Airbus A340-313
Service difficulty reports · 74
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 = 'A340313' 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 = 'A340313' 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 CA090403001Release Pin · failed(CAN) DURING OPS TEST OF THE SLIDE/RAFT DEPLOYMENT, WITH THE EMERGENCY CONTROL HANDLE OF THE DOOR IN ARMED POSITION, DOOR HANDLE WAS LIFTED UP, THE DOOR STARTED TO OPEN WHEN THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FIRED. HOWEVER, DOOR FAILED TO OPEN FSDR CA070528008Sensor · inoperative(CAN) NR 2 ENGINE OIL TEMPERATURE HIGH, 30 MILES FROM AIRPORT, ENGINE SHUTDOWN IAW QRH PROCEDURES, AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE OIL TEMP SENSOR AND FUEL RETURN VALVE REPLACED, NO SUBSEQUENT FAULTS AFTER PARTS CHANGED. (TC NR 20070528008)SDR CA061208005Compressor · stalled(CAN) IN CRUISE, 2 HOURS FROM DESTINATION THE ENGINE STALLED AND EGT WAS RISING. WHEN EGT REACHED 1010 DEG. C, THE ENGINE WAS SHUTDOWN. THE OIL PRESSURE WENT TO ZERO AND BOTH N1 AND N2 ROTORS WERE ROTATING. DFDR DATA SHOWS: N2 VIBRATION WAS HIGH (3.5 TO 5.5 SDR CA061005005Ecu · failed(CAN) DEPARTURE AND ENROUTE TO DESTINATION, NR 2 ENGINE PARAMETERS ERRATIC, THEN INDICATE THAT NR 2 EGT OVER LIMITS, THEN VIBRATION. ENGINE SHUTDOWN AND BOTTLE DISCHARGED. REPLACED ECU IAW MM, RT VSV ACTUATOR REPLACED. FADEC MOTORING CHK ACCOMPLISHED IAW MM,SDR CA060725001Switch · burned(CAN) WHILE ENROUTE, ON A POLAR ROUTE IN THE MIDDLE OF HUDSON BAY, THE FLIGHT CREW REPORTED ACRID SMOKE COMING OUT OF OVERHEAD PANEL IN THE AREA OF THE TERRAIN SWITCH AND THE FAILURE OF THE GPWS. THE SMOKE THEN DISSIPATED. THE CREW DECLARED A PAN PAN (URGENCSDR CA060511002Manifold · crackedAIRCRAFT HAD 22 MANIFOLDS FOUND CRACKED. LOOKED AT ANOTHER AIRCRAFT TO PROVIDE SPARES, BUT FOUND MOST OF ITS MANIFOLDS CRACKED TOO. DRAGER (VENDOR) CONTACTED, AND WILL PROVIDE REPLACEMENTS. MANIFOLD IS MADE OF A VARIETY OF PLASTIC, WHICH IS BRITTLE.SDR CA060404003Video Display · burned4H VIDEO MACHINE GOT REALLY HOT AND SMELLED BURNED AT THE END OF FLIGHT. THICK WHITE SMOKE CAME FROM PTV. FOUND PTV OPERATION SERV. FOUND SEAT PWR SUPPLY U/S AND ODOR OF SMOKE. DEACTIVATED BY PULLING AND COLLERING C/B.SDR CA060214002Lock · malfunctioned(CAN) THRUST REVERSER NR 4 UNLOCKED. SHUTDOWN NR4 V/S ON OVERWEIGHT LANDING 500FT/MIN LANDING WT 233000 KG. SEE FMR M1243972. ACTION:411T/S 78-31-00-810-970 CARRIED OUT NO FAULT FOUND. SUSPECT PRIMARY LOCK P/N 2885000-9 LOCATED AT IB UPPER SIDE. 4 LOCK PLUGSDR CA050727002Yaw Damper · leakingIN CRUISE, YELLOW HYD SYSTEM LEAK TURNED OFF ENG GREEN PUMPS 1 & 2. NO NOSE STEERING ON LANDING. FOUND HYD LEAK IN THS COMPT YAW DAMPER ACTUATOR 19CS1. REPLACED AS PER J/C 9-227L-01.SDR CA050516003Tire · deflatedPREMATURE FAILURE OF NR 2 TIRE OF A/C 902 ON LANDING IN YVR MAY 01,2005 FROM FLIGHT 850 FROM HKG. NR 2 TIRE WAS FOUND DEFLATED. MAIN WHEEL REPLACED ON A/C 902 IAW 32-41-11-400.SDR CA050509004Light · burned(CAN) APPRO 15 AFTER TAKEOFF, PURSER REPORTED SMOKE IN R1 GALLEY AREA, SMOKE INCREASED. GALLEY C/B'S PULLED, ELECT SMOKE, CARRIED OUT AND FLIGHT RETURNED TO DEPARTURE. OVERWEIGHT LANDING CARRIED OUT. FOUND R1 DOOR F/A READING LT ASSY BURNED. INSPECTION CASDR CA041214009Antenna · damaged(CAN) ON ND. SYSTEM RETURNED TO NORMAL BUT GIVEN HISTORY, RETURNED HNL. ANTENNA. COULD BE FELT AND HEARD CLUNKING. REPLACED WX RADAR ANTENNA AS PER W/C 34-41-11-000-801-862-050. REPLD BOTH RADART/R UNITS AS PER W/C 34-41-313-400. RADAR ANT 34-40-0247 OFF FTN 6SDR CA041214008Antenna · damaged(CAN) ON ND. SYSTEM RETURNED TO NORMAL BUT GIVEN HISTORY, RETURNED HNL. ANT. COULD BE FELT AND HEARD CLUNKING. REPLACED WX RADAR ANT IAW W/C 34-41-11-000-801-862-050. REPLACED BOTH RADAR T/R UNITS IAW W/C 34-41-313-400. RADAR ANTENNA 34-40-0247 OFF FTN 639J4G SDR CA040614002Engine · fod(CAN) APPROX 30 MINS FROM DEPARTURE, NR 4 ENG EGT OVERTEMPED AND CLIMBED TO 946 DEGREES AND WAS SHUT DOWN. THERE WAS NO LOUD NOISE OR SHAKING. THE AC MADE A NORMAL LANDING AND THE CFR WERE NOT CALLED OUT. AC REMOVED FROM SERVICE AND CP CONTACTED TO CARRY OSDR CA040225017Sensor · malfunctioned(CAN) AFTER TAKE OFF ABOUT 100 FOOT ABOVE GROUND LEVEL FLAPS LOCK ECAM MESSAGES, TRIED RESET , NIL FIX, RETURN TO GATE. RESET OF THE COMPUTER SLAT FLAP COMPUTERS ON GROUND FIXED THE PROBLEM BUT SAME THING HAPPENNED ON THE SECOND ATTEMPT. AIRCRAFT UNDER INVESTISDR CA040218005Thrust Reverser · inoperative(CAN) SHORTLY AFTER T/O ROTATION ECAM ENG. NR 1 REV. UNLOCKED. NO BUFFET EXPERIENCED. JETTISONED FUEL AFTER ECAM AND RETURNED TO LAND, OVERWEIGHT 229,000, VERTICAL SPEED AT TOUCHDOWN ESTIMATED APPROX 300/FTM. THRUST REVERSER PLACED UNDER MEL 78-30-01. IAW RESDR CA040113005Safety Valve · inoperative(CAN) ON APPROACH, GEAR DID NOT EXTEND NORMALLY ON FIRST ATTEMPT, SECOND ATTEMPT HAD SAME RESULT. CREW ELECTED TO CARRY OUT GO AROUND. LANDING GEAR CONTROL LEVER REPLACED AND TESTED IAW MM 32-31-11-400, MLG ISOLATION SAFETY VALVE (85GA) REPLACED IAW MM 32-31-1SDR CA040113001Selector · malfunctioned(CAN) SELECTED GEAR DOWN AND NOTHING HAPPENED FOR AT LEAST A MINUTE, THEN WIGGLED HANDLE THEN THE GEAR CAME DOWN. NOTE: AC SENT TO HANGAR FOR TROUBLE/SHOOTING.SDR CA031113009Engine · malfunctioned(CAN) ON FLT FROM YYZ TO DELLI, 3HRS INTO FLT, NR 4 ENG ROLLED BACK TO 75 PERCENT N1 THEN RECOVERED APROX 1,500 NM FROM DESTINATION. LATER ENG OIL FILTER CLOGGED LT CAME ON THEN ENG REDUCED TO 67 PERCENT FOR REST OF FLT. DURING DESCENT NR 4 ENG SHUTDOWN. ENGISDR CA030826006Engine · overheated(CAN) CLIMBING THROUGH FL130, NR 4 ENGINE STALLED AND HIGH TEMPS. A/C RETURNED HNL WITH ENG SHUT DOWN AND FIRE BOTTLES BLOWN. ENG HAD 17,536 HRS SINCE SHOP VISIT AND 2,068 CYCLES SINCE SHOP VISITSDR CA030820001Wheel · failed(CAN) AFTER TAKE OFF UNABLE TO CLOSE GEAR DOOR TO CLOSE AIRCRAFT RETURN TO GATE, FOUND BOTH CENTER GEAR WHEEL AT RIM, CENTER GEAR DOORS DAMAGEDSDR CA030611003Thrust Reverser · cracked(CAN) OPERATOR HAS IDENTIFIED CRACKS IN BOTH THE NR 3 AND 4 IN-BOARD THRUST REVERSER HALF, J-RINGS, ON AIRCRAFT 904. THE CRACKS ARE THE SUBJECT OF AD 2003-108 (B), BUT OPERATOR HAS NOT COMMENCED THE AD INSPECTION AS IT IS ONLY DUE BEFORE 6666 FC OR WITHIN 216SDR CA020315005Line · leaking(CAN) AFTER TAKEOFF, DURING FLAP RETACTION ECAM MSG HYDRAULIC BLUE ENGINE PUMP PRESSURE LOW CAME ON INTERMITTENTLY. AIRCRAFT RETURNED TO VANCOUVER. FOUND NR 2 ENGINE RETURN LINE LEAKING FROM A CRACK ELBOW. LINE REPLACED AND LEAK CHECKED OK. ALL FILTERS AND ENGSDR CA020121005Engine · failed(CAN) ENGINE SHUT DOWN. WHILE IN CRUISE NR 1 ENGINE SURGED FOLLOWED BY GRADUAL INCREASE IN EGT AND FUEL FLOW. SHORTLY AFTER, ENGINE FILTER CLOG MESSAGE DISPLAYED AND THEN ENGINE LOW OIL PRESSURE.FOUND EVIDENCE OF NR 4 BEARING FAILURE. REPLACED ENGINE.RESULT SDR CA020104015Control Unit · failed(CAN) MISSED APPROACH IN HONG KONG DUE TO FLAP PROBLEM. AIRCRAFT DID A FLAPLESS LANDING CLASS 1 F/CONTROL FLAPS FAULT-ECAM COMPLETED, RECYCLED. FLAPS INSPECTED AND FOUND RT SYSTEM TORQUE LIMITER 5081 CV AND RT INPUT GEARBOX TORQUE LIMITER 5120 CV POPPED. BOTSDR CA020104018Seal · leaking(CAN) APPROX. 1 HOUR AFTER TAKE OFF, NR 3 OIL QUANTITY INDICATED AMBER, NR 3 OIL PRESSURE WENT INTO RED (6PSI) ACCOMPANIED BY ECAM ADVISING TO SHUT DOWN ENGINE. AIRCRAFT RETURNED TO VANCOUVER. FOUND NR 3 ENGINE STARTER DRIVE SEAL LEAKING. SEAL REPLACED AND GRSDR CA011127015Engine · failed(CAN) ENROUTE FROM VANCOUVER TO JAPAN, THE FLIGHT EXPERIENCED A POWER LOSS ON NR 3 ENGINE. ROLL BACK TO 77 PERCENT THEN AUTO RE LIGHT OCCURRED RAPIDLY. LATER ON INTO THE FLIGHT, THE FLIGHT CREW HAD THE ENGINE LOW PRESSURE MESSAGE AND ON APPROACH TO NARITA, THSDR CA011127014Limiter · failed(CAN) AIRCRAFT LANDED WITH FLAP LOCKED IN THE RETRACT POSITION. AIRCRAFT DID OVERSHOOT, THEN EXECUTED A FLAPLESS LANDING. RT SYSTEM TORQUE LIMITER AND INPUT GEARBOXES 2-5 FOUND EXTENDED.SDR CA011114013Gearbox · failed(CAN) ON APPROACH, FLAPS 2 SELECTED, FLAPS DID NOT EXTEND. AIRCRAFT WENT AROUND AND LANDED FLAPLESS AND SLATS EXTENDED.FLIGHT CONTROL FLAPS FAULT MESSAGE. AFTER INVESTIGATION FOUND THE TORQUE LIMITERS EXTENDED FOR THE ROTARY ACTUATOR AND THE INPUT GEARBOX. SDR CA010814005Actuator · failed(CAN) ON MAINTENANCE CHECK FOUND TRIM HORIZONTAL STABILIZER ACTUATOR BALLNUT TRANSFER TUBE DISCONNECTED FROM BALLNUT. REPLACED TRIM HORIZONTAL STABILIZER ACTUATOR AND SYSTEM TESTED.SDR CA010430012Seal · faulty(CAN) CENTER RIGHT END LANDING GEAR DOOR WARNING MESSAGE SHOWING THE DOOR NOT CLOSED.DOOR UPLOCK AND DOOR ACTUATOR CHANGED WITHOUT ANY SUCCESS. FOUND TO BE THE DOOR ZONE 2 SEALS AT FAULT.REPOSITION OF THE NR 2 SEALS LT AND RT, GEAR SWING CARRIED OUT AND CHECK SDR CA010115007Warning System · activated(CAN) ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE FLIGHT CONTROL FLAP FAULT DURING LANDING.FLAPLESS LANDING. SYSTEM RESET, FLAPS NR1 & NR2 RESET AND OPERATION CHECKED CARRIED OUT, SERVICEABLE.SDR CA001110020Engine · failed(CAN) LOUD RUMBLING NOISE WITH CORRESPONDING DECREASE IN POWER, ON NR 2 ENGINE RAPID INCREASE IN EXHAUST GAS TEMPERATURE, FOLLOWED BY VIBRATION. ENGINE WAS SHUT DOWN. SUSPECT ENGINE BEARING FAILURE. ENGINE CHANGED. ADDITIONAL INFORMATION WILL FOLLOW AFTER INVSDR CA001110015Unknown · odor(CAN) ON CLIMB OUT FROM TORONTO ACRID ELECTRICAL SMELL IN GALLEY AND COCKPIT, GALLEY POWER SELECTED OFF. SMELL DISAPPEARED, POWER RE-ESTABLISHED, SMELL REAPPEARED. GALLEY POWER SELECTED OFF, AIRCRAFT RETURNED TO TORONTO. INSPECTED ALL OVENS, COFFEE MAKERS WIRSDR CA001019022Computer · failed(CAN) ON FINAL INTO CALGARY, WITH FLAPS AT POSITION 2, AFTER SELECTION ON LANDING GEAR DOWN, HAD ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE, FLIGHT CONTROL PRIMARY 1 AND 2 AND 3 FAULT. FLIGHT CONTROL INTO DIRECT LAW, RESET ATTEMPT ON PRIMARY 1 IN THE ASDR CA000802004Gcu · failed(CAN) AIRCRAFT ELECTRICAL, AC BUS 1-2 AT FAULT IN CRUISE. FOUND NR 2 GCU C/B POPPED. STRONG ELECTRICAL SMELL FROM UNIT. REPLACED NR 2 GCU, AIRCRAFT FOUND SERVICEABLE.SDR CA000621036Hydro Mech Unit · failed(CAN) ON ENGINE SHUT DOWN ALL 4 MASTERS SELECTED OFF, NR 2 ENGINE CONTINUED TO RUN FOR 2 MINUTES. ELECTRONIC DE-CENTRALIZED AIRCRAFT MONITORING MESSAGE HIGH PRESSURE FUEL VALVE NOT NR 2 SHUT DOWN.CHANGED HYDROMECHANICAL UNIT, LEAK CHECKED AND IDLE TESTED NO FASDR CA000209037Door · lack of lube(CAN) AIRCRAFT FAILED TO PRESSURIAZE AFTER TAKE OFF. R1 DOOR ECAM MESSAGE. DOOR MECHANISM LUBRICATED.SDR CA991231028Bearing · failed(CAN) NR 4 BEARING FAILURE ON NR 3 ENGINE,SDR CA000209036Panel · delaminated(CAN) PANEL NEAR LEADING EDGE OF NR 4 PYLON FOUND DELAMINATED. PANEL REPLACED.SDR CA991210030Trim Motor · leaking(CAN) GREEN SYSTEM HYD QUANTITY AND PRESSURE LOSS DURING FLIGHT. INVESTIGATION REVEALED A LEAKING PITCH TRIMMER LEAKING. UNIT REPLACED ALONG WITH BOTH ENGINE DRIVEN PUMPS AND CASE DRAIN FILTERS.SDR CA000110087Actuator · leaking(CAN) GREEN HYD SYS QUANTITY DROPPED TO ZERO, 1 & 4 PUMPS SHUT OFF AND ALTERNATE GEAR SELECTION CARRIED OUT. INVESTIGATION REVEALED NR 5 RT SPOILER SERVO ACTUATOR LEAKING.SDR CA991231027Ecu · failed(CAN) ENGINE FAILED, RELITE AND SUSEQENT COMPRESSOR STALL EXPERIENCED. ENGINE BORESCOPED WITH NO FAULTS FOUND, BOTH VARIABLE STATOR ACTS AND ECU REPLACED.SDR CA991210060Bottle · discharged(CAN) DOOR R3 SHOWING NOT ARMED ON FLIGHT ATTENDANDANTS PANEL AND ON ECAM. R3 DOOR ASSIST BOTTLE RECHARGED.SDR CA991210055Seal · leaking(CAN) SMOKE IN CABIN WITH APU ON AND ACU PACKS ON. INVESTIGATION REVEALED APU LOAD COMPRESSOR OIL SEAL LEAK. APU REPLACED.SDR CA991210054Door · out of adj(CAN) AMBER IN TRANSIT LIGHT ON FOR CENTER GEAR DOOR AFTER RETRACTION. AIRCRAFT LANDED. ADJUSTED CENTER LINE GEAR FIXED DOOR. SYSTEM OK.SDR CA991210032Engine · failed(CAN) REPORT TO FOLLOW. VSV ACTUATOR POSITION DEMAND DISAGREE FAULT VSVACT/HMU/J6 ANNUNCIATION. OPERATOR HAS FORBIDDEN DISPATCH WITH SIMILAR FAULT MESSAGES. INITIAL TESTING HAS SO FAR NOT REVEALED ANY FAULT. CFMI IS INVESTIGATING.SDR CA991210031Slide Raft · failed(CAN) R1 DOOR SLIDE/RAFT FAILED TO DEPLOY ON TEST. PACKBOARD SPEED LACING DID NOT RELEASE. UNIT REPLACED.SDR CA991103089Bearing · spalled(CAN) N1 FAN SEIZED. REPORT TO FOLLOW. NR 4 BEARING FAILURE EXPERIENCED.SDR CA991103088Bearing · spalled(CAN) COMPRESSOR STALLED. REPORT TO FOLLOW. NR 4 BEARING FAILURE EXPERIENCED. TH E OUTER RACE WAS SPALLED.
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