Aerospatiale ATR 72-212A
Service difficulty reports · 695
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 = 'ATR72212A' 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 = 'ATR72212A' 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 COEA2026040702705Seal · damagedFLIGHT 8663, ENROUTE ANC - FAI AIR TURNBACK/DISCREPANCY: AIR TURNBACK PERFORMED DUE TO SOUNDS OF RATTLING AND SQUEALING FROM FLOOR AREA FORWARD OF CENTER CONSOLE. NO EMERGENCY DECLARED. MAINTENANCE FOUND AVIONICS ACCESS DOOR SEAL ROLLED OVER ON ITSELF. OPSDR COEA2026040301705Controller · faultedFLIGHT 8663, ANC - FAI, AIR TURNBACK/DISCREPANCY: L/H WINDSHIELD HEAT FAULT DURING FLIGHT. THE AIRCRAFT WAS RETURNED TO ANC. NO EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD TEMP CONTROLLER. OPS CHECKS GOOD.SDR MTNA20250307001Unknown · smokeDURING STARTUP OF AIRCRAFT N708FE ON FLIGHT 8129 BQN-POS, THE CREW NOTICED A HAZE IN THE COCKPIT THAT SMELLED LIKE SMOKE ALONG WITH THE CAPTAIN'S SIDE INTERCOM AND MICROPHONE NOT WORKING. THE CREW SHUTDOWN THE AIRCRAFT AND MAINTENANCE BEGAN TROUBLESHOOTING. BSDR 29GA2025020400001Valve · leakingDURING TAKEOFF LOST GREEN HYDRAULIC SYSTEM PUMP. LOW LEVEL ILLUMINATED, AND LANDING GEAR FAILED TO RETRACT. PERFORMED QRH DECLARED AN EMERGENCY OBSERVED LANDING GEAR SPEED. PERFORMED MANUAL EXTENSION, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MAIN LANDINGSDR 29GA2025010300001Warning Message · activatedLANDING GEAR NOT DOWN ANNUNCIATOR IN FLIGHT NUMEROUS TIMES. OHM OUT CHECK RADIO ALTIMETER COAX CABLE AND ANTENNAS TEAT NORMAL.SDR 29GA2025120100001Selector Valve · malfunctionedON DEPARTURE AFTER RETRACTING LANDING GEAR, WE HAD 3 UNLOCK LIGHT INDICATION ON BOTH PANELS. AIRCRAFT FLYING SLUGGISH TO INDICATE LANDING GEAR WAS NOT RETRACTED, DECLARED EMERGENCY AND DID AN AIR RETURN TO MYAM. CORRECTIVE ACTION- REMOVED AND REPLACED MLG SELESDR 29GA2024120700001Engine · flamed outENGINE #1 FLAMEOUT ON APPROACH DUE TO FUEL STARVATION ACCOMPLISHED WITH A BRIEF LOSS OF POWER IN ENGINE #2. CORRECTIVE ACTION- PERFORMED VISUAL EXAMINATION OF FUEL LEVEL WITH MANUAL MAGNETIC INDICATOR. FOUND 880 LBS. OF FUEL ON RH AND NO INDICATION ON LH TANKSDR 29GA2024060700001Skin · puncturedDURING POST FLIGHT WALK AROUND PUNCTURE FOUND IN AIRCRAFT BEHIND CAPTAINS' SEAT ON OUTSIDE OF AIRCRAFT. CORRECTIVE ACTION-LH FUSELAGE SKIN REPAIR AT AFT SIDE OF FRAME 10, 7 INCHES ABOVE STRINGER 14 HAS BEEN ACCOMPLISHED IAW SRM, POST REPAIR PRESSURE AND FUNCTISDR 29GA2024043000001Uplock · malfunctionedONCE LEVEL OFF UPPER PANEL UNLOCK RED LIGHT ILLUMINATED LANDING GEAR. REMOVED AND REPLACED NLG UPLOCK BOX, OPS CHECK GOOD.SDR 29GA2024042200001Skin · handler errorDURING GROUND OPERATION OF MSN 1038 AT FFL AIRPORT (FORT LAUDERDALE USA) ON MAY 01ST 2024, THE AIRCRAFT (STATIC) WAS IMPACTED AT HIGH SPEED BY A BAGGAGE CART AT LEVEL OF RH FR22. AFTER PRELIMINARY INSPECTION AS PER INSPECTION LIST REF. ES_00238510_01_A, THE A/SDR 29GA2024041800001Connector · looseLT MAIN LANDING GEAR UNSAFE INDICATION ON SECONDARY PANEL DURING FINAL APPROACH. PRIMARY PANEL INDICATED GREEN. COMPLETED ONE PANEL UNSAFE INDICATION CHECKLIST BEFORE LANDING. CORRECTIVE ACTION- FOUND FWD. LH DOWN LOCK SENSOR ELECTRICAL CONNECTOR LOOSE AND RESSDR 29GA2024031200001Connector · loose#2 ENGINE OVER TORQUE ON TAKEOFF (111.1%) AFTER ABORTED TAKEOFF TQ REMAINED AT 70% WITH PL AT GROUND IDLE. TAKEOFF ABORTED BELOW 70 KNOTS. FOUND PEC SYSTEM FAULTY ON MCDU INSPECTED PVM AND FOUND LOOSE CANNON PLUG, RESECURED CONNECTOR, PERFORMED ERASING OF PECSDR 29GA2024021400001Proximity Switch · faultedON APPROACH HAD LEFT MAIN UNLK LIGHT ON OVERHEAD PANEL. WENT OFF UPON DOING GO AROUND. CORRECTIVE ACTION: FOUND 11GB PROXIMITY SWITCH AT FAULT ON MCDU, REMOVED AND REPLACED 11GB PROX SWITCH, GEAR SWINGS AND OPS CHECK GOOD.SDR 29GA2024020900001None · handler errorDURING RELOCATION AIRCRAFT COLLIDED WITH VEHICLE DAMAGE TO LOWER LEFT SECTION AFT OF PASSENGER DOOR. MAPPED THE EXTERNAL FUSELAGE AREA BETWEEN FRAME 39 AND 42. LAV REMOVED FOR ACCESS TO INTERNAL SIDE. DENT JUST AFT OF FRAME 41 BETWEEN STRINGER 14L AND 15L FSDR 29GA2023110200001Engine · unknownAT 1000 FEET FOUND EVIDENCE OF SPARKS COMING OUT OF #1 ENGINE EXHAUST. FOUND DAMAGED BLADES ON #1 ENGINE ASSY, REMOVED AND REPLACED ENGINE ASSY OPS AND LEAK CHECKS GOOD.SDR 29GA2023101100001Unknown · unknownAT APPROXIMATELY10000 FT, WE HAD EXCESSIVE PRESSURE AND DELTA P LOTS OF BANGING SOUNDS. AUTO PILOT DISCONNECTED MULTIPLE TIMES, HAND FLOWN EXCESSIVE VIBRATION AND FLIGHT CONTROLS FELT OFF. CORRECTIVE ACTION REMOVED AND REPLACED PRESSURE SWITCH OPS CHECK GOOD.SDR 29GA2023092500001Door · leakingAC WOULD NOT PRESSURIZE. FA CALLED AND SAID THERE WAS A LOUD SQUEAL OR HISSING SOUND COMING FROM EMERGENCY EXIT A1. REINSTALLED LH EMERGENCY EXIT IAWAMM. FUSELAGE PRESSURIZATION OPS CHECK NORMAL PER AMM NO FURTHER ISSUES.SDR 29GA2023082100001Oil Cap · looseLEFT MASTER WARNING OIL PRESSURE LOSS. FOUND OIL CAP LOOSE, SERVICED ENGINE RESECURED CAP, REPLACED ENGINE IBV FILTER OPS CHECK GOOD.SDR 29GA2023011300001O-Ring · damagedFLIGHT 3945, NR 2 ENGINE OIL PRESSURE DROPPED OFF PRECAUTIONARY ENGINE SHUTDOWN. PERFORMED LOSS OF OIL PRESSURE CHECK IAW 05-50-00, FOUND PVM LEAKING. REMOVED AND REPLACED TRANSFER TUBE O-RING OPERATIONAL CHECK GOOD. ORIG SUBMISSION DATE: 1/13/2023SDR 29GA2022120500001O-Ring · damagedFLIGHT: 95 JAX/PNS ENGINE 2 OIL LOW PRESSURE IN FLIGHT SHUT ENGINE 2 IN FLIGHT. CORRECTIVE ACTION: FOUND OIL AT RIGHT EXHAUST DUCT STARTER GENERATOR. REMOVED AND REPALCED STARTER GENERATOR DRIVE SHAFT O RING, RIGHT ENGINE OPERATIONAL CHECK NORMAL.SDR COEA2022122901701Support · crackedCRACKED ALUMINUM ROLLER GUIDE SUPPORT REPLACED BY NEW STEEL SUPPORT. REPAIRED IAW SRAS ES_0157948_01.SDR 29GA2022080200001Brake · weakFLIGHT: 3989 AFW/AFW THE CAPTAIN REPORTED AN APPROXIMATE 50% LOSS OF BRAKE EFFECTIVENESS WHILE AT 10KTS. PERFORMED FUNCTIONAL TEST OF ANTISKID SYSTEM, BLED HIGH- AND LOW-PRESSURE SYSTEM OPERATIONAL CHECK GOOD.SDR 2022F00042Axle · bentNLG WAS SENT IN FOR O/H. UPON DISASSEMBLY, THE SLIDING ROD, TURNING TUBE, AND AXLE ALL HAD SIGNIFICANT DEFORMATION. IT WAS LEARNED THE A/C THE GEAR WAS INSTALLED ON HAD A TAIL STRIKE IN 2017, AND THE NLG WAS RELEASED FOR SERVICE AFTER ENGINEERING EVALUTION BSDR 29GA2021061700001Warning Light · false activationFLIGHT: 79 TLH/FLL LANDING GEAR "UNLOCK" LIGHT ONLY ON MAIN PANEL WHEN GEAR SELECTED DOWN POSSILBE TIE TO MFC FAULT AS SOON AS MFC RECOVERED NOSE GEAR EXTENDED AND WE HAD 3 GREEN. CORRECTIVE ACTION: PERFORMED OPERATIONAL CHECK COULD NOT DUPLICATE.SDR 29GA2021051300001Bracket · bentFLIGHT: 146 GSP/MCO LAVATORY DOOR UNABLE TO OPEN FROM THE INSIDE. CORRECTIVE ACTION: INSPECTED LAV DOOR LATCH MECHANISM AND FOUND DOOR FRAME BRACKET WHERE LATCH MAKES CONTACT WITH DOOR FRAME BENDED OUT OF SAHPE PREVENTING NORMAL OPERATION OF THE DOOR, STRAIGHTSDR Q0MF202009020372Pump · abnormalON AUG 30, MANDARIN AIRLINES B-16856 AE366 FROM MZG TO TSA, ENG 1 FLAME OUT DURING T/O PHASE AFTER POWER LEVER TO NOTCH, RTO. ACTION TAKEN: THE MECHANIC CHECK FOUND PEC FAULT CODE 31/32/71, REPLACED PEC FOR PREVENTIVE MAINTENANCE. CHECK QAR DATA FOUND ENG NRSDR 29GA2020030200001Connector · looseFLIGHT# 9005 FLL/TPA REPORT: DOOR EMER LIGHT ILLUMINITED AFTER TAKE OFF. CORRECTIVE ACTION: FOUND EMERGENCY DOOR HATCH LIGHT TO BE ILLUMINATED. HATCH WAS IN LOCKED AND CLOSED POSITION. RESET CANNON PLUG AND OPENED AND CLOSED HATCH, AND PERFORMED OPS CHECK OF SDR CA190626011Adapter · corroded(CAN) WE FOUND CORROSION ON THE BOTTOM, TCAS ANTENNA ADAPTER, AT THE SAME TIME WE REALISED THAT THE COUNTERSINK FASTENERS HOLES WERE ON THE WRONG SIDE. NEW ONE WAS ORDERED FROM THE TYPE CERTIFICATE HOLDER AND THE NEW TCAS ANTENNA ADAPTER RECEIVED HAVE THE SAMESDR CA190624003Blade · fractured(CAN) DURING GROUND RUN AFTER THE T6 CABLE REPLACEMENT, ENGINE SURGING OCCURRED AND UNUSUAL NOISE WAS HEARD. THE ENGINE WAS SHUT-DOWN AND DURING INSPECTION, WHILE MANUALLY TURNING THE PROPELLER, A NOTICEABLE RUBBING SOUND COULD BE HEARD. VISUAL INSPECTION VIA SDR CA190607003Bearing · failed(CAN) CUSTOMER REPORTED THAT THE LEFT HAND ENGINE WAS SHUT DOWN IN FLIGHT AFTER THE CREW HEARD A LOUD NOISE WITHOUT ENGINE ALARM. SMOKE WAS OBSERVED AT THE STATION AND IN THE CABIN. (TC# 20190607003)SDR CA190425007Fire Warning · illuminated(CAN) DURING A LANDING APPROACH, WHILE AT APPROXIMATELY 2000 FT, THE RIGHT-HAND ENGINE FIRE WARNING ILLUMINATED. THE CREW ELECTED TO SHUT DOWN THE ENGINE, AND DECLARED AN EMERGENCY LANDING. THE AIRCRAFT LANDED UNEVENTFULLY, INVESTIGATION CARRIED OUT AND IS NOWSDR CA190416003Control Unit · malfunctioned(CAN) DURING POST PROPELLER DEFECT RECTIFICATION, ENGINE NUMBER TWO DISCOVERED THAT THE FUEL FLOW IS NOT RESPONDING TO THE PLA MOVEMENT WHEN EEC IS IN OFF POSITION. MFCU WAS REPLACED, ISSUE WAS RESOLVED. (TC# 20190416003)SDR CA190405008Unknown · odor(CAN) CREW REPORTED THAT OIL SMELL IN COCKPIT (WITHOUT SMOKE) AT FI, IN DESCENT AND SOMETIMES IN CLIMB.SDR CA190627003Case · cracked(CAN) CREW REPORTED TO HAVE SMOG IN CABIN AND COCKPIT DURING CRUISE. AS PER MM, VISUAL INSPECTION OF BOTH ENGINE EXTERNAL OIL LEAKS CHECK C/O. NL SENSOR PACKING CONDITION CHECKED FOR OCM INSPECTION BUT NO ABNORMALITY FOUND. ALSO, AS PER MM CHECKED ENGINE SWITCSDR CA190514004Sensor · malfunctioned(CAN) DURING CLIMB AND PASSING THROUGH FL80, THE FLIGHT CREW WITNESSED TORQUE ON THE LEFT-HAND ENGINE EXHIBITING AN UN-COMMANDED ROLL BACK. AT FL100, LEFT-HAND ENGINE TORQUE DECREASED TO A LEVEL THAT WAS 20% LESS THAN RIGHT-HAND ENGINE TORQUE. UPON ATTAINING CSDR CA190219005Bearing · damaged(CAN) DURING FLIGHT, THE RIGHT HAND ENGINE EXPERIENCED TORQUE FLUCTUATION AND INTER TURBINE TEMPERATURE RISING FOLLOWED BY FIRE WARNING INDICATION. THE FLIGHT CREW RESPONDED BY PULLING THE FIRE HANDLE AND DISCHARGE THE FIRE BOTTLE. THE AIRCRAFT LANDED UNEVENTFSDR CA160216011Blades · damaged(CAN) DURING TAXI OUT THE MOMENT THE PILOT ADVANCED POWER LEVER, THERE WAS SMOKE IN CABIN. THE PILOT SHUTDOWN NR 2 ENGINE AND TAXIED BACK TO THE BAY. GROUND ENGINEER FOUND 3 TO 4 PT2 BLADES MISSING TIP HALVES. TURBO MACHINERY CHIP DETECTOR WAS FOUND WITH SIGNISDR CA151216015Engine · smoke(CAN) DURING TAXI TO THE GATE, THE CONTROL TOWER INFORMED THE CREW THAT SMOKE WAS COMING OUT OF THE NR 1 ENGINE. THE ENGINE HAD BEEN FEATHERED WHEN THE SMOKE CAME OUT. THE CREW RECEIVED A FIRE WARNING AND PULLED THE TEE HANDLE AS A PRECAUTIONARY MEASURE, RESSDR CA151216010Vane · failed(CAN) DURING CLIMB, A LOW OIL PRESSURE WARNING OCCURRED. THE CREW ELECTED TO TURN BACK TO THE DEPARTURE AIRPORT WHERE POST FLIGHT INSPECTION FOUND SIGHT GLASS OIL LEVEL ABOVE ADD 1. THE CHIP DETECTOR WAS CLEAN BUT A FUEL ODOR WAS NOTED IN THE OIL. THE FUEL HSDR CA151216012Unknown · odor(CAN) THIS ENGINE HAS BEEN EXPERIENCING BLEED AIR CONTAMINATION SINCE NOV. 6TH. DECONTAMINATION OF THE ACFT AIR SYS WAS PERFORMED, REPLACEMENT OF THE AIR CYCLE MACHINE, ENGINE BLEED VALVE ETC. TO NO AVAIL, OIL ODOR RETURNED AFTER A WEEK OF OPERATION AT WHICH SDR CA151215002Turbine Case · separated(CAN) ON REACHING CRUISE, A FIRE INDICATION OCCURRED FOLLOWED BY A LOUD NOISE AND ENGINE SHUTDOWN. AN UNEVENTFUL SINGLE ENGINE LANDING WAS THEN CARRIED OUT. POST FLIGHT INSPECTION DID NOT REVEAL ANY FIRE DAMAGE. HEAVY DAMAGE TO THE POWER TURBINE AREA WITH ASDR CA151215011Engine · damaged(CAN) DURING CLIMBING OUT THE CREW NEEDED TO SHUT THE LT ENGINE DOWN. THE ACFT RETURNED FOR A SAFE LANDING. BORESCOPE INSPECTION REVEALED EXTENDED DAMAGE AT NUMEROUS LOCATION IN THE ENGINE. THE ENGINE WILL BE SENT FOR INVESTIGATION AND REPAIR.SDR CA151130018Warning Light · false activation(CAN) THE RT ENGINE WAS SHUTDOWN DUE TO LOW OIL PRESSURE ACCOMPANIED BY MASTER CAUTION LIGHT DURING FLIGHT. THE PILOT DIVERTED THE AIRCRAFT AND MADE AN UNEVENTFUL LANDING. PRELIMINARY TROUBLESHOOTING REVEALED OIL LEVEL STILL VISIBLE ON SIGHT GLASS WITH NO SIGSDR CA151130005Blades · damaged(CAN) DURING A WALK-AROUND, PRIOR TO FLIGHT, THE PILOT DISCOVERED MULTIPLE BLADE DAMAGE TO THE SECOND POWER TURBINE STAGE. ACFT GROUNDED AND WAITING FINAL INSPECTION FOR DISPOSITION.SDR CA151030012Engine · shutdown(CAN) DURING CRUISE THE ENGINE SUFFERED AN IN-FLIGHT SHUTDOWN. TROUBLESHOOTING & ENGINE REPLACEMENT IN PROGRESS. NO FURTHER DETAILS OF THE EVENT AT THIS TIME.SDR CA151029016Engine · contaminated(CAN) DURING DESCENT, WHEN BOTH POWER LEVERS WERE MOVED TO IDLE, A SIGNIFICANT AMOUNT OF SMOKE APPEARED IN COCKPIT WITH SMOKE FUME ODOR. AN UNEVENTFUL LANDING FOLLOWED AT DESTINATION. POST FLIGHT INSPECTION FOUND OIL INSIDE THE GAS GENERATOR AND INTERCOMPRESSOSDR CA151015007Blade · fractured(CAN) IN CRUISE FLIGHT, THE PILOT SHUTDOWN THE LT ENGINE AFTER LOW OIL PRESSURE WARNING. THE ACFT RETURNED TO ORIGIN AND MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING REVEALED PT2 BLADE WERE FRACTURED. THE ENGINE WILL BE REMOVED FOR INVESTIGATION.SDR CA151015010Oil System · leaking(CAN) DURING FLIGHT, REPORTS OF FLUID LEAKING FROM THE NACELLE FUEL/OIL DRAIN OF NR 1 ENGINE PROMPTED THE CREW TO SHUT THE ENGINE DOWN. NO COCKPIT INDICATIONS REPORTED. THE ACFT LANDED SINGLE ENGINE WITHOUT ANY FURTHER PROBLEMS. POST FLIGHT INSPECTION FOUND SDR CA151015001Engine · making metal(CAN) DURING FLIGHT, THE PILOT RECEIVED A LOW OIL PRESSURE WARNING AND FOLLOWED PROCEDURES AND SHUT THE ENGINE DOWN. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT INSPECTION REVEALED A SIGNIFICANT AMOUNT OF DEBRIS ON THE 1 OF THE CHIP DETECTORS. SDR CA151007008Bearing · leaking(CAN) SMOKE FOUND IN COCKPIT AND CABIN DURING DECREASING POWER LEVER. AFTER TROUBLESHOOTING, AN OIL LEAK FROM BEARING NR 5 IS SUSPECTED.
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