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"

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SDR 05FDEA00447Skin · corrodedBULK PIT UNDER FLOOR AREA FS 69 STR 48 LT HAS AN AREA THAT EXTEND 2 INCHES FWD OF FS 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00477Skin · corrodedBULK PIT UNDER FLOOR AREA FR69 STG48L HAS AN AREA THAT EXTEND 2" FWD OF FR 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14.Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00458Seat Track · gougedMDCC ZONE 250, FS 54.2 LT SEAT TRACK NR 3 HAS GOUGES ON SCALLOP HOLE 1 - EA AREA. REMOVED AND REPLACED SEAT TRACK FITTING IAW A310-200 SRM 51-72-10.Mar 8, 2005 · N419FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00457Crossbeam · corrodedMDCC ZONE 250, FS 54.2 BETWEEN LT SEAT TRACK 4 -5, LATERAL STUCTURE HAS CORROSION AT SCREW HOLES. REMOVED AND REPLACED CROSS BEAM IAW A310-200 SRM 51-72-10.Mar 8, 2005 · N419FE · Airbus A310 · Fuselage Main, StructureSDR 05FDEA00456Plate · crackedLEFT WING LOWER AILERON ACCESS DOOR LANDING PLATE HAS CRACK IN IT. REMOVED CRACKED LANDING AND INSTALLED A NEW LANDING IAW A310-200 SRM 51-72-10.Mar 8, 2005 · N419FE · Airbus A310 · AileronsSDR 05FDEA00455Adapter · corrodedMDCC ZONE 251 FS 60 BETWEEN RT SEAT TRACK NR 4 - 5, 1 - EA. CLS ADAPTER BROKEN. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.Mar 8, 2005 · N419FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00454Adapter · gougedMAIN CABIN FRAME 36, CLS ADAPTER -Y60 IS GOUGED, BETWEEN SEAT TRACK 3 - 4 LT. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.Mar 8, 2005 · N419FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00453Angle · corrodedTHS ACTUATOR STRUCTURAL HOUSING HAS APPROX 12 INCH OF CORROSION (10 EA. AREAS). REMOVED CORROSION IN 10 EA AREAS ON THS ACTUATOR STRUCTURAL HOUSING. ALL AREAS WERE WITHIN LIMITS EXCEPT AREA 10 WHICH WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED L-ANMar 8, 2005 · N446FE · Airbus A310 · Horizontal Stabilizer StructureSDR 05FDEA00452Shear Tie · corrodedBULK PIT UNDER FLOOR STG 55L FROM FS 65 TO FS 66 HAS CORROSION AND CORROSION. EXTENDS BETWEEN SPLICE ANGLE AND STG AND UNDER SHEAR TIE AT FS 66. REMOVED CORROSION IAW A310-200 SRM 51-74-10. STRINGER CORRODED BEYOND ALLOWABLE LIMITS AS PER A310-200 SRM 51-10Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Internal Mounting StructureSDR 05FDEA00451Floorbeam · corrodedAFT PIT FLOOR FS 66 10 INCH TO RT OF CTR HAS A 5 INCH BY 2 INCH AREA OF CORROSION. REMOVED CORROSION PER A310-200 SRM 51-74-10. CORROSION OUT OF LIMITS PER SRM 51-10-00. REMOVED CORRODED FLOORBEAM AND INSTALLED NEW BEAM PER A310-200 SRM 51-72-10. REPROTECTMar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Floor BeamSDR 05FDEA00450Skin · corrodedAFT PIT UNDER FLOOR 16 INCH FWD OF FS 54.1, STG 47R HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED AND REPLACED DAMAGED AREA IAW A310-200 SRM 53-10-14. TREATED, PRIMED, TOPCOATED IAW A3Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00449Shear Tie · corrodedBULK PIT UNDER FLOOR STG 53R FROM 1 INCH FWD OF 66 TO FR 67 HAS CORROSION EXTENDING UNDER SHEAR TIE AT FR 66 AND EXTENDING UNDER FASTENERS IN SEVERAL AREAS. REMOVED CORROSION, CHECK LIMITS MAT'L LOSS EXCEEDED LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVEMar 8, 2005 · N446FE · Airbus A310 · Fuselage Internal Mounting StructureSDR 05FDEA00448Structure · corrodedAFT PIT UNDER FLOOR FROM 12 INCH FWD OF FS 59 TO 3 INCHES FWD OF FS 59 STG44L HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. THE AREA WAS FOUND OUT OF LIMITS IAW A310-200 SRM 53-10-00. REPAIRED STRINGER IAW A310-200 SRM 53-10-14. TREATED, PRIMEMar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, StructureSDR 05FDEA00446Skin · lightning strikeLT FUSELAGE FRAME 11A APPROX AT STR 18L HAS A LIGHTNING STRIKE. BLENDED OUT AREA IAW SRM 51-73-10 AND 53-10-12 FIG 220 SH 1. 34 PERCENT MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-12-12 DIA 104. REPAIRED SKIN WITH DOUBLER AND FILLER ONLY PER SRM 53-Mar 8, 2005 · N419FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00445Adapter · corrodedMDCC ZONE 241, FR 39, BETWEEN NR 2 - 3 RT SEAT TRACK LCS ADAPTER HAS 1 AREA OF CORROSION INSIDE SCALLOP HOLE. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.Mar 8, 2005 · N419FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00444Adapter · crackedMDCC ZONE 250, FR 55/58 BETWEEN LT SEAT TRACK 2 - 3, 1 EA, CLS ADAPTER BROKEN. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.Mar 8, 2005 · N419FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00443Flap Track · corrodedRT WING FLAP O/B UPPER SURFACE AT NR 3 FLAP TRACK AND NR 4 FLAP TRACK HAS 2 EA AREAS OF NOTED CORROSION REF N00771. REMOVED CORR IAW SRM 51-74-10, FOUND IN LIMITS IAW SRM 57-53-12.Mar 8, 2005 · N446FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA00442Skin · puncturedRT WING I/B FLAP UPPER SURFACE 3.9 IN FROM T/E AND 30 IN FROM I/B END SKIN PUNCTURED REF N00914. REPAIRED FLAP IAW SRM 57-52-12 FIG 4D.Mar 8, 2005 · N446FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA00441Attach Fitting · corrodedVERTICAL STAB UPPER EDGE LEFT AND RIGHT FORE TO AFT HAS CORROSION AROUND CAP ATTACH FASTENER HOLES REF N00734. REMOVED AND REPLACED RT CHORD IAW SRM 51-40-21 AND DRW A55371360 AND REPAIRED LT CHORD IAW SRM 51-74-40 FIG 201Mar 8, 2005 · N446FE · Airbus A310 · Vertical Stabilizer, Attach FittingsSDR 05FDEA00440Doubler · damagedREPAIR ON RT ELEVATOR I/B T/E LOWER SURFACE REQUIRES EVALUATION REF N00817. REMOVED EXISTING REPAIR AND INSTALLED CORRECT REPAIR IAW SRM 55-21-11 CONF 1 FIG 203 AND EA 6-5510-86111.Mar 8, 2005 · N446FE · Airbus A310 · Elevator, Plate/SkinSDR 05FDEA00438Panel · damagedRT WING PANEL 650KB HAS 4 EA ELONGATED HOLES REF N00521. REPAIRED PANEL IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00437Panel · damagedLT WING PANEL 550HB HAS 2 EA ELONGATED HOLES REF N00520. REPAIRED HOLES IAW EA 6-5710-85051.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00436Panel · damagedRT WING PANEL 650HB HAS 3 EA ELONGATED HOLES REF N00523. REPAIRED PANEL 650HB IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00426Rib · crackedRT WING L/E UPPER SIDE OF PANEL LANDING, LANDING FOR PANEL HAS 2 EA CRACKS AT 11 IN I/B OF RIB 14 AND 11 IN O/B OF RIB 14 REF N00631. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A57244165.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Rib/BulkheadSDR 05FDEA00424Door · damagedNOSE LANDING GEAR DOORS HAS STRUCTURAL DAMAGE REF N00748. REPAIRED RT GEAR DOORS IAW SRM 52-82-11 C1 FIG 201.Mar 8, 2005 · N446FE · Airbus A310 · Landing Gear DoorsSDR 05FDEA00423Skin · crackedRT WING T/E SKIN HAS A .4 CRACK ON IB CORNER OF CUTOUT FOR PANEL 681 AB REF N00265. REPAIRED SKIN IAW EA 6-5710-86028.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00422Skin · damagedREPAIR FUSELAGE AT LT ELEVATOR T/E AFT FROM OB END HAS NO DATA REF N00806. REMOVED AND INSTALLED CORRECT REPAIR IAW EA 6-5100-87090 REF A310 SRM 55-21-11, REPAIR NR 5 G.Mar 8, 2005 · N446FE · Airbus A310 · Elevator, Plate/SkinSDR 05FDEA00421Seat Track · corrodedNR 4 SEAT TRACK LT OF CENTER FROM FS 16 TO FS 18 HAS CORROSION REF N00519. REMOVED AND REPLACED SEAT TRACK FROM FS 16 TO FS 18 IAW SRM 51-40-21 AND EA 6-5310-86038.Mar 8, 2005 · N446FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR CA050309006Rudder · separated(CAN) AFTER DEPARTURE IN CRUISE AT 35000 FT, THE CREW REPORTED THAT A LOUD BANG WAS HEARD. THE PILOT TOOK MANUAL CONTROL AND RETURNED TO LAND SAFELY AT THE DEPARTING AIRPORT. VISUAL INSPECTION AFTER LANDING REVEALED THAT A LARGE PORTION OF THE RUDDER SURFACE Mar 5, 2005 · Airbus A310 · Rudder StructureSDR VW3R20050009Extension · defectiveGIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. PLEASE NOTE THIS EVACUATION SLIDE IS ALSO USED ON A310 AIRCRAFT.Feb 11, 2005 · Airbus A310 · Escape SlideSDR 05FDEA00039Skin · corrodedRT 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.Jan 6, 2005 · N454FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00038Skin · corrodedRT 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.Jan 6, 2005 · N454FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00034Fairing · crackedNR 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.Jan 6, 2005 · N454FE · Airbus A310 · Nacelle/Pylon, Main FrameSDR 05FDEA00033Skin · damagedNON-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.Jan 6, 2005 · N454FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA00027Skin · damagedFUSELAGE REPAIR AT APROX. FS 1 STR 56 LT. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5310-81826.Jan 6, 2005 · N454FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00026Skin · damagedFUSELAGE - REPAIR AT APROX. FS 63 STR 42 RT. REPAIRED IAW SRM 53-17-12, FIG 203.Jan 6, 2005 · N454FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 04FDEA03418Proximity Sensor · malfunctionedNR 1 AUTOPILOT, FLIGHT DIRECTOR AND PITCH TRIM INOP. REMOVED AND REPLACED FCC NR 1 IAW A310 MM 22-18-34-4. AFS LAND TEST WILL NOT PASS, FAILS TEST AT DIFFERENT PHASES. AUTO PILOTS ENGAGE INTERMEDIATELY. AUTO THROTTLE WOULD DISENGAGE AT RANDOM. PITCH TRIM Dec 15, 2004 · N435FE · Airbus A310 · Landing Gear Position and WarningSDR 04FDEA03417Control Handle · obstructedSLATS WOULD NOT RETRACT AFTER TAKEOFF. SLAT/FLAP HANDLE WOULD ONLY OPERATE BETWEEN 15/0 AND 20/20 POSITIONS. RETURNED TO MEM AND MADE 20/20 LANDING. NO OTHER INDICATIONS OF MALFUNCTION ON SFPI OR FLAPS/SLATS SYS 1/2 INDICATIONS. FOUND DEBRIS IN FLAP HANDLEDec 15, 2004 · N425FE · Airbus A310 · Trailing Edge Flap Control SystemSDR VW3R200400004Girt Bar · mislocatedGIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PAD RIDES UP ON CAVITY RIDGE OF GIRT BAR.Dec 10, 2004 · Airbus A310 · Escape SlideSDR 04FDEA03379Fitting · damagedACCOMPLISH MAINTENANCE "C" CHECK #003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND, SEVERAL HOLES OF FITTINGS AT ACCESS DOORS (1Dec 6, 2004 · N452FE · Airbus A310 · Air Conditioning DoorsSDR 04FDEA03378Fitting · damagedACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND SEVERAL HOLES OF FITTINGS AT ACCESS DOORS (Dec 6, 2004 · N452FE · Airbus A310 · Air Conditioning DoorsSDR 04FDEA03377Skin · dentedACCOMPLISH MAINTENANCE "C" CHECK, NR 003 ENT BY: 067708, PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. LEFT WING, KRUEGER FLAP OUTER SURFACE FOUND DENTED. Dec 6, 2004 · N452FE · Airbus A310 · Leading Edge DevicesSDR 04FDEA03376Fairing · damagedACCOMPLISH MAINTENANCE "C" CHECK, 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. PYLON NR 2, LOWER AFTER FAIRING WITH INTERIM REPAIR ONDec 6, 2004 · N452FE · Airbus A310 · Nacelle/Pylon, Main FrameSDR 04FDEA03375Skin · wornACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. FUSELAGE, WEAR AT EXTERIOR FUSELAGE SKIN SURFACE ON FDec 6, 2004 · N452FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 04FDEA03374Structure · misrepairedVERTICAL STAB TOO LARGE COMPOSITE REPAIR ON LT SIDE L/E. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-50375, DATED 06/23/2000. DAMAGED STEEL COVER WAS REPAIRED BY NEW ONE, IAW EA 6-5500-50375.Dec 6, 2004 · N452FE · Airbus A310 · Vertical StabilizerSDR 04FDEA03373Fairing · damagedREPAIR, NR 4 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49991 REV NO. POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:48:9 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:44:51:3 S=M. COMPLIEDec 6, 2004 · N452FE · Airbus A310 · Trailing Edge FlapsSDR 04FDEA03372Fairing · damagedREPAIR, NR 2 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49992 REV NO POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:56:3 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:45:04:9 S=M. COMPLIEDDec 6, 2004 · N452FE · Airbus A310 · Trailing Edge FlapsSDR 04FDEA03371Structure · damagedCOMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R, DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708 LT WING, REPAIRS (2 EA) LT INBD FLAPDec 6, 2004 · N452FE · Airbus A310 · Trailing Edge FlapsSDR 04FDEA03349Skin · damagedCOMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. RT WING REPAIR RT INBD FLAP LWR SURFACE. REPAIRED IAW EA 6-5750-81812Dec 5, 2004 · N452FE · Airbus A310 · Trailing Edge FlapsSDR 04FDEA03348Skin · damagedREPAIR RT OUTBOARD TE FLAP LOWER SURFACE OUTBOARD OF NR 2 CANOE FAIRING. REPAIRED IAW EA 6-2750-50362, DATED JUNE/16/2000.Dec 5, 2004 · N452FE · Airbus A310 · Trailing Edge Flaps
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