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 04FDEA03347Skin · activatedCOMPLY 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. REPAIR RT INBD FLAP UPPER SURFACEDec 5, 2004 · N452FE · Airbus A310 · Trailing Edge FlapsSDR 04FDEA03346Skin · damagedCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 24 NOV0 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. REPAIR APPROX FS 59 FWD OF RT AFT CARGODec 5, 2004 · N452FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 04FDEA03345Structure · gougedNR 1 ENGINE, THRUST REVERSER RT FOUND WITH WEAR CLOSE TO BREATHER. ACCOMPLISHED IAW EA 6-7830-81809.Dec 5, 2004 · N452FE · Airbus A310 · Engine Thrust ReverserSDR 04FDEA03344Skin · crackedPYLON LOWER SPAR, INSP FOR COMPLY WITH E.O. 6-5450-7-3302 REV NO. B3 POS PT3 ENT BY: 067708. NR 1 PYLON, LOWER AFT FAIRING WITH LOOSE RVTS, CRK'D AND PAINT IN BAD CONDITION. LOWER FAIRING REPAIRED IAW EA 6-5480-81814. REINSTALLED IAW AMM 54-55-00. PAINTEDDec 5, 2004 · N452FE · Airbus A310 · Nacelle/Pylon, Plate/SkinSDR 04FDEA03333Floorbeam · corrodedBULK CARGO FLOOR STRUCT RT SIDE FS 64 TO 67 FLOOR STRUCTURE W/MULTIPLE CORRODED FROM TOP TO UNDERNEATH SURFACE. REMOVED AND REPLACED TEE PROFILE AT FS 63 TO FS 67 RBL 37 RT IAW A310 SRM 51-40-21.Dec 2, 2004 · N422FE · Airbus A310 · Fuselage Main, Floor BeamSDR 04FDEA03271Screw · brokenAFTER TAKEOFF, THE FLAP HANDLE COULD NOT BE MOVED PAST THE FLAPS 0 DEGREES, NOR COULD MOVE IT PAST THE FLAPS 20 DEGREE POSTION. THE FLAPS DID MOVE FROM THE 20 DEGEES TO 15 AND BACK. FOUND SPECIAL-SCREW ITEM 161 REF A310-200 IPC 53-11-31-13 BROKEN. PARTS NEENov 30, 2004 · N425FE · Airbus A310 · FastenersSDR 04FDEA03230Stringer · damagedTWO HOLES HAVE DAMAGE, 1 GOUGED AND 1 MISDRILLED ON BACK SIDE, FS 54 LT SIDE STRINGERS 35 AND 37 AS MARKED. COMPLIED WITH EA 6-5310-84341.Nov 26, 2004 · N401FE · Airbus A310 · Fuselage Main, Longeron/StringerSDR 04FDEA03182Computer · malfunctionedUSING TOGA FOR T/O ON A WET SLIPPERY RWY. THROTTLE 2 RACED TO TRP THRUST LIMIT BUT THROTTLE 1 REMAINED AT 40 PERCENT N1, DISCONTINUED T/O ATTEMPT. REMOVED AND REPLACED THRUST CONTROL COMPUTER AS PER AMM 22-36-34-4-02. PERFORMED AFS TEST/LAND TEST AS PER AMNov 22, 2004 · N456FE · Airbus A310 · Auto Throttle SystemSDR 04FDEA03176Stringer · corrodedTHS BAY PROFIL STRINGER HAS 4" OF CORROSION FS 90 RT OVER TORQUE BOX. REMOVED T-PROFILE AT FS 90 ON UPPER RT EDGE BEAM THAT WAS CORRODED OUT OF LIMITS AND REPLACED IAW A310/200 SRM 51-72-10.Nov 21, 2004 · N422FE · Airbus A310 · Fuselage Main, Longeron/StringerSDR 04FDEA03175Seat Track · damagedLEFT SEAT TRACK NR 5 FROM FS 18 TO 21 BETWEEN FS 20 AND 21 HAS MATERIAL REMOVED OUT OF LIMITS, LOCATION B(65 INCHES) OTBD. REPAIRED BY REMOVING DAMAGED SECTION AND SPLICING IN A NEW SECTION IAW A310/200 SRM 53-10-16 FIG 208.Nov 21, 2004 · N422FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03173Skin · damagedRIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650KB HAS 1 EA ELONGATED SCREW HOLE AS MARKED AREA RIB 23 TO 24. COMPLIED WITH FED EX ENGINEERING AUTHORIZATION 6-5710-83632 (NOTE: MAJOR REPAIR PER EA ).Nov 20, 2004 · N401FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA03172Skin · damagedRIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650 HB HAS 6 EA ELONGATED SCREW HOLES AS MARKED AREA RIB 21 AND 22. COMPLIED WITH FEDEX ENGINEERING AUTHORIZATION 6-5710-83632.Nov 20, 2004 · N401FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA03192Uplock · failedAFTER TAKEOFF, NOSE GEAR AMBER "DOOR" WARNING LIGHTS (FWD AND OVERHEAD) REMAINED ON FOLLOWING GEAR RETRACTION. NO EXCESSIVE NOISE OR VIBRATION OBSERVED. WHEN GEAR WAS EXTENDED AGAIN, "DOOR" LIGHT REMAINED ON (BOTH FORWARD AND OVERHEAD INDICATIONS) RETURNED TNov 18, 2004 · N408FE · Airbus A310 · Landing Gear Position and WarningSDR 04FDEA03024Skin · delaminatedLT WING OUTBOARD TE PANEL (BOTTOM SKIN - FOUND 6 LOCATIONS WITH DELAMINATION. AREAS OF DELAMINATION ARE AS FOLLOW (INBD TO OUBD): 1: 36.5 X 12, 2: 14 X 14, 3: 4 X 3, 4: 2.5 X 2.5, 5: 2 X 0.5, 6: 1.5 X 0.5 ......NOTED 2EA EXISTING REPAIRS ON UPPER SKINNov 7, 2004 · N456FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02996Thrust Reverser · inoperativePDIS 447 78-30 0007243 27OCT04 MCI OPEN U NR 1 REVERSER UNLOCK LITE ON T/O. REJECTED T/O AT 70 KNOTS. MEL 27OCT04 05:03 MCI U ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 06NOV04 (MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) Oct 27, 2004 · N447FE · Airbus A310 · Engine Thrust ReverserSDR 04FDEA02993Warning Light · illuminatedFUEL FILTER CLOG LIGHT ON T/O AT 60KTS. REJECTED T/O. ALL INDICATIONS NORMAL ON 60 PERCENT RUNUP FOR ENG ANTI-ICE. ECAM WARNING STOPPED STOPPED AS SOON AS POWER WAS REDUCED. I THINK IT WAS NR 1 ENG, BUT AM NO T POSITIVE. ENT BY: 001941 RPT BY: 119121 FAOct 25, 2004 · N410FE · Airbus A310 · Engine Fuel DistributionSDR 04FDEA02924Frame · dentedN00196 INCOMING CONDITION, JUST FORWARD OF FRAME 10 RT SIDE IS A DENT 1 INCH X .5 INCH X .050 INCH WHICH IS OUT OF LIMITS IAW SRM 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER AND FILLER C/W EA 6-5330-55381 AND SRM 51- 71-70, TECHNICAL REQUEST OE-356-09-Oct 12, 2004 · N410FE · Airbus A310 · Fuselage Main, FrameSDR 04FDEA02923Frame · dentedN00197, INCOMING CONDITION, JUST FORWARD OF FR 10 LT SIDE IS A DENT (2 INCH X 2 INCH X .090 INCH) WHICH IS OUT OF LIMITS IAW SRM TABLE 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER, FILLER IAW EA 6-5330-55382 AND SRM 51-71-70, EO-356-09-04-007-2/-4, DWG R536 Oct 12, 2004 · N410FE · Airbus A310 · Fuselage Main, FrameSDR 04FDEA02887Roller Tray · corrodedAFT CARGO FLOOR STRUCTURE FR 60, RT SIDE ROLLER TRAY STRUCTURE NOTED CORROSION TOP TO UNDERNEATH NUTPLATES AS MARKED. REMOVED CORROSION ON RT SIDE ROLLER TRAY STRUCTURE AT FR 60 2 EA AREAS. MAX MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW A310 SRM 51-74-10Oct 7, 2004 · N422FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02872Proximity Sensor · malfunctionedGEAR WOULD NOT RETRACT AFTER TAKEOFF IN EITHER SYSTEM. PERFORMED BITE TEST OF PROX DETECT UNIT 54GB. NO MEMORIZED FAULTS. PERFORMED SYS TEST WITH THE FOLLOWING SENSOR FAULTS, 03 (LT BOGIE SYS 1), 04 (RT BOGIE SYS 1), 05 (NOSE CENTERED SYS 1), 06 (LT MLGOct 5, 2004 · N415FE · Airbus A310 · Landing Gear Position and WarningSDR 04FDEA02835Panel · damagedPANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1.Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02834Panel · damagedPANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998.Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02833Panel · damagedPANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02810Seat Track · crackedMAIN CABIN FR52 SEAT DUMMY TRACK (CLS ADAPTOR) AT TRACK 2R, 24 INCHES TO RT OF CTRIS, CRACKED UNDERNEATH AT BEND RADIUS APPROX 4 IN LONG. REMOVED AND REPLACED CLS ADAPTOR FR52 2R IN MAIN CABIN IAW SRM A310/200 51-40-21.Sep 23, 2004 · N410FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02795Floorbeam · corrodedAFT CARGO COMPT FS 63 FLOOR STRUCTURE, ON LEFT SIDE 3EA AREAS OF CORROSION ON TOP SURFACE AND UNDERNEATH FLOOR STRUCTURE. REMOVED AND REPLACED FLOOR STRUCTURE BEAM IAW A310 SRM 51-40-21.Sep 21, 2004 · N411FE · Airbus A310 · Fuselage Main, Floor BeamSDR 04FDEA02724Seat Track · crackedMDCC SEAT TRACK SECTION AT R2, BETWEEN FR54 TO 8 INCHES AFT OF FR54.1 HAS DAMAGE TO THE SCALLOP LUGS. (ON EDGES AND BENEATH LUGS) REMOVED DAMAGE AND FOUND TO BE CRACKED IAW SRM 51-73-10. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21.Sep 17, 2004 · N411FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02692Floor Support · corrodedBULK CARGO COMPT. FLOOR STRUCTURE FR66 LT SIDE , MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW SRM 51-74-10, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D CSep 16, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02691Floor Support · corrodedBULK CARGO COMPT. FLOOR STRUCTURE, ON RT SIDE FR 66 TO FR 63 CORROSION ON TOP AND BENEATH SURFACE. REMOVED CORROSION IAW SRM 51-70-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D COMING ****Sep 16, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02679Seat Track · crackedDAMAGED SEAT TRACK ADAPTER AT FRAME 61 CENTER LINE REF EA 6-5320-81893. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21 AND EA 6-5320-81893. **** S/D COMING ****Sep 14, 2004 · N411FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02678Seat Track · crackedMAIN CARGO DECK AT FRAME 47 BETWEEN TRACKS 1R AND 2R, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK AT FRAME 47 BETWEEN TRACKS 1R AND 2R IAW A310 SRM 51-40-21.**** S/D COMING ****Sep 14, 2004 · N411FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02677Dampener · inoperativeAFTER TAKEOFF YYC, ATTEMPTED TO RAISE GEAR, ABLE, TO THE INTERLOCK POSITION, INDICATED GEAR DOWN, UNLOCKED TRIED CYCLING GEAR AND CIRCUIT BREAKERS. NO LT GEAR PITCH DAMPENER POPPET EXTENDED. LT GEAR PITCH DAMPER REPLACED IAW AMM 32-11-15-4. NR 2 MAIN WHEEL RSep 14, 2004 · N407FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 04FDEA02675Dummy Rail · crackedMCD AT FR 53 BETWEEN SEAT TRACKS 2L AND 3L, DUMMY TRACK IS CRACKED UNDERNEATH AT T-CAP RADIUS. REMOVED AND REPLACED CROSSBEAM, P/N A5381293420000 IAW A310 SRM 51-40-21.Sep 11, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02606Fairing · crackedSMIS 453 05-21 0003629 28JUN04 MC1 OPEN R WS-P 00026805 MOD TYPE H MOD NR C-CHECK REV NR PS ACCOMPLISH MAINTENANCE C-CHECK NR 002 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 28JUN04 19:47:42:3 BY:067708 S=M PLND: DATE:01AUG04 AT: LIS-VNSep 2, 2004 · N453FE · Airbus A310 · Aerodynamic FairingsSDR 04FDEA02587Dummy Rail · crackedREF. SNRM N00259, MAIN DECK CARGO COMPT. AT FR 43 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02586Dummy Rail · crackedMAIN DECK CARGO COMPT. AT FR 45 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02585Dummy Rail · crackedMAIN DECK CARGO COMPT. AT FR53 BETWEEN R1 AND R2 SEAT TRACK DUMMY TRACK IS CRACKED . REMOVED AND REPLACED DUMMY TRACK IAW A310-200 SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02584Dummy Rail · crackedREF. SNRM N00257 MAIN DECK CARGO COMPT. AT FR 46 DUMMY TRACK IS CRACKED BETWEEN R1 AND R2 SEAT TRACKS. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02583Dummy Rail · crackedMAIN DECK CARGO COMPT AT FR 40/41 BETWEEN R1 AND R2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02582Dummy Rail · crackedREF. SNRM N00261 MAIN DECK CARGO COMPT. AT FR 42 BETWEEN L1 AND L2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02581Pan · corrodedREF. SNRM N00246 LWR FWD CARGO FR21 30 INCHES LT OF CENTER DATUM FLOOR CARGO ELECTRIC ROLLER PAN HAS CORROSION. REMOVED AND REPLACED WITH NEW ROLLER PAN IAW A310/200 SRM 51-40-21.Aug 31, 2004 · N414FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02564Control Module · inoperativeLANDING GEAR FAIL TO RETRACT ON TAKEOFF. QRH PROCEDURES FOLLOWED BUT GEAR HANDLE WOULD NOT RETRACT. OVER WEIGHT QRH PROCEDURES FOR LANDING COMPLETED. LANDED AT 290,000 LBS AT FPM SINK RATE, SMOOTH LANDING, NO CROSS WINDS FACT 26AUG04 05:03 PVG U T/S IAW Aug 25, 2004 · N419FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 04FDEA02631Stringer · corrodedMDIS 421 53-10 0009094 03SEP04 SIN OPEN U FUSELAGE STRINGER 44 LT FRAME 13A TO 16A FOUND CORRODED AT MULTIPLE LOCATIONS. ENT BY: 086361 RPT BY: 086361 SHGN 03SEP04 07:32 SIN U SDR HAS BEEN SUBMITTED. ENT BY: 086361 RPT BY: 086361**** S/D COMING **Aug 24, 2004 · N421FE · Airbus A310 · Fuselage Main, Longeron/StringerSDR 04FDEA02547Crossbeam · crackedQA PICKUP FLOORBEAM AT FWD FACE OF FR 33 BETWEEN Y450 AND Y953 WITH HAIR LINE CRACK.Aug 23, 2004 · N421FE · Airbus A310 · Fuselage Main, StructureSDR 04FDEA02441Seat Track · corrodedMAIN CABIN CARGO FLOOR 3 AREAS OF CORROSION ON SEAT TRACKS AT FR66 AND FR67 ZONE 251 TRACK F. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW SRM 53-10-16Aug 11, 2004 · N412FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02394Outflow Valve · inoperativePDIS 415 21-30 0007170 FWD NR 1 OUTFLOW VALVE STUCK IN THE OPEN POSITION (AMBERARROW ON ECAM). NR 1 PRESS REGULATOR IN USE-ECAM SHOWED 0 V/S AND CABIN ALT. AT 260 FT. WHEN SWITCHED TO NR 2 REG. ECAM SHOWED ACTUAL V/S MATCHED A/C CLIMB RATE AND CABIN Aug 6, 2004 · N415FE · Airbus A310 · Pressure Regulator/Outflow ValveSDR 04FDEA02365Valve · inoperativePDIS 447, 78-30 0007040 05AUG04 CAE OPEN ON T/O AT 43 PERCENT N1,GOT REV UNLOCK LIGHT. MEL 05AUG04 05:40 CAE R ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 15AUG04 MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2)1. THRUST REVERAug 5, 2004 · N447FE · Airbus A310 · Engine Thrust ReverserSDR 04FDEA02366Module · failedPDIS 450 32-60 0006380 05AUG04 MEM CLOSE R LOGPAGES: 00675737 GEAR HANDLE WOULD NOT RAISE. TRIED BOTH POSITIONS. GOT ALL 3 RED DOOR LIGHTS. BUT GEAR INDICATIONS SHOWED ALL 3 DOWN. CHECKED CONTROL BOX FOR FAULTS,NO FAULTS LOGGED, JACKED A/C RAN Aug 4, 2004 · N450FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 04FDEA02338Tee Fitting · corrodedREF. SNRM N00243 MDCC T-CAP JUST AFT OF COCKPIT DOOR HAS LEVEL 2 CORROSION REMOVED CORROED T-CAP SECTION INSTALLED A SPLICE IN SECTION IAW A310/200 SRM 53- 12-15, 51-40-20, AND 51-75-10Aug 1, 2004 · N412FE · Airbus A310 · Fixed Inner DoorsSDR 04FDEA02337Seat Track · corrodedREF. SNRM N00381, MDC BETWEEN FR15A AND FR19 SEAT TRACK 4L HAS (LEVEL 2) CORROSION 12 INCHES FWD OF FR17. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-12-16 AND DWG A53610798Aug 1, 2004 · N409FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02336Panel · dentedRT WING OB T/E PANEL ZONE 691 HAS 100 DENTS, OF WHICH 40 ARE DELAMINATED (TOP AND BOTTOM OF PANEL) ( AREA 2 INCHES X 12INCHES ) REMOVED DAMAGED T/E PNL AND INSTALLED NEW T/E PNL IAW A310/200 DWG 57243876.Aug 1, 2004 · N409FE · Airbus A310 · Wing, Plate/Skin
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