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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201206022056Skin · misrepairedSKIN MISREPAIRED, REPAIRED IAW SRM 53-10-12, FIG 225, SHEET 1, PAGES 357 TO 362. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201206022061Floor Support · misrepairedFLOOR SUPPORT LONGERON 3L BETWEEN FRAMES 12A TO 15A MISREPAIRED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-72-10. REPAIR IS A MAJOR IAW GMM 6-2-100.SDR FDEA201206022060Seat Track · misrepairedSEAT TRACK 5L Y1959 BETWEEN FRAMES 15A TO 17 MISREPAIRED. R & R SEAT TRACK IAW SRM 51-72-10, PAGES 1 TO 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201206022062Floor Support · misrepairedFLOOR SUPPORT MISREPAIRED. REMOVED FLOOR SUPPORT ASSY AND INSTALLED NEW IAW SRM 51-72-10 PAGES 1 TO 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201206022059Floorbeam · misrepairedFLOORBEAM MISREPAIRED. REPAIRED PER SRM 53-10-15 FIG 203 SHEETS 1-2 PG'S 245-252.SDR FDEA201206022055Skin · failedSKIN AT FRAMES 35 TO 36 & BETWEEN STRINGERS 54 LT TO 54 RT MISREPAIRED. REPAIRED SKIN WITH NEW DOUBLER IAW SRM 53-10-12, FIG 225, SHEET 1, PAGES 357 TO 362.SDR FDEA201206012050Floor Panel · crackedFLOOR PANEL 231CF HAS 28 INCHES OF CHAFFING SKIN & A 7 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201206012049Floor Panel · chafedFLOOR PANEL 231EF HAS THIRTY TWO SQUARE INCHES OF CHAFFING ON UPPER SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201206012047Floor Panel · crackedFLOOR PANEL 252WH HAS ONE, NINE INCH CRACK, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV JSDR FDEA201206012046Floor Panel · crackedFLOOR PANEL 252PH HAS ONE, TEN INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201206012045Floor Panel · damagedFLOOR PANEL 251RT BROKEN ACROSS ENTIRE MID-SECTION OF PANEL FABRICATED. REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201205292006Floor Panel · delaminatedFORWARD CARGO COMPARTMENT FLOOR PANEL 131ZF HAS FOUR AREAS OF DELAMINATION ON EDGES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201205292005Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL 131QF HAS PUNCTURE ALONG AT TIRE EDGE (BACK SIDE). FABRICATEDED FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201203311201Pressure Switch · failedNR 2 ENGINE FUEL FILTER CLOG ECAM/ MASTER CAUTION IMMEDIATELY AFTER TAKE OFF. ECAM CAUTION EXTINGUISHED AROUND 80 PERCENT N1 WHEN THROTTLES RETARDED. REMOVED AND INSPECTED NR 2 ENGINE FUEL FILTER. NO DEBRIS FOUND. INSTALLED NEW FILTER IAW MM 73-12-03-02.SDR FDEA201203130923Computer · inoperativeFLAP SYS 1 FAULT LIGHT IN FLIGHT RELEASED FOR SERVICE IAW MEL: 27-51-01-01 CATEGORY: C, "MEL 27-51-01-01: NR 2 SLATS/ FLAPS CONTROL COMPUTER - INOP. SLAT/FLAP WING TIP BRAKE TEST HAS BEEN ACCOMPLISHED." SFCC PN 49-079-05 (SYS NR 1) GOOD. SFCC PN 49-079-05 SDR FDEA201203130922Handle · dirtyFLAP/SLAT HANDLE FAILED TO MOVE PAST 15/0 SETTING ON RETRACTION AND 20/20 SETTING ON LANDING. T/S SFCC FAULTED SUPPLY PSW. PARTS ID ARE FOR T/S, ADDITIONAL PARTS MAY BE REQUIRED. HIGH PRESS SW. REMOVED FLAP/SLAT HANDLE, CLEANED SPRING AND RE-ASSEMBLE. OPSDR FDEA201202070508Pin · misinstalledAFTER TAKEOFF, FLAP LEVER WOULD NOT RETRACT BEYOND 15/0 POSITION. LEVER WOULD NOT DROP DOWN INTO GATE. SLAT/FLAP POSITION REMAINED AT 15/15. ON APPROACH, FLAPS CAME TO 20/20, BUT LEVER WOULD NOT GO INTO 30/40 POSITION. CHECKED UNDER CENTER PEDESTAL FOR DESDR FDEA201201130164Skin · failedR1 DOOR AFT EXTERNAL SKIN PANEL REQUIRES REMOVAL TO SUPPORT FRAME 16A REPAIR. SKIN PANEL TO BE REPLACED AFTER FRAME 16A REPAIR. R & R R1 AFT EXTERNAL SKIN PANEL IAW SRM 51-72-10, 51-40-21 AND 51-40-44.SDR FDEA201201110098Failsafe · failedR1 DOOR FAILSAFE RING REQUIRES REMOVAL TO FOM FARME 16A RT FRAME REPAIR. REMOVED FAIL SAFE RING IAW SRM 51-40-21 AND EA 6-5310-135257B. LOCATED AND DRILLED NEW FAIL SAFE RING AT R1 DOOR IAW DWG 12R53610899 AND SRM 51-40-44. INSTALLED NEW FAIL SAFE RING AT R1SDR FDEA201201050027Frame · damagedFRAME 16A RT DAMAED. REMOVED FRAME IAW SRM 51-40-21, PG 1 AND EA 6-5310-135257B. LOCATED AND DRILLED NEW FRAME IAW SRM 51-40-44, PG 9. INSTALLED NEW FRAME IAW SRM 51-40-21, PG 19 AND EA 6-5310-135257B, STEP 18, PG 4.SDR FDEA201201050026Depressor · damagedR1 DOOR FRAME 16A SEAL DEPRESSOR DAMAGED FRAME 16A. REPAIR REMOVED SEAL DEPRESSOR IAW SRM 51-72-10. LOCATED AND DRILLED NEW SEAL DEPRESSOR IAW A310 51-40-44. INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-40-21 AND 51-72-10.SDR FDEA201111225002Duct · leakingDURING CLIMB ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. REMOVED AND REPLACED NR 1 SYS ANTI-ICE DUCT IN PYLON PER AMM 20-26-00-000. PERFORMED LEAK CHECK WITH APU AIR, FOUND NO LEAKS AT DUCT. ACFT OK FOR SERVICESDR FDEA201111225003Warning Light · illuminatedDURING CLIMB, ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK, COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. OPENSDR FDEA201111164941Flap System · stickingON CLIMB OUT, AFTER SLATS RETRACT, KRUGER FLAP DID NOT RETRACT. RE-CYCLED AND KRUGER WOULD NOT RETRACT. ACCOMPLISHED CHECKLIST AND RETURNED TO DEPARTURE. BITE TESTED SFCC 1. FAULTED LT RETRACT SWITCH. FOUND LT RETRACT SWITCH TO BE STICKING FREED STUCK SWSDR FDEA201109213999Actuator · failedFAILURE OF THE MLG DOOR ACTUATOR AS NOTED ON EA 6-5310-145668. R & R RT MLG DOOR FITTING AND ACTUATOR IAW EA 6-5310-145668. REF N00005 AND N00010 FOR ALL WORK PERFORMED.SDR FDEA201109203977Support Bracket · crackedOFF ACFT PART, RT KEELBEAM AT FR 61, HYD LINE SUPPORT BRACKET CRACKED FROM HOLE TO CORNER 1 IN LONG VERIFIED MATERIAL, FABBED BRACKET IAW DWG A534100616, HEAT TREATED IAW SRM 51-25-00, ROCKWELL TESTED IAW SRM 51-28-10, CONDUCTIVITY TESTED IAW NTM 51-10-17, ASDR FDEA201109063710Skin · misrepairedSKIN AT R1 PASSENGER DOOR LOWER AT FS 1187 FRAME 14A. MISREPAIRED. REPAIR CARRIED OUT AS PER E.A. 6-5210-143668, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.SDR FDEA201109013620Floorboard · delaminatedKEELBEAM IN WHEEL WELL HAS FLOORBOARD 147AF HAS 5 SQ IN APPROX DELAMINATION ON EDGE FABRICATED FLOORBOARD 147AF IAW DWG SRZ 25-005, REV J MAJOR REPAIR IAW GMM6-2-000.SDR FDEA201108263514Floor Panel · brokenFORWARD CARGO FLOOR PANEL 132YF FOUND BROKEN. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-10-29 REV.30 FLOOR PANEL FABRICATED AS PER DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201108263492Support Fitting · crackedRT WING NR 2 FLAP TRACK FORWARD FIXED FAIRING FORWARD SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-40-21 REV 79. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.SDR FDEA201108263491Support Fitting · brokenRT WING NR 3 FLAP TRACK FORWARD FIXED FAIRING FWD SUPPORT FITTING BROKEN. REMOVED AND REPLACED AS PER SRM 51-40-21 REV 79. FUEL LEAK CHECK CARRIED OUT AS PER AMM 28-11-00-05-0 REV 30. FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.SDR FDEA201108263513Floor Panel · damagedMAIN DECK CARGO COMPARTMENT BETWEEN FRAME 53 AND FRAME 54 RT OTBD FLOOR PANEL FOUND DAMAGED. FABRICATED FLOOR PANEL PER DWG SRZ 35-005 REV J AND INSTALLED AS PER AMM 53-10-25 REV 30. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108253468Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AND FOUND RT WING REAR SPAR LOWER CHORD NEAR RIB 1 HAS A CRACKED INDICATION. RT WING REAR SPAR REAMED TO DIAMETER 0.560" IAW EO 6-5710-7-3322 PART 1, WORK STEP 4.G. HIGH FREQUENCY EDDY CURRENT INSPECTION CARRSDR FDEA201108253467Spar · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT AND FOUND HOLE ITEM 29 ON RT WING REAR SPAR, NEAR RIB 1 WITH CRACK INDICATION. RT WING REAR SPAR CRACKED FASTENER HOLE REAMED TO DIAMETER 0.560 INCH IAW EO 6-5710-7-3322, PART 1, WORK STEP 4G. HIGH FREQSDR FDEA201108253471Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LT WING REAR SPAR AND FOUND DAMAGE. REPAIRED IAW EO 6-5710-7-3322 B1 PT 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV112.SDR FDEA201108253470Spar · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LT CENTER TANK REAR SPAR AND FOUND DAMAGED AT APPROX 6 O`CLOCK. REPAIRED IAW EO 6-5710-7-3322B1 PT 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV112.SDR FDEA201108253484Skin · crackedEVIDENCE OF FUSELAGE SKIN CRACK UNDER LAV SERVICE DOOR. REPAIRED IAW RDAS ISSUE A AND EA 6-5330-154038 PARTS 1 AND 2.SDR FDEA201108243464Bellcrank · failedDURING LANDING GEAR FREE FALL EXTENTION TEST PROCEDURES, THE LT AND RT MLG FAILED TO EXTEND AFTER HANDLE REACHED MAXIMUM ALLOWABLE TURNS OF 20.5. REMOVED AND REINSTALLED FLOOR PANELS FOR ACCESS IAW AMM 53-23-04. R & R FREE FALL CONTROL BELL CRANK IAW SRM 51-SDR FDEA201108243463Skin · corrodedCENTER WING BOX LT FR 49 HAS OXIDATION AT UPPER SURFACE BETWEEN STR 27-28. BELOW SEAT TRACK 6L DEFECT MEASURES 8 SQ INCHED IN THE CORNER. CLEANED UPPER SURFACE OF CWT BOX FR 49 STR 27-28 AT ST 6L IAW SRM 51-74-10. R & R FASTENER IAW SRM 51-40-21. REMOVED ASDR FDEA201108243458Attach Fitting · corrodedCTR WING BOX BETWEEN SEAT TRACK L5-L6 HYD LINES ATTACHMENT FITTING CORRODED FR 49-50. CLEANED 6 EA LINES AND FITTING FOUND TO BE OUT OF LIMIT IAW AMM 12-21-12-02 R & R 6EA FITTING IAW 51-40-10 PRESSURE AND LEAK CK SATISFACTORY IAW AMM29 10-00-04.SDR FDEA201108233411Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT. LOWER FORWARD DOOR CUTOUT FOUND DAMAGED. REPAIRED IAW EO 6-5310-7-3318, PT 17. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.SDR FDEA201108233414Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON CREW DOOR CUTOUT & FOUND DAMAGED. REPAIRED IAW EO 6-5310-7-3318 PT 15. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.SDR FDEA201108233412Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON SKIN & FOUND DAMAGED. REPAIRED IAW EO 6-5310-7-3318 PT 15. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.SDR FDEA201108233410Skin · damagedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT ON RT AFT CREW DOOR. UPPER FORWARD CUTOUT FOUND DAMAGED. REPAIRED PER EO#6-5310-7-3318 PT 18 STEP 8. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.SDR FDEA201108193388Panel · corrodedRT ELEVATOR, L/E PANEL 345DT, OTBD LANDING HAS 1 EA CORRODED FASTNER HOLE, 2EA MISDRILLED HOLES, AND CORROSION ON THE WEB ATTACHMENT STRAP. REMOVED LEVEL 1 CORROSION AT RT ELEVATOR L/E PANEL FASTNER HOLE AND WEB ATTACHMENT STRAP IAW SRM 51-74-10, PAGE 204. FSDR FDEA201108183365Skin · gougedRT WING FIX L/E IS GOUGED APPROX 6" LONG BETWEEN SLAT TRACK 5 AND 6, FROM CONTACT WITH NR 2 SLAT LOWER SKIN FASTENERS. SMOOTHED AND BLENDED AREA IAW SRM 51-75-10 AT RT WING FIX L/E SLAT TRACK 5 AND 6. NDT FOR CRACK AND LIMITS, NO LIMIT REMAINING THICKNESS.SDR FDEA201108183356Skin · gougedRT HORIZONTAL STAB L/E PANEL 341AB, EXTERNAL SKIN SCRATCHED AND GOUGED, ENTIRE LENGTH OF INBD EDGE. BLENDED OUT AREAS (4EA) ON RT HORIZONTAL STAB L/E PANEL 341AB EXTERNAL SKIN IAW SRM 51-73-10; CHECKED LIMITS FOUND AREAS (3EA) WITHIN LIMITS, 1 AREA OUT OF LSDR FDEA201108173304Floorbeam · crackedFORWARD CARGO COMPARTMENT MAIN DECK FLOORBEAM AT FRAME 36, RBL 27 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-15 FIG.203 SHT 1 REV. 18 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108173303Attach Fitting · corrodedLT WING RIB 5 FWD LUG BORE DIAMETER HAS CORROSION THAT HAS EXCEEDED MAX ALLOWABLE REWORK DIMENSIONS "4.8405 IN". REMOVED LEVEL 1 CORROSION FROM LT WING RIB 5 BY OVERSIZING THE BORE AND SPOT FACING THE AFT LUG FACE, NDT INSPECTED (NIL FINDING) INCLUDED ACID SDR FDEA201108163289Adapter · crackedCLEVIS ADAPTER AT FR 46 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX.2" LONG AT FWD & AFT FLANGE. R & R CLEVIS ADAPTER AT FR 46, BETWEEN TRACKS 2R AND 3R IAW SRM 51-72-10, PG. 1-3.
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