Airbus A310-324
Service difficulty reports · 1,439
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 = 'A310324' 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 = 'A310324' 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 FDEA201703180949Aoa · malfunctionedDURING CLIMB THRU FL 340, PROBES & STAT ALPHA CONTROL CIRCUIT BREAKER TRIPPED. MULTIPLE PROBE HT FAILS. FOLLOWED ECAM & QRH PROCEDURES. ATS LEVER TRIPPED OFF IN SEQUENCE WITH THE NR 2 ENGINE LIGHT. R & R RELAY LT 213 IAW WDM 30-31-04. DURING OPS CHECK IAWSDR FDEA201703040774Line · leakingLOST ALL GREEN SYSTEM HYD FLUID LEAVING FL 320. USED LANDING GEAR GRAVITY EXTENTION PROCEDURE. HYD SYS CIRCUIT BREAKERS HAVE BEEN COLLARED IN E/E BAY. FOUND A PIN HOLE IN LT GREEN HYD RETURN LINE, REMOVED AND REPLACED THE LINE IAWSMP 20-23-11-00, & 20-23-12-SDR FDEA201702080461Girt Bar · detachedR1 DOOR WILL NOT ARM. FOUND GIRT BAR DETACHED NOT ALLOWING PROPER OPERATION REINSTALLED GIRT BAR IAW MM 25-61-22-04-01.SDR FDEA201701170209Jackscrew · fluid lossSLATS 1 AND 2 FAULTED OFF DURING SLATS EXTENSION. SLATS REMAINED AT THE RETRACT POSITION AND DID NOT MOVE WHEN THE HANDLE WAS RECYCLED. COMPLIED WITH QRH AND LANDED WITH SLATS RETRACTED AND FLAPS 40. FOUND RIGHT WING INBOARD JACKSCREW EMPTY OF FLUID, REMOSDR FDEA201701160199Computer · failedDURING APPROACH WHEN EXTENDING SLATS, NO MOVEMENT. CYCLED, RAN QRH, LANDED WITH SLATS UP AND FLAPS 40. REMOVED & REPLACED BOTH NR 1 & 2 SFCC'S IAW AMM 27-51-18-04 & BOTH OPS CHECKED GOOD IAW AMM 27-51-00-05.SDR FDEA201701050043Limit Switch · failedWHILE TROUBLE SHOOTING R1 DOOR ARMING PROBLEM, SLIDE TRIED TO DEPLOY. REMOVED AND REPLACED RI DOOR LIMIT SWITCH 14WN AND TESTED IAW AMM 52-73-13-04-09.SDR FDEA201701050045Switch · malfunctionedR1 SLIDE INDICATOR WAS BLINKING ON & OFF AT BLOCK IN PRIOR TO DISARMING. R & R THE R1 DOOR LIMIT SWITCH 14WN.SDR FDEA201701050044Slide · unknownDURING TROUBLESHOOTING OF THE R1 DOOR ARMING PROBLEM, THE SLIDE TRIED TO DEPLOY. COMPLIED WITH R1 SLIDE REMOVAL ONLY IAW EA 6-5210-T0330666 PART 1.SDR FDEA201612314582Relay · failedR1 SLIDE INDICATION FLASHES CONTINUOUSLY WHEN SLIDE IS ARMED ON RIGHT ECAM. RELEASED FOR SERVICE PER MEL 52-30-04. REMOVED AND REPLACED RELAYS 9ES AND 10ES REF ESPM 20-46-50. PERFORMED ADJUSTMENT TEST OF ESCAPE SLIDE WARNING REF MM 52-73-00-05. OPS CK OK OSDR FDEA201612134398Floor Support · corrodedMAIN DECK FRAMES 12A - 14, Y953 FLOOR SUPPORT FOUND CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201612134397Skin · dentedFUSELAGE SKIN FOUND A DENTED BETWEEN FRAMES 65 - 66, STRINGER 36 - 37R. REPAIRED IAW SRM 53-10-12- 201 PARA 6 FIG225 SHEET 2 . MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201612094367Angle · crackedFRAME 47 RT INTERNAL ANGLE\ FOUND CRACKED. REPAIRED THE ANGLE IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201612094366Angle · crackedANGLE AT FRAME 47 LT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201612094369Angle · crackedTEE ANGLE AT STIFFENER 8 RT FOUND CRACKED. REPAIRED IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201612094368Angle · crackedTEE ANGLE AT STIFFENER 8 LT FOUND CRACK. REPAIRED THE TEE ANGLE IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100SDR FDEA201612074345Attach Fitting · crackedAFT CARGO DOOR ACTUATOR ATTACH FITTING FOUND CRACK BY HFEC INSPECTION. REPLACED THE ATTACH FITTING IAW SRM 51-40-21.SDR FDEA201612074344Floor Support · corrodedMAIN DECK FR11-FR14 Y770 FLOOR SUPPORT CORRODED.SDR FDEA201612074343Attach Fitting · crackedFWD CARGO DOOR ACTUATOR ATTACH FITTING WITH CRACK SIGNAL. REPLACED THE ATTACH FITTING IAW SRM 51-40-21.SDR FDEA201612074342Skin · crackedLEFT WING BOTTOM SKIN FOUND CRACKED AT 581AB CUTOUT. REPAIRED IAW EA 6-5730-T0330205 P1 AND DWG R57249152. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201612064330Flap System · malfunctionedFLAPS STUCK AT 0 DURING APPROACH. COMPLIED WITH ECAM & QRH. NO RELIEF IN CYCLE. LANDED SLATS 30 FLAPS 0. TSM 27-50, BOTH SFCC'S INDICATE FLAP JAMB, LEFT FLAP SYSTEM TORQUE LIMITER TRIPPED. SRM 27-50-02 FIG 101 BLOCK 2, ALL SCREW JACK TORQUE LIMITERS INSPSDR FDEA201612034317Limit Switch · inoperativeAFTER PARKING, THE R1 DOOR SLIDE INDICATION WAS FLASHING. R & R THE DOOR LIMIT SWITCH IAW AMM 52-73-13-04-09 OPS CHECKED GOOD IAW 73-13-05-09.SDR FDEA201611274258Battery Pack · inoperativeDURING LANDING, SLIDE INDICATION ON ECAM FOR R1 WAS FLASHING. REMOVED AND REPLACED ASPU BATTERY NR 1 IAW AMM 52-73-18-04, ASPU BITE CHECKED GOOD. SLIDE INDICATION TEST CHECKED GOOD SEVERAL TIMES IAW AMM 52-73-00-5. ACFT OK FOR SERVICE.SDR FDEA201611224197Bottle · low pressureR1 DOOR SLIDE ARMED INDICATION FLASHING WHILE TAXING IN AFTER LANDING. RT DOOR DAMPER AND EMERGENCY OPERATING CYLINDER PRESSURE FOUND TO BE LOW. SERVICED CYLINDER IAW AMM 52-10-14-03-09. ARMED R1 DOOR, RECEIVED SLIDE INDICATION ON ECAM. CYCLED R1 DOOR ARMSDR FDEA201611194116Power Supply · malfunctionedCOULD NOT GET RT SLIDE TO ARM. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN AND BOTH BATTERIES ON ASPSU IAW AMM 52-73-18-04, BITE TEST OK. R1 DOOR SLIDE ECAM INDICATION OPS NORM. REMOVED PLACARD.SDR FDEA201611123995Warning Message · intermittentBOTH ECAM SLIDE INDICATIONS ARE INTERMITTENT. RESET EMERGENCY SLIDE SYSTEM AND PERFORMED OPS CHECK SEVERAL TIMES IAW AMM 52-73-13-04. OPS CHECKED GOOD.SDR FDEA201610263703Relay · failedAT FL 370 , THE NR 2 LEFT INNER PUMP FAULTED. PUMP FAULTED AND STRONG ACRED ODOR IN THE COCKPIT AND THE AVIONICS COMPARTMENT, ON DESCENT THE REMAINING THREE INNER PUMPS FAULTED AND FUEL FEED RESORTED TO OUTER TANK TO ENGINE. ACCESSED THROUGH THE COCKPITSDR FDEA201609273375Indication Sys · faultyINFORMATION ONLY, REJECTED T/O 9L, PARKING BRAKE SET INDICATION, WE NEVER SET PARKING BRAKE. ONCE WE STARTED TAXI TO RUNWAY, CHECKED HANDLE DOWN POSITION, WE HAD NORMAL CONFIGURATION ON BELOW THE LINE CHECK LIST, PERFORMED RTO, SPEED BELOW 60 KTS, CLEARED RUNSDR FDEA201609153243Coalescer Bag · odorAFTER PARKING, THE AVIONICS SMOKE WARNING SOUNDED. PULLED CIRCUIT BREAKERS, TURNED ON OVERRIDE NR 1 AND 2 AND OPEN THE AVIONICS HATCH, SMELLED SMOKE. POWERED DOWN THE AIRCRAFT AND EVACUATED. R & R LT AND RT COALESCER BAGS IAW AMM 21-51-16-04. AFTER ENGINESDR FDEA201609133211Slat · lack of lubeDURING APPROACH, SLATS WOULD NOT EXTEND, COMPLIED WITH PHASE 1, ECAM & QRH - SLATS CONFIRMED STUCK. DID NO SLAT/FULL FLAP LANDING IAW QRH. CREW CALLED IN FIRETRUCKS FOR SAFETY PRECAUTION. ACCOMPLISHED SFCC 1 AND 2 BITE TEST IAW AMM TSM 27-80-00 FOUND SFCCSDR FDEA201607192536Smoke Detector · faulty"AVIONICS SMOKE" DISPLAYED ON ELECTRICAL PANEL AFTER ENGINE SHUTDOWN AT GATE. NO SMOKE WAS EMITTED ON THE SNIFFER FAN. R & R SMOKE DETECTOR.SDR FDEA201606131980Computer · faultyAPPROX 60 NM FROM DESTINATION, GOT FUEL ADV ON ECAM. LT OUTER 6K, LT INNER 11.0, CTR WAS 0, TRIM TANK WAS 0, RT INNER STARTED AT 11, THEN 10, THEN 9, THEN 8, ALL THE WAY TO ZERO. RIGHT WAS 4.0 AND DECREASING. DIVERTED. WITH T/O OF 57, FUEL USED COUNTER WASSDR FDEA201605021440Windshield · crackedDURING CRUISE FLIGHT AT FL 360, BEGAN TO SEE AN ORANGE GLOW IN LOWER LT CORNER OF CAPTAINS FWD WIND SCREEN. TURNED OUT TO BE WINDSHIELD HEAT ARCING, SO TURNED OFF CAPTAINS WINDSHIELD HEAT. ABOUT THE SAME TIME, CAPTAINS FWD, OUTER WINDSHIELD SHATTERED. REMOVSDR FDEA201603100888Gcu · malfunctionedREJECTED TAKE OFF AT 90 KNOTS, AC BUS 2 OFF, GEN 2 FAULT. PERFORMED BITE CHECK ON GND POWER CONTROL UNIT & FOUND, RT GEN POWER SYS, FAULTED. R & R NR 2 GEN CONTROL UNIT IAW AMM 24-22-12-04. RAN NR 2 ENG IAW JRH WITH NO FAULTS NOTED. ALSO PERFORMED ADJUSTMESDR FDEA201602150560Skin Panel · corrodedCORROSION ON UPPER RT WING SKIN, APPROX 83.5" FROM WTB. CORROSION FORMED AROUND FASTENER HEAD & EXTENDS AFT, APPROX 2"X4". REMOVED VISIBLE CORROSION ON RT WING UPPER SKIN IAW SRM 51-74-10. CHECKED LIMITS BLEND AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 57-2SDR FDEA201602120510Sequence Valve · faultyRIGHT MLG DID NOT EXTEND DURING NORMAL EXTENSION. GEAR EXTENDED TO DOWN & LOCKED WITH MANUAL EXTENSION. FREE FALL EXTENSION SYS RETURNED TO NORMAL CONDITION IAW AMM 32-33-00-2. INSPECTED MAIN LG DOOR & WW AREA & NO DEFECT FOUND. JACKED UP ACFT IAW AMM 07-1SDR FDEA201602030435Sensor · failedDUAL SLATS FAULT 1 & 2 ON APPROACH, 3000' MSL 170 KTS, FLAPS STUCK AT 15'. R & R SLAT COMMAND SENSOR UNIT 51CV IAW AMM 27-51-17-04. R & R BOTH SFCC'S IAW AMM 27-51-18-04. FLAP & SLATS OPERATION TESTED GOOD IAW AMM 27-81-00-05. ALSO REF TSM 27-80-07.SDR FDEA201601240289Windshield · crackedCRACK ON CAPTAINS' OUTER FRONT WINDSHIELD. WINDOW HEAT WAS ON, BUT TURNED OFF ONCE CRACK DEVELOPED. R & R CAPTAINS WINDSHIELD. R & R LT WINDOW TEMP CONTROLLER -19DG. R & R LT WINDOW HEATING PROTECTION UNIT -87DG.SDR FDEA201601200234Gcu · failedON TAKEOFF AT 80 KNOTS GEN II FAILED, THEN FOLLOWED BY GEN 1, TOTAL ELEC FAILURE. REJECTED TAKEOFF, CLEARED RUNWAY & RAN QRH. REJECTED AT 100 KNOTS. INTERROGATED GPCU & FPUND BOTH 1 & 2, GCU FAILED. R & R BOTH GCU'S IAW MM 24-22-12-04. RAN BOTH ENGS IAW SDR FDEA201601130138Skin · delaminatedRIGHT SIDE RUDDER PANEL, FOUND DELAMINATED AT TE RR 48 - RR 49, APPROX 6" X 6". REMOVE THE OUTER SKIN IN THE DAMAGED AREA IAW SRM 55-41-12 PARA 31. PERFORM A TAP TEST AROUND THE DAMAGE AREA TO MAKE SURE NO DELAMINATION IAW NTM 51-10-19, NO DAMAGE. PERFORM SDR FDEA201601120125Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 60 WITH CRACK SIGNAL, RT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR SDR FDEA201601120124Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 62 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201601120123Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 60 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR ISDR FDEA201601120122Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 46 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR ISDR FDEA201601120121Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 41 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IASDR FDEA201601120120Fitting · crackedCENTER WING INSPECTION, REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 31 WITH CRACK SIGNAL, LT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR ISDR FDEA201601120119Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 14 WITH CRACK SIGNAL, RT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201601120118Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 62 WITH CRACK SIGNAL, RT SIDE. REPAIRED IAW EA 6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED FASTENER IAW EA 6-5710-T0322510. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201601120117Fitting · crackedCENTER WING INSPECTION REAR SPAR INTERNAL ANGLES & TEE FITTING, HOLE NR 61 WITH CRACK SIGNAL, RT SIDE. REPAIRED THE CRACKED HOLE IAW EA6-5710-T0322510. NDT CHECK, NO CRACK FOUND. WET INSTALLED THE BUSHES, WASHER & FASTENER IAW EA 6-5710-T0322510. THIS IS ASDR FDEA201601050025Selector Valve · malfunctionedAFTER TAKEOFF, LG RETRACTION FAULT SYS NR 1, GEAR REMAINED DOWN. RETURNED FOR LAND. CANNOT OPEN THE LT LG DOOR ON GND. RT LG DOOR OPENED OK ON GND. R&R LG NORMAL CONTROL MICROSWITCH UNIT 2GA PER AMM 32-31-11-04. R&R LANDING GEAR SELECTOR VALVE 3GA PER AMMSDR FDEA201601040021Stringer · corrodedAFT CARGO BAY STRINGER 54R, FOUND CORRODED BETWEEN FRAMES 59 - 63. REPAIR THE STRINGER IAW SRM 53-10-14-201 FIG 201 VIEW F & G. MAJOR REPAIR IAW GMM 6-2-100.
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