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 COEA2014012304819Skin · damagedUPPER WING CUT OUT FOR ACCESS PANEL 622CT HAS FRETTING. REPAIR IAW SRAS DO TS-531 06 3474 ISSUE D.SDR COEA2014012202819Floor Support · crackedLEFT LONGITUDINAL FLOOR BEAM IS CRACKED FWD OF FRAME 35. REPAIRED IAW EO 5315-02 REV ORIGINAL 8/20/2013.SDR COEA2014012101819Floorbeam · crackedRIGHT LONGITUDINAL FLOOR BEAM IS CRACKED AFT OF FRAME 33 & FWD OF FRAME 34. REPAIR IAW EO 5315-02 REV ORIGINAL 8/20/2013.SDR COEA2014012203819Skin · dentedLEFT FUSELAGE SKIN IS DENTED BETWEEN FRAMES 34 & 35 ABOVE STRINGER 14L. REPAIR IAW ATR72 SRM 53-00-00 FIG 403.SDR COEA2014013005801Stiffener · crackedRIGHT TRUNION FITTING UPPER SURFACE STIFFENER HAS A CRACK AT THE UPPER FASTENER FOR THE FRAME 26 FAIRING SUPPORT. REPAIR IAW SRAS S535R0199 2982 ISSUE B 1/29/2014.SDR COEA2014013004801Skin · dentedFUSELAGE TAIL SECTION HAS A DENT ON THE LT SIDE BETWEEN FRAMES 46 - 47 & STRINGERS 11 - 12. REPAIR IAW SRM 53-00-00 FIG 403 & SRAS DT S-428-14 8194 DATED 1/30/2014.SDR COEA2014013003801Skin · damagedRIGHT WING CUTOUT FOR PANEL 622CT HAS LEVEL 1 FRETTING. REPAIR IAW SRAS DO TS-4809 07 4337 ISSUE C.SDR COEA2014013002801Skin · damagedLEFT WING CUTOUT FOR PANEL 522CT HAS LEVEL 1 FRETTING. REPAIR IAW SRAS DO TS-4809 07 4337 ISSUE C DATED 1/27/2014.SDR COEA2014013001801Skin · damagedLEFT WING CUTOUT FOR PANEL 521DT HAS FRETTING. REPAIR IAW SRAS DO TS-4809 07 4337 ISSUE C DATED 1/27/2014.SDR COEA2013121804801Bolt · shearedFLIGHT 7250 YVR TO OAK DISCREPANCY. DURING FLIGHT, FWD CARGO DOOR LEAKS AIR THROUGH A GAP IN LOWER FWD SECTION OF DOOR. AFTER ARRIVAL INTO OAK, MX FOUND MULTIPLE SHEARED BOLTS IN FWD LOWER DOOR FITTING. REMOVED FITTING, INSPECTED & INSTALLED NEW BOLTS IAW ASDR KPVA20140114011Splice · crackedDURING HEAVY MAINTENANCE, WING PRESSURE DECK AFT SECTION DAMAGED. REPAIRED IAW SRI: DT/S-6824/13-20928 ISS B.SDR KPVA20140114021Skin · tornDURING HEAVY MAINTENANCE, CARGO BAY DOOR PAN AREA SKIN TORN, REPAIRED IAW SRM 52-31-00, REPAIR 402. HFEC INSPECTION (ROTOTEST) CARRIED OUT IAW SRM 52-31-00. REPAIR 402, STEP 2 B 2,C. NO DEFECT FOUND.SDR KPVA20140114016Skin · corrodedDURING HEAVY MAINTENANCE. LEFT WING LOWER SKIN CORRODED AT T/E BETWEEN RIBS 3-4. CORROSION BLENDED IAW SRI DT/S-6640/13-20943.UT AND HFEC INSPECTION DONE AT REPAIRED AREA IAW DT/S-6640/13-20943 ISSUE A, NO FAULT FOUND.SDR KPVA20140114009Window Frame · corrodedDURING HEAVY MAINTENANCE, FUSELAGE COCKPIT NODE 5 LT AND RT WINDOW FRAME CORRODED. REAMED AND OVERSIZED LOCK FASTENERS INSTALLED IAW DT/S-6558/13/20926, ISSUE C.SDR MTNA112620130001Detector · out of positionAFTER ENGINE START, AFTER CONDITION LEVERS MOVED TO MAX RPM, RECEIVED A MASTER WARNING FOR ELECTIC SMOKE. RELOCATED THE ACFT SO IT WAS FACING INTO THE WIND AND NO WIND BLOWING UP THE TAIL PIPES OF THE ENGINES. THE ENGINES WERE RUN AND ALL SYSTEMS WERE NORMALSDR KPVA20140114015Skin · corrodedDURING HEAVY MAINTENANCE, LEFT WING LOWER SKIN AT FUEL PUMP CUT-OUT CORRODED. REPAIRED IAW DT/S-6614/13-20944 ISSUE A, UT AND HFEC INSPECTION DONE IAW DT/S-6614/13-20944 ISSUE A, NO DEFECT FOUND.SDR KPVA20140114005Seat Track · corrodedDURING HEAVY MAINTENANCE. SEAT TRACK, BETWEEN FRAMES 41 AND 44. REPLACED IAW SRM 53-00-00, REPAIR 453.SDR KPVA20140114020Panel · corrodedDURING DURING HEAVY MAINTENANCE. RIGHT TOP WING PANEL 622CT AND PANEL CUT-OUT CORRODED. REPAIRED IAW SRM 57-14-12 AND DT/S-7013-13/21063 ISSUE A, HFEC AND BONDING INSPECTION IAW DT/S-7013/13-21063 ISSUE A, NO DEFECT FOUND.SDR KPVA20140114014Panel · corrodedDURING HEAVY MAINTENANCE, LEFT TOP WING PANEL 521DT AND PANEL CUT-OUT CORRODED. REPAIRED IAW SRM 57-14-12 AND DT/S-7013/13-21063 ISSUE A, HFEC AND BONDING INSPECTION DONE IAW DT/S-7013/13-21063 ISSUE A, NO DEFECT FOUND.SDR KPVA20140114013Panel · corrodedDURING HEAVY MAINTENANCE, LEFT TOP WING PANEL 522CT AND PANEL CUT-OUT CORRODED. REPAIRED IAW SRM 57-14-12 AND DT/S-7013/13/21063, ISSUE A, HFEC AND BONDING INSPECTION DONE IAW DT/S-7013/13-21063 ISSUE A, NO DECFECT FOUND.SDR KPVA20140114004Floorbeam · wornDURING HEAVY MAINTENANCE. FLOORBEAM FRAME 21 BETWEEN LT AND RT INBD SEAT TRACKS, RBL 3, UPPER AFT FLANGE REPAIRED IAW SRM 52-00-00, REPAIR 449.SDR KPVA20140114019Spar · corrodedDURING HEAVY MAINTENANCE, RIGHT WING UPPER FLANGE AT RIB 4 CORRODED. REPAIRED IAW DT/S-6898/13-21040 ISSUE "A", HFEC AND ULTRASONIC INSPECTION DONE IAW DT/S-6898/13-21040, ISSUE "A."SDR KPVA20140114018Bracket · corrodedDURING HEAVY MAINTENANCE, RIGHT WING AFT SPAR UPPER STRIP SLAT CORRODED BETWEEN RIBS 3-8. CORROSION BLENDED AND FAYING SURFACE RESTORED IAW SRI DT/S-6898/13-21040.SDR KPVA20140114017Skin · corrodedDURING HEAVY MAINTENANCE, RIGHT WING LOWER SKIN AT FUEL PUMP HOLE CORRODED. REPAIRED IAW DT/S-6696/13-20933A, HFEC INSPECTION IAW DT/S-6696/13-20933A. NO DEFECT FOUND.SDR KPVA20140114012Spar · corrodedDURING HEAVY MAINTENANCE, LEFT WING AFT SPAR UPPER STRIP SLAT, CORRODED BETWEEN RIBS 3-4. CORROSION BLENDED AND FAYING SURFACE RESTORED IAW SRI DT/S-6898/13-21040.SDR KPVA20140114008Skin · corrodedHEAVY MAINTENANCE, 2013. RT FUSELAGE SKIN BETWEEN FRAMES 14-15 BETWEEN STRINGER 10-11 AND FRAMES 15-16 BETWEEN STRINGER 9-10 CORRODED. REPAIRED IAW SRM 53-00-00, REPAIR 403.SDR KPVA20140114007Skin · crackedDURING HEAVY MAINTENANCE, PASSENGER DOOR TOP AFT INNER SKIN FOUND CRACKED. REPAIRED IAW SRM 52-11-00.SDR KPVA20140114006Intercostal · wornDURING HEAVY MAINTENANCE, PASSENGER DOOR INTERCOSTAL WORN. REPLACED INTERCOSTAL IAW SRM 51-25-01.SDR KPVA20140114003Floorbeam · corrodedDURING HEAVY INSPECTION. FLOORBEAM AT FRAME 39 CORRODED. SECTION REPLACED IAW SRM 53-00-00, REPAIR 455.SDR KPVA20140114002Floorbeam · corrodedDURING HEAVY MAINTENANCE. FLOORBEAM AT FRAME 38 CORRODED. SECTION REPLACED IAW SRM 53-00-00, REPAIR 456.SDR KPVA20140114001Floorbeam · corrodedDURING HEAVY MAINTENANCE. FRAME 26 FLOORBEAM LOWER FLANGE CORRODED BL 0. AREA BLENDED, HOLES REAMED AND OVERSIZED FASTENERS INSTALLEDIAW DT/S-6222/13-20906, ISSUE C.SDR MTNA20131111046Crease Beam · gougedFOUND GOUGES IN CREASE BEAM WEB, OUT OF LIMITS. REPLACED WEB IAW SRM.SDR MTNA20131111045Crease Beam · gougedFOUND GOUGES IN CREASE BEAM WEB OUT OF LIMITS. REPLACED WEB IAW SRM.SDR COEA2013112201821Skin Panel · corrodedEXTERNAL SKIN PANEL HAS SEVERAL SPOTS OF LEVEL 2 CORROSION BETWEEN FRAMES 14 - 16. REPAIR IAW SRAS DT S-6251 13 8077 DATED 11/21/2013.SDR MTNA110620130003Connector · contaminatedNR 1 ENGINE TORQUE DROPPED TO 0 PERCENT IN FLIGHT THE ACFT YAWED & ENGINE NOISE DROPPED. TROUBLESHOTING SYSTEM, FOUND CONNECTOR ON NR 1 MFCU, AFU AND EEC HAD OIL CONTAMINATION. CONNECTORS WERE CLEANED IAW MM 20-24-06. A POWER ASSURANCE RUN WAS ACCOMPLISHED SDR COEA2013112602821Fitting · crackedLEFT REAR SPAR END FITTING LOCATED JUST ABOVE THE CREASE BEAM IS CRACKED ON THE FWD SIDE OF FRAME 27. REPLACED WITH NEW OEM PART.SDR MTNA201311040001Brake Sys · contaminatedDURING TAXI, NORMAL BRAKING FOR BOTH LT AND RT PEDALS ON THE PILOT AND COPILOTS REQUIRES FULL PRESSURE ON BOTH PEDALS TO STOP THE ACFT. EMERGENCY BRAKES ARE ALSO WEAK. MECHANIC BLED BOTH LOW PRESSURE AND HIGH PRESSURE HYD SYSTEMS IAW JIC 32-42-00, BLD 10010SDR CA131007012Engine · smoke(CAN) SHORTLY AFTER TAKEOFF, A FIRE INDICATION OCCURRED FOLLOWED BY SMOKE IN THE CABIN. THE PILOT SHUT THE ENGINE DOWN AND THE FIRE INDICATION DISAPPEARED. THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. SDR MTNA10032013001Metering Valve · leakingON TAXIOUT, FLIGHT CREW FOUND THE F/O`S BRAKE PEDALS INEFFECTIVE. REPLACED BRAKE METERING VALVE IAW JIC 32-42-51. SYS CHECKRF GOOD IAW JIC 32-42-00.SDR MTNA092620130001Master Cylinder · leakingAFTER COMPLETION OF FLIGHT, F/O`S LEFT BRAKE BECAME INOPERATIVE. AFTER TROUBLESHOOTING, REPLACED F/O`S BRAKE MASTER CYLINDER IAW JIC 32-42-13, BRAKES BLED IAW JIC 32-42-00, CHECKED GOOD AND ACFT RETURN TO SERVICE.SDR COEA2013090609816Access Panel · corrodedDURING HEAVY CHECK, FUEL PANEL 521DT HAS FRETTING CORROSION ON UNDERSIDE OF PANEL. REPLACED PANEL WITH OEM PART.SDR COEA2013091111816Skin · corrodedDURING HEAVY, LT HORIZONTAL STAB L/E HAS CORROSION UNDER DEICE BOOT. BLENDED.SDR COEA2013082308805Unknown · odorCREW DECLARED AN EMERGENCY FOR THEIR APPROACH, DUE TO AN ODOR OF ELECTRICAL SMOKE. LANDED WITHOUT INCIDENT. COULD NOT DUPLICATESDR COEA2013091112816Access Panel · corrodedDURING HEAVY CHECK, LT WING ACCESS PANEL 521DT HAS FRETTING DAMAGE. REPAIR IAW SRAS DO/TS-3018/09, 5261, ISSUE C.SDR COEA2013091114816Access Panel · corrodedDURING HEAVY CHECK, LT WING ACCESS PANEL 522CT HAS FRETTING DAMAGE. REPAIR IAW SRAS DO/TS-3018/09, 5261, ISSUE C.SDR COEA2013091113816Access Panel · corrodedDURING HEAVY CHECK, RT WING ACCESS DOOR CUTOUT FOR PANEL 622CT HAS FRETTING DAMAGE. REPAIRED IAW SRAS DO/TS-3018/09, 5261, ISSUE C. MAJOR REPAIR.SDR COEA2013090507816Channel · crackedDURING HEAVY CHECK, RT ENGINE COWL 445AT INBD OUTER CHANNEL SECTION IS CRACKED. REPLACED WITH OEM PART.SDR COEA2013090406816Seat Track · damagedDURING HEAVY CHECK, LT INBD SEAT TRACK HAS WEAR DAMAGE WITH POSSIBLE CORROSION BETWEEN FR15 TO FR18. SPLICE REPAIR IAW SRM 53-00-00, FIG 454, REV 86.SDR COEA2013091115816Floor Support · crackedDURING HEAVY CHECK, RT CARGO LONGITUDINAL FLOOR SUPPORT IS CRACKED AT FR18. SPLICE REPAIR IAW EO 5315-02.SDR COEA2013090610816Web · corrodedDURING HEAVY CHECK, AFT CARGO DOOR THRESHOLD HAS CORROSION. REPLACED THRESHOLD WEB WITH OEM.
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