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 COEA2015032607805Skin · chafedHEAVY CHECK MAJOR REPAIR. LT WING LOWER SKIN IS CHAFED AT RIB 13 FLAP BEAM. REPAIRED IAW SRAS ACFT MSN 372 392 ISSUE C DATED 9 25 15 SUPERSEDES ISSUE B. REPAIR IS PERMANENT WITH NO DTI.SDR COEA2015032601821Ahrs · failedAIR TURN BACK, DISCREPANCY. DURING CLIMB OUT, THE AHRU FAILED. THE CREW ELECTED TO RETURN, NO EMER DECLARED & ACFT LANDED SAFELY. REPLACED THE CAPTAIN'S AHRU. ACFT RETURNED TO SERVICE.SDR COEA2015032415805Frame · crackedWO 144800 NR 200012 HEAVY CHECK COE & MINOR REPAIR. LT FRAME 5 JUST BELOW NODE 6 JUNCTION, WEB TO INBD FLANGE RADIUS CRACKED. REPLACED WITH OEM PART.SDR COEA2015032410805Fitting · chafedHEAVY CHECK MAJOR REPAIR. LT WING RIB 13 FLAP HINGE ARM OTBD FITTING HAS CHAFING DAMAGE CAUSED BY THE GROUNDING WIRE. OUT OF LIMITS IAW SRM 51-10-10 REV 91. REPAIR IAW SRAS DT S 1797/15 9206 ISSUE B 4 23 2015.SDR COEA2015032409805Fitting · chafedHEAVY CHECK MAJOR REPAIR. RT WING RIB 13 FLAP HINGE ARM INBD FITTING HAS CHAFING DAMAGE CAUSED BY THE GROUNDING WIRE. OUT OF LIMITS OF SRM 51-10-10 REV 91. REPAIR IAW SRAS DT S 1797 15 9207 ISSUE B DATED 4 23 2015.SDR COEA2015032306805Skin · corrodedHEAVY CHECK MAJOR REPAIR. LT UPPER WING PANEL LANDING 522CT HAS FRETTING. REPAIR IAW SRAS DO TS 1529 05 3169 ISSUE E DATED 4 17 15.SDR COEA2015032305805Skin · corrodedHEAVY CHECK MAJOR REPAIR. RT UPPER WING PANEL LANDING 622CT HAS FRETTING & TOOLING DAMAGE. REPAIR IAW SRAS DO TS 1529 05 3169 ISSUE E DATED 4 17 15.SDR COEA2015032214805Floorbeam · corrodedHEAVY CHECK MINOR REPAIR. FLOORBEAM 36 HAS LEVEL 2 CORROSION AT THE SCREW HOLES IN MULTIPLE LOCATIONS. REPLACED WITH OEM PART.SDR COEA2015032213805Floorbeam · corrodedHEAVY CHECK MINOR REPAIR. FLOORBEAM 39 HAS LEVEL 2 CORROSION AT THE SCREW HOLES IN MULTIPLE LOCATIONS. REPLACED WITH OEM PART.SDR COEA2015032212805Doubler · corrodedHEAVY CHECK MINOR REPAIR. LT FRAME 39 FWD DOUBLER HAS LEVEL 2 CORROSION AT THE LEVEL OF THE AFT CARGO THRESHOLD. REPLACED WITH OEM PART.SDR COEA2015032204805Crease Beam · corrodedHEAVY CHECK MINOR REPAIR. RT CREASE BEAM WEB FRAME 16 - 17 HAS LEVEL 2 CORROSION. REPLACED WITH OEM WEB.SDR COEA2015032202805Stanchion · corrodedHEAVY CHECK COE, MINOR REPAIR. RT STANTION FRAME 13 HAS LEVEL 2 CORROSION AT THE LOWER END. REPLACED WITH OEM PART.SDR COEA2015031901819Unknown · malfunctionedAIR TURN BACK, DISCREPANCY, DURING CLIMB OUT, THE CREW EXPERIENCED A TORQUE FLUCTUATION ON THE NR 2 ENG CAUSING THE ACFT TO YAW BACK & FORTH. THE CREW RETURNED THE ACFT BACK. NO EMER WAS DECLARED. PERFORMED ENG RUNS TO TRY & FIND THE ISSUE, BUT COULD NOT DUSDR COEA2015031101805Warning Light · false activationAIR TURN BACK DISCREPANCY. DURING INITIAL CLIMB OUT, THE ACFT CARGO DOOR UNLOCK LIGHT ILLUMINATED. THE ACFT RETURNED. OPENED & VISUALLY INSPECTED REAR CARGO DOOR. OPERATIONS CHECKED GOOD IAW AMMS 52-11-00. ACFT RETURNED TO SERVICE.SDR COEA2015030502801Block · faultyAIR TURN BACK DISCREPANCY, AFTER GEAR RETRACTION, THE FLAP UNLOCK WARNING ILLUMINATED & DID SO DURING CLIMB OUT. THE CREW ELECTED TO RETURN BACK. NO EMER WAS DECLARED. REPLACED THE FLAP VLV BLOCK. OPERATIONS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR COEA2015021803807Computer · malfunctionedFLIGHT 8234, WHEN CREW EXTENDED THE LT MLG, THE UNLOCK LIGHT ILLUMINATED ON LT MAIN PRIMARY & SECONDARY WENT OFF AT 4 - 5 SEC AFTER FREE FALL. ATTEMPTED THE GRAVITY ASSISTED PROCEDURES & WAS ABLE TO OBTAIN A FULL LOCKED GEAR INDICATION. AN EMERGENCY WAS NOTSDR COEA2015012302807Proximity Switch · out of adjustWHILE ON FLIGHT TO TEST GEAR FOR PREVIOUS LG DISCREPANCY, SDR COEA2015012101807, THE GEAR RETRACTED WITHOUT A PROBLEM. WHEN THE GEAR WAS PUT DOWN FOR LANDING, THE LT MAIN GEAR INDICATIONS DID NOT INDICATE DOWN & LOCKED. THE CREW ATTEMPTED TO USE THE EMER EXTSDR CA150126007Fastener · sheared(CAN) DURING RT FLIGHT DECK WINDOW REPLACEMENT MAINTENANCE DISCOVERED A FAILED LOCK FASTENER IN THE CENTRE POST AREA, BOTTOM ONE. THE HEAD OF THE PIN WAS SHEARED OFF. MAINTENANCE VISUALLY INSPECTED THE AREA WITH NO VISIBLE CRACKS. THE FASTENER WAS REPLACED BY SDR COEA2015012101807Actuator · failedON APPROACH, THE LG WOULD NOT EXTEND NORMALLY. THE LT MLG UNLOCK LIGHT REMAINED ILLUMINATED. THE CREW PERFORMED THE EMER LG GRAVITY EXTENSION PROCEDURE IAW THE QRH & THE PROCEDURE WAS SUCCESSFUL. DID NOT DECLARE AN EMER. TROUBLE SHOT & REPLACED THE LT MAINSDR COEA2015011401801Controller · faultyON CLIMB OUT, APPROACHING 11000FT, THE ACFT EXPERIENCED A LOSS IN CABIN PRESSURE. THE CREW SWITCHED TO MANUAL MODE & WAS UNABLE TO PRESSURIZE THE ACFT. AN EMER DESCENT WAS COMPLETED TO 10000 FT & A RETURN INITIATED DUE TO THE DEPRESSURIZATION. NO EMER WAS DSDR COEA2014010606819Door · detachedDURING POST FLIGHT INSPECTION, RIGHT MLG DOOR DETACHED FROM ACFT DURING TAXI IN, CAUSING GOUGE IN PANEL 194CR, RT MAIN GEAR DOOR, PANEL & ALL OTHER DAMAGED AREAS WERE REPLACED IAW JIC 52-81-00 RAI 10000 002. PERFORMED LG NORMAL, EMER TEST & OPERATIONS CHECKSDR COEA2014122401821Door · unsecureDURING DEPARTURE, AFTER GEAR UP, THE AFT CARGO DOOR UNLOCK WARNING LIGHT ILLUMINATED. THE CREW RETURNED & BLOCKED BACK INTO THE RAMP. NO EMER DECLARED. MX INSPECTED & SECURED THE CARGO DOOR. OPERATIONS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR COEA2014120310803Wire · chafedAIR TURN BACK. ON DEPARTURE DURING CLIMB, THE NR 1 ACW GEN FAULTED. THE QRH WAS CONSULTED & THE CREW ELECTED TO RETURN. NO EMER WAS DECLARED. THE ACFT LANDED WITHOUT INCIDENT. DUE TO ICING CONDITIONS ENROUTE THE ACW GEN WAS NOT DEFERRABLE. AFTER EXTENSIVESDR CA141204006Engine · fire(CAN) THE FIELD SERVICE REPRESENTATIVE RECEIVED TODAY A REPORT OF A LEFT ENGINE FIRE FOLLOWED BY IN FLIGHT SHUT DOWN (IFSD) DURING CLIMB. THE PILOT DISCHARGED BOTH FIRE EXTINGUISHERS AND PERFORMED AN EMERGENCY LANDING WITHOUT FURTHER INCIDENT. ONLY LIMITED DETSDR COEA2014111307801Switch · failedAIR TURN BACK. ON REACHING CRUISE ALTITUDE, THE ACFT LOST PRESSURIZATION. ELECTED TO RETURN. NO EMERGENCY WAS DECLARED. ACFT LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING, IT WAS DETERMINED THAT THE CABIN PRESSURIZATION WORKED NORMALLY WHEN NR 1 ENGINE SDR COEA2014102709803Contactor · faultedSHORTLY AFTER TAKEOFF THE NR 1 ACW GEN FAULTED & WOULD NOT RESET. DUE TO ICING CONDITIONS, THE ACFT WAS RETURNED, NO EMER WAS DECLARED. AFTER TROUBLESHOOTING, MAINTENANCE WAS ABLE TO GET THE GEN BACK ONLINE BY REPLACING THE NR 1 ACW CONTACTOR. OPERATIONS CHESDR COEA2014101002805Sensor · faultyFLIGHT BLOCKED OUT, ONCE AIRBORNE, THE MASTER CAUTION ILLUMINATED WITH THE NR 1 DC GEN FAULT. THE CREW ELECTED TO RETURN, NO EMER WAS DECLARED. REPLACED THE HOT HALL EFFECTS SENSOR & NR 1 ENG DC GEN CONTACTOR. OPERATIONS CHECKED GOOD. ACFT RETURNED TO SERVSDR COEA2014100208803Frame · damagedWORK ORDER 139727 NR 2 HEAVY CHECK POST CHECK INSPECTION COE & MAJOR REPAIR. EDGE DAMAGE TO RT FRAME 13 INNER FLANGE ABOVE STRINGER 12. REPAIR IAW SRAS DT S-5916 14 8742 DATED 10/6/2014.SDR MTNA201409290001Seal · leakingAFTER ACFT DEPARTED AND PASSING 18,000 FEET, THE CABIN ALTITUDE BEGAN INCREASING. BY 19000 FEET THE CREW RECEIVED A CONTINUOUS REPETITIVE CHIME MASTER WARNING ALERT. ATTEMPTS TO RECOVER THE PRESSURIZATION WERE UNSUCCESSFUL. THE CREW COMPLETED THEIR QRH PROCSDR MTNA20140923017Pan · dentedFOUND DENT IN AFT CARGO DOOR LOWER PAN PN S52176204202. REPAIRED DENT IAW DWG 72R7001-02 DATED 9/5/14.SDR COEA2014090806803Panel · corrodedWORK ORDER 137960 NR 500025. HEAVY CHECK COE, MAJOR REPAIR. PANEL 521DT FOIL HAS FRETTING. REPAIR IAW DO TS 4828 10 6020 ISSUE B DATED 9/22/14.SDR COEA2014090804803Housing · corrodedWORK ORDER 137960 NR 600017. HEAVY CHECK COE, MAJOR REPAIR. RT CTR WING ACCESS PANEL HOUSING FOR PANEL 622CT HAS FRETTING. REPAIR IAW DOTS 4828 10 6020 ISSUE B DATED 9/22/14.SDR CA140910005Smoke Detector · faulty(CAN) ON THE GROUND, THE AFT SMOKE WARNING CARGO LIGHT CAME ON FLIGHT ATTENDANT PANEL. RESET OF AIRCRAFT, POWER OFF 7.5 MINS. COULD NOT RESET WARNING. THE AFT SMOKE DETECTOR WAS REPLACED AND SYSTEM TESTED SERVICEABLE.SDR COEA2014090405803Skin · galledWORK ORDER 137960 NR 500017. HEAVY CHECK COE, MAJOR REPAIR. LT CTR WING FEEDER TANK ACCESS DOOR CUT OUT HAS GALLING. REPAIR IAW DOTS 4828 10 6020 ISSUE B DATED 9/22/14.SDR COEA2014090203803Stringer · damagedWORK ORDER 137960 NR 200010. HEAVY CHECK COE, MAJOR REPAIR. STRINGER 7A AT FRAME 20 RT HAS TOOLING DAMAGE. STRINGER SPLICE BETWEEN FRAME 19 - 21 IAW SRM 53-00-00 REPAIR 422.SDR COEA2014083007803Skin · peelingWORK ORDER 137960 NR 500004 HEAVY CHECK COE MAJOR REPAIR. LT WING HAS TWO SPOTS OF COMPOSITE PEELING ON THE LOWER SURFACE NEAR THE LE, OTBD OF RIB 19 & INBD OF RIB 21. REPAIR IAW SRAS DT S-5621 4 8730 DATED 9/30/14.SDR COEA2014081901805Indicator · faultyAIR TURN BACK, DURING CLIMB OUT, THE CREW NOTICED THE LT FUEL QTY INDICATOR ACTING ERRATICALLY, SHOWING A RAPID DECREASE IN THE AMOUNT OF FUEL ONBOARD. AFTER LEVELING OFF, THE INDICATED FUEL LEVEL CONTINUED TO DROP, EVENTUALLY DISPLAYING ZERO, AT WHICH TIME TSDR MTNA070720140001Filter · leakingDURING FLIGHT, THE BLUE HYD SYSTEM LOW LEVEL INDICATION LIGHT ILLUMINATED. 30 MINUTES LATER THE GREEN SYS INDICATION LIGHT ILLUMINATED. THE CREW DECLARED AN EMERGENCY & THE ACFT LANDED SAFELY. AFTER TROUBLESHOOTING THE ACOUSTIC FILTER IT WAS FOUND TO HAVESDR MTNA201407070002Filter · leakingDURING TAXI OUT, COPILOTS LEFT BRAKE PRESSURE WAS INSUFFICIENT. THE CREW TAXIED THE ACFT BACK TO THE RAMP. REPLACED THE HYD ACOUSTIC FILTER AT 9GXA IAW ATR-72JIC 29-10-00 RAI 10080. THE SYS CHECKED GOOD. THE BRAKE LOW PRESSURE LINE WAS BLEED IAW JIC 32-4SDR COEA2014071103807Panel · corrodedRIGHT UPPER WING PANEL 623GT HAS LEVEL 2 CORROSION ON MATING SURFACE. REPLACED WITH NEW PART.SDR COEA2014071102807Panel · corrodedRIGHT UPPER WING FUEL ACCESS DOOR CUT OUT FOR PANEL 622CT & ASSOCIATED FOIL ON PANEL 622CT BOTH HAVE FRETTING DAMAGE. REPAIR IAW SRAS DO & TS-3854 07, 4243 ISSUE D DATED 7/10/2014.SDR COEA2014061701807Structure · crackedTHE FWD CARGO DOOR FWD LATCH FITTING & INNER SKIN WERE FOUND CRACKED UNDER THE LOWER LATCH LOCK MECHANISM FWD BEARING MOUNT ASSEMBLY. REPLACE WITH OEM PARTS.SDR COEA2014053001803Heat Exchanger · crackedSMOKE IN CABIN & AFW. DISCREPANCY, WHILE RUN & TAXI TRAINING WAS BEING CONDUCTED, THE CABIN WAS DISCOVERED TO BE FULL OF SMOKE. THE ACFT WAS SHUT DOWN. THE FIRE DEPARTMENT WAS NOTIFIED & THE THREE OCCUPANTS EGRESSED THE AIRPLANE. THE FWD & AFT DOORS WERE OSDR KPVA20140626003Rib · crackedDISCREPANCY, LT INBD FLAP CAM GUIDE NR 2 FROM INBD HAS EXCESSIVE MOVEMENT, ZONE 8. RIB 3 IS CRACKED & WILL NEED TO BE REPLACED. REMOVED UPPER SKIN ON FLAP IAW SRM 51-25-03. REMOVED BROKEN RIB, LOCATED & DRILLED NEW RIB IAW SRM 51-25-03 & 51-25-01. INSTALLESDR MTNA042220140001Autofeather Sys · malfunctionedDURING CRUISE, NR 1 ENGINE NP DROPPED TO 30 PERCENT, TORQUE DROPPED TO ZERO, ALL OTHER ENGINE PARAMETERS WERE NORMAL. DECLARED AN EMERGENCY & MADE A UNEVENTFUL LANDING. REPLACED THE NR 1 AUTO FEATHER UNIT. THE SYS CHECKED GOOD IAW MM JIC 61-22-00 OPT 10010SDR KPVA20140421001Autofeather Sys · faultyENGINE NR 2 AUTO FEATHERED DURING CLIMB FROM LNY, NO UP TRIM OBSERVED. DIVERTED TO OGG & LANDED WITH NO FURTHER INCIDENT. R & R NR 2 AFU UNIT IAW MM 720110 SEC 7 PARA AB. NO OP TRIMMED NR 2 ENG IAW JIC 73-2361OPT 10040, RAN UP NR 2 ENG IAW JIC 72-00-00 ERU SDR MTNA201404120001Master Cylinder · failedDURING TAXI, THE COPILOT'S LT BRAKE PEDAL BOTTOMS OUT WITH MINIMAL BRAKE PRESSURE. THE MECHANIC REPLACED THE MASTER CYLINDER IAW JIC 32-42-13, RAI 1000. THE SYSTEM CHECKED GOOD AND THE ACFT WAS RETURN TO SERVICE.SDR MTNA20140127004Support Fitting · wornLEFT WING FLAP BEAM LATERAL LINK FITTING LUG, OVERSIZED AT RIB 13. LUG OVERSIZED AND BUSH INSTALLED IAW SRI DT/S-223/14-21209.SDR MTNA201401140001Circuit Board · burnedDURING APPROACH, HAD ELECTRICAL BURNED ODOR IN COCKPIT. SYSTEM LIGHT ON FOR FDR CAME ON. FOUND CIRCUT BRAKERS FDAU/DFDR FLIGHT SUPPLY, FDAU/DFDR GROUND SUPPLY TRIPPED. INTERNAL COMPONENT THAT CAUSED THE BURNED ODOR IS PCB OF THE FDAU.SDR COEA2014013005819Door Frame · crackedPREVIOUS REPAIR IN THE FWD CARGO DOOR FRAME IS CRACKED ON THE UPPER END OF THE SECOND FROM AFT FRAME. REPAIRED IAW SRM 52-31-00 REPAIR 411.
Back to Aerospatiale ATR 72-212