/DABRE/700Feb 3, 2006 · N430FE · Airbus A310 · Wing StructureSDR 06FDEA0529Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 134-182. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATFeb 3, 2006 · N430FE · Airbus A310 · Aircraft StructuresSDR 06FDEA0528Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 346-400. REPAIR REQUIRES EVALUATION FOR MAJOR OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATFeb 3, 2006 · N430FE · Airbus A310 · Trailing Edge FlapsSDR 06FDEA0527Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 236-276. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATED Feb 3, 2006 · N430FE · Airbus A310 · Trailing Edge FlapsSDR 06FDEA0526Repair · misinstalledFOUND REPAIR LOCATED ON L/H INBD FLAP, LT WS128-WS176. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALFeb 3, 2006 · N430FE · Airbus A310 · Aircraft StructuresSDR 06FDEA0515Actuator · malfunctionedON TAKEOFF, UPON HITTING TOGA SWITCHES BOTH ATS LEVERS TRIPPED OFF. IMMEDIATELY RESET 1 AND 2 ATS LEVERS, COULD NOT DEVELOP TOGA N1, BOTH ENGINES STOPED AT 90 PERCENT N1. REJECTED AT 60 KNOTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-B "MEL 22-30-01Feb 2, 2006 · N414FE · Airbus A310 · Auto Throttle SystemSDR 06FDEA0438Skin · crackedLOWER SURFACE OF LT WING TE AT THE I/B MOST OF OUTBD FLAP THERE IS A CRACK EMMINATING REPAIRED IAW AIRBUS REPAIR DRAWING R572.Jan 30, 2006 · N456FE · Airbus A310 · Wing, Plate/SkinSDR 06FDEA0372Converter · no testREMOVED AND REPLACED SDAC IAW AMM 31-55-22-4. OPERATIONAL TEST FOUND SATISFACTORY. A/C OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION.Jan 24, 2006 · N802FD · Airbus A310 · DC Rectifier/ConverterSDR 06FDEA0365Bearing · unknownCOMPLY WITH EA 6-5720-92381 INSPECTION/CHECK OF PYLON AFT ATTACH FITTING UPPER BEARINGS ENT BY: 501863 RPT BY: 501863 FACT 20JAN06 07:25 BFM R COMPLIED WITH EA 6-5720-92381 INSPECTION CHECK OF PYLON AFT ATTACH FITTING UPPER BEARINGS RII:573074 ENT BY: 57Jan 24, 2006 · N456FE · Airbus A310 · Nacelle/Pylon Miscellaneous StructureSDR 06FDEA0360Regulator · out of adjustRTO DUE TO AMBER OIL PRESSURE HIGH LIGHT ON NR 1 ENG. SWAPED NR 1 AND 2 OIL SIGNAL COND. R & R NR 1 OIL PRESS SIGNAL CONDITIONER IAW MM 79-33-31 , RAN ENG - NO HELP OIL PRESS AT IDLE STILL 54 PSI. REINSTALLED ORIGIONAL. R & R NR 1 OIL PRESS TRANSMITTER IJan 24, 2006 · N455FE · Airbus A310 · Engine Oil QuantitySDR 06FDEA0332Repair · misinstalledFOUND 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 FJan 23, 2006 · N442FE · Airbus A310 · Wing StructureSDR 06FDEA0331Repair · unknownFOUND 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 SJan 23, 2006 · N442FE · Airbus A310 · Wing StructureSDR 06FDEA0329Repair · misinstalledFOUND 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-Jan 23, 2006 · N442FE · Airbus A310 · Elevator StructureSDR 06FDEA0328Repair · misinstalledFOUND 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-Jan 23, 2006 · N442FE · Airbus A310 · Elevator StructureSDR 06FDEA0327Repair · misinstalledFOUND 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-Jan 23, 2006 · N442FE · Airbus A310 · Elevator StructureSDR 06FDEA0325Repair · misinstalledFOUND 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 Jan 23, 2006 · N442FE · Airbus A310 · Horizontal Stabilizer StructureSDR 06FDEA0324Repair · misinstalledFOUND 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-Jan 23, 2006 · N442FE · Airbus A310 · Horizontal Stabilizer StructureSDR 06FDEA0239Repair · damagedSMIS 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 EJan 17, 2006 · N442FE · Airbus A310 · Aircraft StructuresSDR 06FDEA0238Repair · correctSMIS 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 DOJan 17, 2006 · N442FE · Airbus A310 · Aircraft StructuresSDR 06FDEA0240Structure · contaminatedPILOT REPORT ACFT WILL TAKE AN ATTITUDE OF 3 DEGREES NOSE UP AT ALL PHASES OF FLIGHT ANY TIME. THE AUTO PILOT IS DISCONECTED. OPEN T.H.S ACCESS PANEL AND NOTICED ACCUMULATION OF WATER ABOUT 14 INCHES HIGH RIGHT BEHIND PRESSURE BULKHEAD. UNPLUGED DRAIN IN Jan 17, 2006 · N804FD · Airbus A310 · Aircraft StructuresSDR 06FDEA0237Placard · correctA/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.Jan 17, 2006 · N442FE · Airbus A310 · Placards and MarkingsSDR 05FDEA04219Skin · crackedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPADec 10, 2005 · N424FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA04218Track · crackedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCDec 10, 2005 · N424FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 05FDEA04217Structure · corrodedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCYDec 10, 2005 · N424FE · Airbus A310 · Passenger/Crew DoorsSDR 05FDEA04216Skin · debondedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCDec 10, 2005 · N424FE · Airbus A310 · Elevator, Plate/SkinSDR 05FDEA04214Skin · debondedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCDec 10, 2005 · N424FE · Airbus A310 · Elevator, Plate/SkinSDR 05FDEA04178Spar · corrodedLT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00541. REPAIRED LT UPPER IB THS SPAR CORD IAW A310-200 SRM 55-11-21 PARA 7.H PAGES 315TO, 320 FIG 211,213 AND 219 SHEET 2.Dec 8, 2005 · N423FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 05FDEA04171Doubler · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LT EXT DOUBLER ABOVE AND AFT OF CAPT,S SIDE WINDOW, STA. 881 TO 904 FR 7 TO FR 8 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00696 REPAIR GOOD IAW EA 6-5330-95466.Dec 7, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04170Skin · corrodedBELLY OF AC RT SIDE FWD OF NR 2 PACK PORTABLE WATER SERVICE HAS CORROSION ON CUTOUT REF N00031. REPAIRED DAMAGE IAW EA 6-5330-94498 AND SRM 51-72-10 AND SRM 53-10-14.Dec 7, 2005 · N423FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA04169Repair · nonePREVIOUSLY REPAIR INSTALLED ON L/W NR 1 SLAT IB LEADING EDGE, SKIN BLIND FASTENER FLUSH. REPAIR WS RIB 2 TO RIB 3, NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00708. REPAIR EVALUATED AS GOOD IAW EA 6-5750-95471.Dec 7, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04168Panel · corrodedNOSE GEAR WELL, FWD WALL HAS 13 SPOTS OF LIGHT CORRODED AND SEVERAL SMALL SPOTS OF BARE METAL. REF N00747, REPAIRED NOSE LANDING GEAR BAY FORWARD PANEL BY REPLACING IAW REPAIR INSTRUCTION R53611077 AND NLG BAY PANEL REPLACEMENT, DWG R53610532. (K)Dec 7, 2005 · N423FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 05FDEA04167Fastener · incorrectPREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00705. EVALUATION OF REPAIR REVEALED INCORRECT FASTENERS INSTALLED REPLACED REPADec 7, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04166Spar · corrodedRT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00542. REPAIRED RT HORIZONTAL T/E UPPER SPAR CORD IAW SRM 55-11-21 PARA 7.H PAGES 315 TO 324 FIG SHEET 2 AND FIG 213.Dec 7, 2005 · N423FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 05FDEA04146Fastener · incorrectPREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA, REF N00705. REPAIR REVEALED INCORRECT FASTENER INSTALLED REMOVED AND REPLACED REPAIR IAWDec 5, 2005 · N423FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04103Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 115 TO WS 200. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPRDec 3, 2005 · N424FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA04102Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 60 TO WS 110. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPRODec 3, 2005 · N424FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA04101Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 40 TO WS 50. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPRDec 3, 2005 · N424FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA04100Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 67 TO WS 207. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVEDec 3, 2005 · N424FE · Airbus A310 · Leading Edge DevicesSDR 05FDEA04099Repair · nonePREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (METAL CENTER SECTION), AT WS 192 TO WS 222. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVDec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04097Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE, BELOW REGISTRATION NR N424FE AT STA 4181 TO STA 4241, FR77 TO FR78, STR 23 LT TO STR 24 LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICADec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04098Repair · unknownPREVIOUS REPAIR INSTALLED AT FUSELAGE RT SIDE OF TAIL CONE AT STA 5094 TO STA 5122, FR101 TO FR102, STR 07RH TO STR 08RH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIRDec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04096Repair · unknownPREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE, L2 REAR DOOR FRAME AT STA 4669, FR75A, STR 20LH TO STR 24LH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA.Dec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04094Repair · noneSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY Dec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04093Repair · unknownSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DIDec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04092Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE AT STA 1923, FR35, STR 22LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR CONFORMS TO AN EXISTING FEDEX EDec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04091Repair · mismanufacturedPREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE BELOW AOA SENSOR AT STA 1364 TO STA 1386, FR18 TO FR19, STR 39LT TO 44LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR Dec 3, 2005 · N424FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA04088Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT SIDE, BELOW R1 DOOR AT STA 1187 TO STA 1212, FS 14A TO FS 15. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR Dec 3, 2005 · N424FE · Airbus A310 · Aircraft StructuresSDR 05FDEA04087Repair · mismanufactured2PREVIOUS REPAIR INSTALLED AT LOWER FUSELAGE 6 O'CLOCK POSITION AT STA 771 TO STA 805, FR1 TO FR2. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUDec 3, 2005 · N424FE · Airbus A310 · Fuselage Main, Plate/Skin
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