Aerospatiale ATR 72-212
Service difficulty reports · 4,441
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 = 'ATR72212' 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 = 'ATR72212' 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 COEA2015123104801Landing · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT ENG NACELLE INBD AFT LANDING FOR PANEL 474AR, HAS CHAFING DAMAGE, LEVEL 2 CORROSION. REPAIR IAW SRAS CE 219 16 9937 DATED 2 2 2016.SDR COEA2015121705807Wire Harness · defectiveFLIGHT 8663, AIR TURN BACK, DISCREPANCY SHORTLY AFTER TAKEOFF. THE LG HANDLE COULD NOT BE MOVED TO RETRACT GEAR. IN ADDITION, ATC WAS NOT RECEIVING ANY TRANSPONDER SIGNAL. CREW ELECTED TO RETURN, NO EMER WAS DECLARED. INTERNAL AND EXTERNAL HARNESSES ON RISDR COEA2015111217807Pan · corrodedFWD CARGO DOOR HAS CORROSION AT INBOARD LOWER STRUCTURE. REPLACED LOWER PAN WITH OEM PART.SDR CA150925001Oil System · pressure loss(CAN) ACFT EXPERIENCED AN INFLIGHT ENGINE SHUTDOWN SHORTLY AFTER TAKEOFF. THE FLIGHT CREW REPORTED THE NR 2 ENGINE WITH A LOW OIL PRESSURE WARNING ON THE CREW ALERT PANEL, CAP, FOLLOWED BY THE LOCAL RED LED ALERT ON THE ENGINE OIL PRESSURE GAUGE. JUST AS THESDR CA150911001Eec · malfunctioned(CAN) DURING NORMAL OPERATION ON A SCHEDULED FLIGHT, THE CREW NOTED THAT TORQUE ON THE LT ENGINE BOTH DIGITAL AND ANALOG INDICATIONS FLUCTUATED. THE ACFT RETURNED TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL LANDING WAS MADE. TROUBLESHOOTING LED TO THE REPLSDR COEA2015081616807Threshold · corrodedLEFT PASSENGER DOOR THRESHOLD, DOUBLER AND DRAIN CHANNEL HAVE CORROSION. REPLACED THRESHOLD WITH OEM PART.SDR COEA2015081612807Closeout Panel · corrodedRIGHT OUTBOARD SEAT TRACK CLOSE OUT PANEL FRAMES 35-36 HAS CORROSION. REPLACED THE CLOSEOUT PANEL.SDR COEA2015081608807Doubler · corrodedBRIDGING CHECK COE & MINOR REPAIR. RT SERVICE DOOR THRESHOLD DOUBLER HAS LEVEL 2 CORROSION. REPLACED DOUBLER WITH OEM PART.SDR COEA2015081607807Channel · corrodedBRIDGING CHECK COE & MINOR REPAIR. RT SERVICE DOOR THRESHOLD, DRAIN CHANNEL HAS LEVEL 2 CORROSION. REPLACED DRAIN CHANNEL WITH OEM.SDR COEA2015081606807Bracket · corrodedBRIDGING CHECK COE & MINOR REPAIR. BRACKET AFT OF FRAME 37, HAS LEVEL 2 CORROSION AT THRESHOLD ATTACH LOCATION. REPLACED BRACKET WITH OEM PART.SDR COEA2015081602807Doubler · corrodedHEAVY CHECK COE & MAJOR REPAIR. FRAME 39 FWD DOUBLER AT LEVEL OF SERVICE DOOR, THRESHOLD HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 4529 15 9581 DATED 10 1 15.SDR COEA2015081508807Stringer Clip · corrodedBRIDGING CHECK COE & MINOR REPAIR. STRINGER CLIP AT FRAME 13, STRINGER 20 LT, HAS LEVEL 2 CORROSION. REPLACED STRINGER CLIP WITH OEM PART.SDR COEA2015081506807Stringer Clip · corrodedBRIDGING CHECK COE & MINOR REPAIR. STRINGER CLIP AT FRAME 13, STRINGER 20 RT, HAS LEVEL 2 CORROSION. REPLACED STRINGER CLIP WITH OEM PART.SDR COEA2015081505807Crease Beam · corrodedBRIDGING CHECK COE & MAJOR REPAIR. LT CREASE BEAM OUTER CHORD HAS LEVEL 2 CORROSION, AT FRAMES 39 - 40. REPAIR IAW SRAS CE 4530 15 9582 DATED 10 5 15.SDR COEA2015081503807Frame · corrodedHEAVY CHECK COE & MAJOR REPAIR. FRAME 13 HAS LEVEL 2 CORROSION ON THE AFT SIDE, BETWEEN STRINGER 19L - 20L. REPAIRED IAW SRAS ES-4388 15 9551 DATED 9 21 15.SDR COEA2015081501807Failsafe · corrodedHEAVY CHECK COE & MINOR REPAIR. FRAME 14 FAIL SAFE HAS LEVEL 2 CORROSION. STRINGER 20L - 21L. REPAIR IAW SRAS CE-4472 15 9584 DATED 9 17 2015.SDR COEA2015081209807Splice · corrodedWO 151753 NR 800007 BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, UPPER PAN SPLICE ON AFT EDGE HAS LEVEL 2 SURFACE CORROSION. REPLACED SPLICE WITH OEM PART.SDR COEA2015081203807Intercostal · corrodedBRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON INTERCOSTAL. REPLACED WITH OEM PART.SDR COEA2015081202807Intercostal · corrodedBRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON INTERCOSTAL. REPLACED WITH OEM PART.SDR COEA2015081204807Fitting · corrodedBRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON CLIP. REPLACED WITH OEM.SDR COEA2015081111807Skin · gougedLEFT WING UPPER COMPOSITE SKIN GOUGED BETWEEN RIB 25-26. REPAIRED IAW SRAS ES-4416/15.10341.SDR COEA2015081015816Panel · chafedWO 148276 NR 500040 HEAVY CHECK COE & MAJOR REPAIR. LT WING, OUTER BOX, UPPER FIXED PANEL HAS CHAFE DAMAGE ON THE LANDING FOR PANEL 523GT. REPAIR IAW SRAS ES 4336 15 9597 DATED 9 10 2015.SDR COEA2015080714816Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE, RT LATERAL LOWER SKIN PANEL HAS AREAS OF TOOLING MARKS & LIGHT CORROSION. REPAIR IAW SRAS S536R0256 9574 DATED 9 3 2015.SDR COEA2015080610807Spar · gougedLEFT WING FRONT SPAR UPPER LEADING EDGE FLANGE HAS NUMEROUS GOUGES, RIBS 25-31. REPAIRED IAW SRAS ES-4389/15.10431.SDR COEA2015080601807Hinge Fitting · corrodedBRIDGING CHECK COE & MINOR REPAIR. RT AILERON OTBD HINGE FITTING IS EXFOLIATED AT THE GROUNDING CONNECTION POINT. REPLACED WITH OEM PART.SDR COEA2015072217816Fitting · corrodedHEAVY CHECK COE & MINOR REPAIR. LT ELEVATOR OTBD END CLOS OUT FITTING HAS LEVEL 2 CORROSION. REPLACED WITH NEW OEM PART.SDR COEA2015072109816Fitting · corrodedWO 148276 NR 200060 HEAVY CHECK COE & MAJOR REPAIR. FIRST OFFICERS SEAT FITTING HAS LEVEL 2 CORROSION ON 3 OF 4 RAISED AREAS COMMON TO NUTPLATES. REPAIR PER SRAS CE-4120 15 9480 DATED 8 6 15.SDR COEA2015072104816Frame · wornWO 148276 NR 200064 HEAVY CHECK COE & MAJOR REPAIR. LT SUB FRAME 27A HAS WEAR DAMAGE FROM WIRE CONDUIT. REPAIR IAW SRAS CE-4077 15 9479 DATED 8 6 15.SDR MTNA07212015002Rib · corrodedCORROSION FOUND ON RT INBD FLAP, OTBD RIB. REPLACED RIB. R & R RIB IAW SRM 51-52-10, 51-25-03, AND 51-25-04.SDR MTNA07212015001Tee Fitting · corrodedCORROSION FOUND ON LT AILERON INBD TEE FITTING. THE FITTING WAS REPLACED. REPLACED INBD T-PICK UP FITTING, LT AILERON IAW SRM 512501-02-001-A01, 512503-02-001-A01.SDR COEA2015071916816Fitting · corrodedWO 148276 NR 300014 HEAVY CHECK COE & MINOR REPAIR. RT ELEVATOR OTBD ON THE AFT END CLOSE OUT FITTING HAS LEVEL 2 CORROSION. REPLACED WITH NEW OEM PART.SDR COEA2015071912816Skin · damagedHEAVY CHECK COE & MAJOR REPAIR. LEFT VERTICAL STABILIZER SKIN HAS FRETTING DAMAGE, LEVEL 2, ABOVE THE UPPER VORTEX GENERATOR. REPAIRED IAW SRAS CE-4167/15 9528 DATED 8 13 15.SDR COEA201507198816Skin · corrodedWO 148276 NR 500034 HEAVY CHECK COE & MAJOR REPAIR. UPPER WING PANEL LANDING FOR PANEL 522CT HAS FRETTING. REPAIR IAW SRAS DO TS 3018 09 5261 ISSUE D DATED 7 31 15.SDR COEA2015071907816Skin · corrodedWO 148276 NR 500033 HEAVY CHECK COE & MAJOR REPAIR. UPPER WING PANEL LANDING FOR PANEL 521DT HAS FRETTING. REPAIR IAW SRAS DO TS 3018 09 5261 ISSUE D DATED 7 31 15.SDR COEA2015071906816Skin · corrodedHEAVY CHECK COE & MAJOR REPAIR. UPPER WING PANEL LANDING FOR PANEL 622CT HAS FRETTING. REPAIR IAW SRAS DO TS 3018 09 5261 ISSUED DATED 7 31 15.SDR COEA2015071711816Landing · corrodedHEAVY CHECK COE & MAJOR REPAIR. RT ENG NACELLE PANEL LANDING AT STATION 3197 HAS LEVEL 2 FRETTING & CORROSION ON THE OTBD SIDE. REPAIR PER SRAS CE-4126 15 9493 DATED 8 7 15.SDR COEA2015071705816Crease Beam · damagedHEAVY CHECK COE & MAJOR REPAIR. LT CREASE BEAM WEB BETWEEN FRAMES 19 - 20 HAS TOOLING DAMAGE. REPLACED PART BY FABRICATION.SDR COEA2015071610816Bulkhead · burnedHEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD HAS BURN MARK RBL 10 IN. REPAIR IAW SRAS DO TS-3897 05 3326 DATED 8 4 15.SDR COEA2015071113816Support Beam · corrodedWO 148276 NR 500019 HEAVY CHECK COE & MAJOR REPAIR. LT FLAP SUPPORT BEAM AT RIB 13 HAS PLAY & FRETTING AT THE LOWER WING ATTACH POINT, LEVEL 2 CORROSION. REPAIR IAW SRAS CE 4020 15 9565 DATED 8 27 2015.SDR COEA2015071103816Doubler · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT FRAME 39 DOUBLER AT FLOOR LEVEL HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE-3965 15 9444 DATED 7 24 15.SDR COEA2015071002816Stringer · corrodedHEAVY CHECK COE & MAJOR REPAIR. STRINGER 2AR HAS TOOLING MARKS & CORROSION FRAME 16 - 17. REPAIR IAW SRM 53-00-00-300-824-A01.SDR COEA2015071001816Stringer · crackedWORK ORDER 148276 NR 200019 HEAVY CHECK COE & MAJOR REPAIR. STRINGER 7R HAS A CRACK, FRAME 13 - 14. REPAIRED USING SRM 530000-300-824-A01.SDR COEA2015070604807Ahrs · malfunctionedFLIGHT 7202 EN-ROUTE, DISCREPANCY. ONCE AIRBORNE, AFTER TAKEOFF, THE NR 2 EADI STARTED SHOWING PITCH & ATTITUDE CAUTIONS. THE CREW ELECTED TO RETURN, NO EMER WAS DECLARED. REPLACED THE NR 2 AHRU. OPERATIONS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR COEA2015062502803Fitting · crackedFLIGHT 7299 EN ROUTE, EMER DECLARED, DISCREPANCY. WHILE AT CRUISE EN ROUTE, THE CREW RECEIVED A GREEN HYD SYS LOW LEVEL INDICATION & CCASS ALERT. WHILE RUNNING THE QRC, THE CREW ALSO RECEIVED A LOW PRESS INDICATION ON THE SAME SYS. AN EMER WAS DECLARED & THSDR COEA2015050701803A/C Pack · damagedFLIGHT 8277 EN-ROUTE, SMOKE IN COCKPIT. APPROX 60 MILES OUT, THE CREW DETECTED A STRONG SMOKE SMELL IN THE COCKPIT. THE CREW DECLARED AN EMER AS SMOKE BEGAN TO BUILD IN THE COCKPIT. WHILE RUNNING THRU THEIR CHECKLIST, FOR SMOKE IN THE COCKPIT, THE SMOKE LIFSDR COEA2015042302819Skin · damagedFLIGHT 7277, BIRD STRIKE, DISCREPANCY. ON APPROACH, THE ACFT FLEW THROUGH A FLOCK OF BIRDS. THE CREW ELECTED TO CONTINUE AFTER DETERMINING THAT THE ACFT WAS MANEUVERING NORMALLY, NO VIBRATION COULD BE DETECTED & ALL ENG GAUGES WERE INDICATING NORMAL. THE ACSDR COEA2015040203805Fitting · corrodedHEAVY CHECK COE & MINOR REPAIR. SHEAR CLIP FWD ON SERVICE DOOR THRESHOLD HAS LEVEL 2 CORROSION AT THE MATTING SURFACE OF FRAME 37. REPLACED WITH OEM PART.SDR CA150408007Engine · flamed out(CAN) DURING DESCENT, THE NR 2 ENG FLAMED OUT WITH NO PRIOR INDICATION. PILOTS PROCEEDED WITH ENG SHUTDOWN PROCEDURE & LANDED WITHOUT FURTHER INCIDENT. GND INSPECTION CONFIRMED FUEL SUPPLY, CHIP DETECTOR CLEAN. ENG GND RUN WAS PERFORMED & THE ENG WAS RUNNINSDR CA150331012Autofeather Sys · malfunctioned(CAN) DURING FLIGHT NR 2 PROPELLER EXPERIENCED UNCOMMANDED FEATHER. THE CREW SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. NR 2 MULTI-FUNCTION COMPUTER AND AUTOFEATHER UNIT WERE REPLACED AND SENT TO ATR MFG FOR ANALYSIS. ENGINE TORQUE SENSORS ALSO REPLACEDSDR COEA2015032608805Skin · damagedNR 1 HEAVY CHECK MAJOR REPAIR. RT WING PANEL LANDING 622CT HAS TOOLING DAMAGE. REPAIR IAW SRAS DO TS 1529 05 3169 ISSUE E DATED 4 17 15.
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