Airbus A310-203

Service difficulty reports · 2,392

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = 'A310203'
  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 FDEA201108153281Fitting · failedNLG LEG DOOR LOWER RT ATTACHMENT FORK BROKEN. R & R NLG LEG DOOR RT FITTING AND ATTACHMENT FORK ,OPS CHECKED GOOD ALL IAW 32-22-15-04.Aug 15, 2011 · N411FE · Airbus A310203 · Landing Gear Door Retract SectionSDR FDEA201108153280Channel · bentINNER FUSELAGE "U" CHANNEL IS BENT STR 33L BETWEEN FR 83 TO FR 84. R & R CHANNEL AT STR 33L BETWEEN FR 83 TO FR 84 IAW SRM 51-40-21. PARAGRAPH 7.Aug 15, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201108143274Intercostal · bentINTERCOSTAL AND UPPER ANGLE ARE BENT STR 33R. INNER FUSELAGE BETWEEN FRAME 85 AND FRAME 86. REMOVED AND FAB AND INSTALLED INTERCOSTAL ANGLE ON FR 85 TO 86 RT STRINGER 33R, REF SRM 51-40-21, PG7 REPROTECTED AREA IAW SRM 51-75-10.Aug 14, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201108133264Floor Panel · delaminatedFLOOR PANEL 242UJ HAS IMPACT DAMAGE. CUTOUT DAMAGE, & FABRICATED REPLACEMENT FLOOR PANEL 242UJ IAW DWG SRZ 25-005, REV J.Aug 13, 2011 · N411FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201108123242Tee Fitting · crackedONE CRACK INDICATION EXCEEDS 25 PERCENT FSH, WAS FOUND AT NR 63 FASTENER HOLE OF LT CENTER WING REF PART 6, NTM 51-10-01 PROCEDURE A, RECORD SHEET FIG 610 AND NTM PART 6 57-10-12. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MAJOR.Aug 12, 2011 · N428FE · Airbus A310203 · Fuselage Main, KeelSDR FDEA201108123241Structure · crackedONE CRACK INDICATION EXCEEDS 25 PERCENT FSH WAS FOUND AT NR 63 FASTENER HOLE OF RT CENTER WING, REF NTM PART 6 51-10-01 PROCEDURE A RECORD SHEET FIG 611 AND NTM PART 6-57-10-12. CRACK REAMED TO THE NEXT NOMINAL DIAMETER 0.561" IAW EO 6-5710-7-3322 PART 1. NDAug 12, 2011 · N428FE · Airbus A310203 · Wing, Center BoxSDR FDEA201108123240Structure · crackedONE CRACK INDICATION EXCEEDS 25 PERCENT FSH WAS FOUND AT NR 30 FASTENER HOLE OF RT CENTER WING, REF NTM PART6 51-10-01, PROCEDURE A, RECORD SHEET FIG 612 AND NTM PART6 57-10-12. CRACK REAMED TO THE NEXT NOMINAL DIAMETER SIZE 0.561" IAW EO 6-5710-7-3322 PART 1Aug 12, 2011 · N428FE · Airbus A310203 · Wing, Center BoxSDR FDEA201108123247Adapter · failedCLEVIS ADAPTOR AT FRAME 43 BETWEEN SEAT TRACKS 2R AND 3R BROKEN. REMOVED AND REPLACED CLEVIS ADAPTOR AT FRAME 43 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 51-40-21 & 51-72-10.Aug 12, 2011 · N411FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201108113220Skin · gougedUPPER AFT AREA OF AFT CARGO DOOR CUTOUT, EXT SURFACE, HAS MULTIPLE SCRATCHES EXTENDING 10" AFT OF CUTOUT (FR63) BETWEEN STRINGERS 27R & 28R. SMOOTHED AND BLENDED 10" SQ IN AFT CARGO DOOR CUTOUT EXT SURFACE FR63, STR 27 & 28 IAW SRM 51-73-10. MAP AREA FOR NAug 11, 2011 · N435FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108113219Panel · crackedRT HORIZ L/E PANEL 341AB, INTERNAL STIFFENER CRACKED AT AFT END, FROM FASTENER TO EDGE OF PART, .3125" LONG, UPPER AFT CORNER OF PANEL. REMOVED FASTENERS HORZ L/E PANEL 341AB STOP-DRILLED CRACK ON INTERNAL STIFFENER, NDT FOR CRACKS. NO CRACKS WERE FOUND, FABRAug 11, 2011 · N435FE · Airbus A310203 · Horizontal Stabilizer, Plate/SkinSDR FDEA201108113200Frame · corrodedAFT CARGO DOOR AFT EDGE SEAL LANDING STRIP GOUGED AT MULTIPLE PLACES ON FUSELAGE CUTOUT FR 63A R & R 3EA AFT CARGO DOOR AFT EDGE SEAL LANDINGS IAW SRM 51-72-10. UPON FURTHER EVALUATION, FOUND CORROSION AT FR 63A, STR 28R TO 29R, REMOVED CORROSION IAW SRM Aug 11, 2011 · N435FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201108083139Access Door · crackedAPU RT ACCESS DOOR 316AR AFT MATING FLANGE ON TAILCONE ASSY DEFORMED BELOW LATCH RECEPTACLE, MEASURED 4 IN LENGTH. REMOVED MATING FLANGE IAW SRM 51-40-21. INSTALLED NEW MATING FLANGE IAW SRM 51-40-21 AT AFT APU DOORS AFT MATING FLANGE.Aug 8, 2011 · N435FE · Airbus A310203 · Auxiliary Power Unit (APU) DoorsSDR FDEA201108083138Tray · corrodedAFT CARGO COMPARTMENT LT FWD PDU TRAY FLANGE IS BENT BETWEEN FR55 AND 56 AND NR 2L AND NR 3L TRACK ROLLERS. R & R PDU TRAY IAW SRM 51-40-21, DUE TO CORROSION FOUND OUT OF LIMITS IAW SRM 51-74-10 CORRODED AREA MEASURES 6.00L X 5.00 W X .012. MATERIAL LOSSAug 8, 2011 · N435FE · Airbus A310203 · Cargo CompartmentsSDR FDEA201108083133Hinge · crackedBOTTOM EXT FUSE EXT ELECTRICAL POWER PLUG ACCESS DOOR INNER DOUBLER CRACKED .2" IN LENGTH. REMOVED ELECTRICAL POWER PLUG ACCESS DOOR, R & R DAMAGED INNER DOUBLER, AND RE-INSTALLED ELECTRICAL POWER PLUG ACCESS DOOR IAW SRM 51-40-21, PARA 5 AND 6.Aug 8, 2011 · N435FE · Airbus A310203 · Accessory Compartment DoorsSDR FDEA201108073130Retainer · crackedRT WING NR1 SPOILER T/E RETAINER STRAP IS CRACKED APPROX 1" LONG INBD END. R & R RETAINER STRIP IAW CMM 57-71-11.Aug 7, 2011 · N435FE · Airbus A310203 · SpoilersSDR FDEA201108073132Access Panel · crackedRT WING L/E ACCESS PANEL NR 624EB CUT OUT LANDING IS CRACKED APPROX 1" LONG. R & R CUT OUT LANDING FOR ACCESS PANEL 624EB IAW SRM 51-40-01, PAR 6 & 7 AND SRM 51-40-44 PG1-16, SRM 51-40-21 PARA 6&7. APPLIED ALODINE, PRIMED AND PAINTED IAW SRM 51-75-10.Aug 7, 2011 · N435FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201108063116Skin · dentedLOWER FUSELAGE DENT 17 INCHES AFT OF LOWER CARGO DOOR. SKIN TRIMMED-OFF BETWEEN FR 26/32 TO FR 33, STR 32R TO 34R PER SRM 53-10-12 REV 79, FIG 225. HFEC INSPECTION CARRIED OUT PER NTM 51-10-08 REV 74 FOUND NO CRACKED EVIDENT. REPAIR DOUBLER FABRICATED ANDAug 6, 2011 · N436FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108063117Adapter · crackedCLEVIS ADAPTER AT FR 45 BETWEEN SEAT TRACK 2 & 3 RT IS CRACKED APPROX 1" LONG AT FWD FLANGE. R & R CLEVIS ADAPTER IN MDCC AT FR 45 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT IAW SRM51-40-21. FLOORBOARD LOCATED AND DRILLED IAW SRM 51-40-44. HOLES TREATED AND PROAug 6, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201108053112Support Bracket · crackedNR1 ENGINE THRUST REVERSER TRANSLATING COWL UPPER GUIDE SUPPORT SLIDER BRACKET CRACKED. REMOVED NR 1 ENG O/B TRANSLATING SLEEVE IAW A310-200 AMM 78-32-11-04. REMOVED CRACKED UPPER COWL GUIDE SUPPORT BRACKET IAW SRM 54-40-21 AND SRM 54-04-01 PG.11. FABRICATEAug 5, 2011 · N435FE · Airbus A310203 · Engine Thrust ReverserSDR FDEA201108033081Stringer · crackedRT SIDE STRINGER 9R BETWEEN FR 98 TO 100 HAS 2 PIECES BROKEN OFF. R & R STRINGER 9R FROM FR 95 TO 102 IAW SRM 51-72-10, PARA 5A & 6A. FABRICATED NEW STRINGER IAW DWG 19A53989507. REPROTECTED IAW SRM 51-21-10, 51-23-10, & 51-75-10.Aug 3, 2011 · N435FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201108033083Intercostal · bentINNER FUSELAGE INTERCOSTAL IS BENT STR 33L BETWEEN FR85 TO FR84. REMOVED INTERCOSTAL STR 33L BETWEEN FR85 TO FR84 IAW SRM51-40-21, PARA 6, B/S FABRICATED STIFFENER AND WEB IAW DWG A53986749.LOCATED AND DRILLED AND INSTALLED STIFFENER AND WEB ,FR85 TO FR84, STAug 3, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201108013054Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 36, 37, X = -35 FOUND DAMAGED. REMOVED AND REPLACED BY FABRICATION PER DWG SRZ-25-005, REV J. AND AS PER AMM 53-10-25 REV 30.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Aug 1, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201108013058Intercostal · bentINTERCOSTAL IS BENT STR 35R INNER FUSELAGE BETWEEN FR86 TO FR87. REMOVED DAMAGED INTERCOSTAL, REPLACED WITH NEW INTERCOSTAL AND STRIP AT STR 35R BETWEEN FR 86 AND FR87 IAW SRM51-75-10 AND SRM51-21-10.Aug 1, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107313046Structure · gougedRT WING SPOILER NR 7 LOWER T/E IS GOUGED APPROX .500" WIDE. R & R T/E OF RT WING NR 7 SPOILER IAW SRM 51-72-10.Jul 31, 2011 · N435FE · Airbus A310203 · SpoilersSDR FDEA201107303040Seat Track · damagedFLOOR TRACK L3 HAS DAMAGED RECEPTICLES LOCATED BETWEEN FLOORBEAM 61 AND 60. REMOVED DAMAGED SECTION FROM BETWEEN FRAMES 58 AND FRAMES 62 AND INSTALLED SPLICE REPAIR IAW SRM 53-10-16, FIG 208 SHEET 1. RESTORED PROTECTIVE COATINGS IAW SRM 51-75-10 AND 51-21-10Jul 30, 2011 · N435FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107303038Mount Bracket · crackedAFT UPPER PYLON RIB 21, 3 INCH CRACK AT WING TO PYLON MOUNT BRACKET. R & R TEE PICK-UP ANGLE IAW SRM 51-72-10, PGS 1-3 AND SRM 51-40-21, PGS 31-36.Jul 30, 2011 · N435FE · Airbus A310203 · Nacelle/Pylon, Attach FittingsSDR FDEA201107303037Access Panel · crackedLT EXTERNAL PACK AREA INBD LANDING FOR PANEL 143FL HAS .250. CRACK REMOVED LANDING FOR PANEL 143FL, INSTALLED NUTPLATES ON NEW LANDING IAW SRM 51-40-21. INSTALLED NEW LANDING ON LT EXTERNAL PACK AREA FOR PANEL 143FL IAW SRM 51-40-21.Jul 30, 2011 · N435FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201107293031Seal · wornPANEL 475CL FWD FINGER SEAL IS WORN APPROX 20 PERCENT ACROSS THE RT SIDE. REMOVED SEAL , FABRICATED NEW SEAL IAW SRM 51-40-44. INSTALLED NEW SEAL IAW SRM 51-40-21.Jul 29, 2011 · N435FE · Airbus A310203 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201107293021Bracket · bentFR 33, STGR 15L, 2 EA ISOLATOR BRACKET BENT. REMOVED 2 EA BRACKETS IAW SRM 51-40-21. FABBED 2 EA BRACKETS IAW DWG A53771078. ALODINED BRACKETS IAW SRM 51-21-10. PRIMED AND TOPCOATED IAW SRM 51-21-10, PARTMARKED IAW GMM 7-0-1001. INSTALLED 2 EA BRAKETS Jul 29, 2011 · N435FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201107293020Frame · corrodedAFT PRESSURE BULKHEAD LWR FWD SIDE CIRCUMFERENCE STRAP CORRODED 2 INCHES LENGTH X 3 INCHES WIDTH BETWEEN STGR 44L AND 46L. REMOVED AND REAPPLIED SEALANT ON AFT PRESS BULKHEAD FWD SIDE IAW SRM 51-74-10 PB 201, R & R ANGLE ANGLE SUPPORT IAW SRM 51-40-21; FABRJul 29, 2011 · N435FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201107293019Intercostal · bentINTERCOSTAL IS BENT STR 33R INNER FUSELAGE BETWEEN FR'S 86 AND 87 FABRICATED. REPLACEMENT INTERCOSTAL, LOCATED, DRILLED, INSTALLED AND REPROTECTED IAW SRM 51-40-44, DWG A539-86751 AND 51-42-11, PG 7-22 AND 51-75-10.Jul 29, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107273001Spring · bentLT MLG 2 DOWNLOCK SPRINGS BENT. REPLACED BENT SPRINGS LT MAIN GEAR LOCK LINK IAW AMM 32-11-19-04.Jul 27, 2011 · N411FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR FDEA201107273000Spring · bentRT MLG DOWNLOCK SPRINGS (2 EA) BENT. REPLACED BENT SPRINGS FOR RT MLG LOCK LINK IAW AMM 32-11-19-04.Jul 27, 2011 · N411FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR FDEA201107272992Strut · corrodedFUSELAGE TAIL SECTION FR 86, 2EA CROSS STRUTS CORRODED AT STR15 LT AND RT.Jul 27, 2011 · N428FE · Airbus A310203 · Aerodynamic FairingsSDR FDEA201107272988Structure · crackedNR 2 ENGINE INBD CORE COWL OUTER SURFACE FOUND 1EA CRACKED POSITION ABOUT 7 O'CLOCK. REPAIRED PER E.O. 6-5440-149014. REPAIR, PER G.M.M. 6-2-100, CLASSIFIED AS MINOR.Jul 27, 2011 · N428FE · Airbus A310203 · Nacelle/Pylon, Plate/SkinSDR FDEA201107272993Crossbeam · corrodedFUSELAGE TAIL SECTION FR84, 1EA CROSS STRUT GOT CORROSION AT STR14 LT 1. REMOVED THE CROSS STRUT IAW SRM 51-40-20 AND 51-40-21. INSTALLED NEW CROSS STRUT WITH FASTEN REF SRM 51-40-21. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 27, 2011 · N428FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201107272989Skin · dentedRT WING OTBD FLAP LOWER SURFACE FOUND LIGHTLY DENTS POSITION NEAR T/E AREA. THE DIMENSION OF THE DAMAGED AREA 4.6"L X 2.5 W X 0.063" MAX DEPTH. THE AREA IS OVER THE LIMITS IAW SRM57-53-12 (TOOL:TS 482). CUT THE DAMAGED AREA AND REPAIRED BY THE DOUBLER AND FAJul 27, 2011 · N428FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201107252942Roller Tray · corrodedINSIDE AFT CARGO COMPT AT THE BOTTOM SURFACE OF 2R ROLLER TRACK, CORROSION 2.5" X 3" AT 10" FWD OF FR62. AFTER REMOVAL OF BALL MATS FOUND 1EA AREA ON ROLLER TRAY TO BE LEVEL 1, OUT OF LIMITS IAW SRM 53-10-15, FIG 102, BEYOND REPAIR, R & R ROLLER TRAY IAW AT FJul 25, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107252941Seat Track · crackedCLS ADAPTER AT FS 43 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX 1 INCH LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2 & 3 IAW SRM 51-40-21.Jul 25, 2011 · N435FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107252937Adapter · crackedCLS ADAPTER AT FS 42 BETWEEN SEAT TRACK 2R AND 3R IS CRACKED APPROX 1.5" LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR42 BETWEEN SEAT TRACKS 2 AND 3RT IAW SRM 51-40-21.Jul 25, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107252931Stringer Splice · corrodedSTRINGER 26R SPLICE AT FRAME 54 HAS A 1 SQ IN AREA OF CORROSION, AFT SIDE OF FRAME. REMOVED CORROSION AT SPLICE PLATE AND FOUND LEVEL 1 CORROSION TO BE OUT OF LIMITS IAW SRM 51-73-10. R & R SPLICE IAW SRM 51-72-10.Jul 25, 2011 · N435FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201107242925Strap · corrodedRUDDER L/E ATTACH LANDING , RT SIDE , INTERNAL STRAP CORRODED, 2SQ IN , 6 INCHES ABOVE NR1 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10, PAR 5, FABRICATED NUT PLATE STRAP IAW DWG A554-71556, ALODINED IAW SRM 51-21-10 PG 6. PRIMED IAW SRM 51-75-10, Jul 24, 2011 · N435FE · Airbus A310203 · Rudder StructureSDR FDEA201107242929Rib · crackedLT PYLON AT RIB 22 UPPER AFT SIDE HAS A 2 IN LONG CRACK. R & R TEE PICKUP ON LT NR1 PYLON AT RIB 22 IAW SRM 51-72-10.Jul 24, 2011 · N435FE · Airbus A310203 · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201107242924Strap · corrodedRUDDER L/E ATTACH LANDING, RT SIDE INTERNAL STRAP CORRODED 2SQ IN, 8" ABOVE NR4 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10: FABRICATED PLATE IAW DWG A554-71556, ALODINED NUT PLATE STRAP IAW SRM 51-21-10 PAR.6, PRIMED IAW A310-200 SRM 51-75-10 PJul 24, 2011 · N435FE · Airbus A310203 · Rudder StructureSDR FDEA201107242923Bracket · crackedFR26, STR 15 LT ISOLATOR BRACKET BROKEN IAW AMM 25-50-00-06. R & R ISOLATOR BRACKET AT FR 26 STR 15 LT IAW SRM 51-72-10 & 51-40-21, PARA 6.Jul 24, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107232913Skin · chafedNR 2 ENGINE OTBD THRUST REVERSER UPPER SIDE T/E AREA FOUND SKIN CHAFED. ACCOMPLISHED THE EA 6-7830-149011. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR.Jul 23, 2011 · N428FE · Airbus A310203 · Engine Thrust ReverserSDR FDEA201107222908Floorboard · damagedAFT CARGO FLOORBOARD 152EF MISSING EDGE FILLER DEFCT MEASURES 2 SQ INCHES. FABRICATED REPLACEMENT FLOORBOARD 152EF IAW DWG SR2 25-005, REV J.Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107222907Floor Panel · crackedFLOOR PANEL 252GF HAS 1EA 12" CRACK FABRICATED REPLACEMENT FLOOR PANEL 262GF IAW DWG SR2 25-005, REV J.Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107222906Floorboard · damagedFLOORBOARD 251GF HAS PUNCTURE. FABRICATED REPLACEMENT FLOORBOARD 251GF IAW DWG SRZ-25-005, REV J.Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107222905Floor Panel · crackedFLOOR PANEL 251WH HAS 12 IN CRACK FABRICATED REPLACEMENT PANEL 251WH IAW DWG SRZ-25-005, REV J.Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
Back to Airbus A310-203