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 = '76' 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 = '76' 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 CA070621003Frame · separated(CAN) DURING TAXI PILOTS FELT THE RT WING DROP SUDDENLY AND HEARD A TIRE SKIDDING SOUND. THEY IMMEDIATELY STOPPED THE AIRCRAFT. MECHANICS FOUND THE LANDING GEAR A-FRAME HAD BROKEN FREE FROM THE MAIN LANDING GEAR TRUNNION. THE LANDING GEAR DID NOT COLLAPSE BUTSDR CA070621002Motor · contaminated(CAN) DURING APPROACH, PILOTS SELECTED LANDING GEAR DOWN, GEAR MOTOR CIRCUIT BREAKER POPPED AND GEAR WOULD NOT EXTEND. AN EMERGENCY EXTENSION WAS CARRIED OUT SATISFACTORILY. AFTER RETURN TO BASE MECHANICS FOUND THAT THE HYDRAULIC MOTOR WAS CONTAMINATED WITH HSDR CA070522006Control Cable · frayed(CAN) AIRCRAFT WAS IN THE HANGER FOR INSPECTION. AN INSPECTION WAS BEING STARTED IN THE AFT TAIL AREA. THE AME APPRENTICE NOTICED THE ELEVATOR TRIM CABLE SEVERELY FRAYED WHERE IT WRAPPED AROUND THE TRIM SERVO. THE CABLE WAS REMOVED AND REPLACED WITH A NEW PARTSDR CA070220007Shaft · fractured(CAN) MAIN LANDING GEAR ACTUATOR SHAFT FRACTURED AT LAST THREAD FARTHEST FROM ROD END BEARING JAM NUT. SHAFT BENT SLIGHTLY THROUGHOUT ITS FULL LENGTH WITH AN APPROXIMATELY 40 DEGREE BEND AT FRACTURE POINT. (TC NR 20070220007)SDR CA070129006Connector · disconnected(CAN) ADF INTERMITTENT NDB AND HEADING. AFTER SWAPPING RECEIVERS, ANTENNA, REPLACING ANTENNA TRAY AND CONNECTOR, REPLACING PINS IN RECEIVER TRAY, FOUND CO-AX CONNECTOR INNNER CORE TOUCHING SHIELDING AT RECEIVER TRAY. SNAG ONLY APPREARED WHEN WIRING HARNESS WASSDR 2007FA0000033Starter · intermittentREPEATED TRYS, BENDIX FAILED TO ENGAGE. LUBRICATED AND INSPECTED BENDIX, FAILS TO ENGAGE EVERY OTHER TIME. IT STARTS (1) TIME THEN FAILS. (K)SDR CA061108006Connector · contaminated(CAN) DURING TRAINING IN IMC CONDITIONS, ATC REPORTED TO STUDENT THAT HE WAS WAY OFF TRACK, PILOT CONFIRMED THAT HSI SYSTEM HAD FAILED. AIRCRAFT RETURNED TO BASE WITH HELP FROM ATC WITH NO OTHER INCIDENCE. MAINTENANCE DUPLICATED DEFECT, HSI SYSTEM INSPECTED ANSDR 2006FA0000946Attach Angle · brokenBOTH LT AND RT ENGINE MOUNTS TO FIREWALL ATTACH POINTS BROKE OUT AFT OF THE FIREWALL IN THE UPPER OB POINT. THIS BREAKAGE IS DIFFICULT TO DETECT DUE TO VISIBILITY ACCESS. THESE BRACKETS BROKE BECAUSE OF FLIGHT THROUGH TURBULENCE. (K)SDR 2006FA0000945Mount · brokenBOTH LT AND RT ENGINE MOUNT TO FIREWALL ATTACH POINTS BROKE OUT AFT OF THE FIREWALL IN THE UPPER OB POINT. THIS BREAKAGE IS DIFFICULT TO DETECT DUE TO VISIBILITY ACCESS. THESE BRACKETS BROKE BECAUSE OF FLIGHT THROUGH TURBULENCE. (K)SDR 2006FA0000644Frame · corrodedA-FRAME TUBE ASSY FAILED AT CORROSION PREVENTION PORT CAUSING LT MAIN GEAR COLLAPSE. (K)SDR 2006FA0000617Frame · crackedCRACK IN RT FWD WING BOLT ATTACH FRAME, P/N: 105-420011-6.SDR 2006FA0000616Frame · crackedCRACK IN RT FWD WING BOLT ATTACH FRAME, P/N: 105-420011-6.SDR 2006FA0000615Frame · crackedCRACK IN RT FWD WING BOLT ATTACH FRAME, P/N: 105-420011-6.SDR 2006FA0000614Frame · crackedCRACK IN RT FWD WING BOLT ATTACH FRAME, P/N: 105-420011-6.SDR 2006FA0000613Frame · crackedCRACK IN RT FWD WING BOLT ATTACH FRAME, P/N: 105-420011-6.SDR 2006FA0000612Frame · crackedCRACK IN RT FORWARD WING BOLT ATTACH FRAME, P/N: 105-420011-6.SDR CA060410009Channel · crackedDISCOVERED DURING INSPECTION. NLG ACTUATOR ATTACH BRACKET WAS FOUND CRACKED FROM THE EDGE OF THE BRACKET, THROUGH A LIGHTENING HOLE AND OUT THE OTHER SIDE. THE AREA IS DIFFICULT TO INSPECT. THIS IS THE SUPPORT CHANNEL THAT THE UPPER END OF THE NLG ACTUATOR SDR AU510002202Plug · cracked(AUS) NOSE LANDING GEAR ACTUATOR END PLUG CRACKED IN AREA OF SPANNER FLATS. LOSS OF HYDRAULIC FLUID. (CASA NR 510002202)SDR AU510002074Points · unserviceableRT MAGNETO CONTACT BREAKER POINT LOOSE ON SPRING ASSEMBLY. CONTACTS HAD BEEN REPLACED APPROXIMATELY 13 HOURS PREVIOUSLY. SUSPECT BREAKER INCORRECTLY SWAGED ONTO SPRING.SDR AU510001792Piston Ring · delaminated(AUS) ENGINE PISTON TOP COMPRESSION RINGS EXHIBITED SLIGHT SIGNS OF DELAMINATION. ENGINE OIL VERY DIRTY. PREMATURE WEAR ALSO FOUND ON EXHAUST VALVE ROTATING CAPS. (CASA NR 510001792)SDR AU510001756Piston Ring · deteriorated(AUS) ENGINE OIL FOUND TO BE VERY BLACK. INSPECTION FOUND THE PLASMA COATING ON THE TOP PISTON RINGS ON ALL FOUR CYLINDERS FRACTURED. (CASA NR 510001756)SDR AU510001510Bracket · crackedRT ENGINE FIREWALL BRACKET CRACKED ON BOTH SIDES OF ANCHOR NUT. FOUND DURING INSPECTION IAW AD/BEECH76/10-2.SDR AU510001482Spar · cracked(AUS) RT AILERON UPPER DOUBLER AND SPAR CRACKED. CRACK LENGTHS 10MM (0.39IN) IN DOUBLER AND 5MM (0.196IN) IN SPAR. (CASA# 510001482)SDR AU510001469Bracket · cracked(AUS) LH AND RH AILERONS PNO 105-130000-1 (LH) AND PNO 105-130000-2 (RH) SPARS AND DOUBLER BRACKETS CRACKED AT PUSHROD SUPPORT BRACKETS. (CASA# 510001469)SDR AU510001460Spar · cracked(AUS) LT AND RT AILERONS PNO 105-130000-1 (LT) AND PN 105-130000-2 (RT) SPARS AND DOUBLER BRACKETS CRACKED AT PUSHROD SUPPORT BRACKETS. (CASA# 510001460)SDR AU510001458Structure · cracked(AUS) LT AND RT AILERONS PNO 105-130000-1 (LT) AND PN 105-130000-2 (RT) SPARS AND DOUBLER BRACKETS CRACKED AT PUSHROD SUPPORT BRACKETS. FLEET INSPECTION FOUND SIMILAR CRACKING ON FOUR OF SEVEN AIRCRAFT. (CASA# 510001458)SDR CA050711004Spark Plug · crackedDURING ROUTINE SCHEDULED 100 HR, 1 SPARK PLUG APPEARED BENT WHILE INSTALLED IN CYLINDER. UPON REMOVAL, CONFIRMED BY INSPECTION THAT SPARK PLUG BODY HAD SEPARATED AT NECKED DOWN AREA OF METAL BODY OF PLUG ON IGNITION LEAD SIDE OF GASKET SEALING SURFACE. AFFECTSDR CA060509005Powerpack · failed(CAN) LANDING GEAR FAILED TO EXTEND. CREW ACTIVATED EMERGENCY EXTENSION. STILL NO INDICATION ON RT GEAR POSITION. SWITCHED BULBS ON GEAR INDICATOR AND DISCOVERED ONE BULB U/S. LANDING CARRIED OUT NORMALLY. FOUND HYDRAULIC POWER PUMP MOTOR BRUSHES WORN. RSDR AU510001633Line · chafedENGINE FUEL LINE CHAFED AND WORN BY THROTTLE CABLE. LOSS OF APPROXIMATELY 5 GALLONS OF FUEL. THROTTLE CABLE HAD BEEN RECENTLY REPLACED.SDR AUS20040470Landing Gear · collapsed(AUS) DURING INSPECTION OF NOSE LANDING GEAR FOR A NOSE LANDING GEAR FAULT, THE NLG COLLAPSED, TRAPPING THE AME BETWEEN THE NOSE CONE AND THE GROUND. DUE TO THE QUICK REACTION OF WORKMATES, THE AME WAS RELEASED FROM BENEATH THE AIRCRAFT AND ADMITTED TO HOSPITASDR DFJ2004F00000Fitting · leakingFOUND PROPELLER GOVERNOR OIL LINE FITTING LEAKING OIL. CAUSED WHITE SMOKE IN FLIGHT DUE TO OIL LEAKING ON EXHAUST. POSSIBLE CAUSE, FITTING NOT PROPERLY TORQUED AT PROPER GOVERNOR OVERHAUL. RECOMMEND CHECKING TORQUE OF FITTING ON INSTALLATION OF PART.SDR AUS20040064Connector · contaminated(AUS) RT ENGINE INSTRUMENT CLUSTER CONNECTOR CONTAMINATED.SDR AUS20040056Damper · faulty(AUS) NOSE WHEEL SHIMMY DAMPER END CAP RETAINING CIRCLIP MISSING.SDR AUS20040033Motor · faulty(AUS) LANDING GEAR HYDRAULIC PUMP ELECTRIC MOTOR FAULTY. INVESTIGATIONFOUND BROKEN WIRE IN THE MOTOR WINDINGS.SDR AUS20040007Rotor · faulty(AUS) RT ENGINE MAGNETO ROTATING MAGNETIC SLIPPED ON SHAFT BY APPROXIMATELY 25 DEGREES.SDR AUS20031256Valve Guide · worn(AUS) NR 1 CYLINDER EXHAUST VALVE AND VALVE GUIDE WORN EXCESSIVELY. VALVE NOT SEATING CORRECTLY. FOUND DURING INSPECTION IAW AD/ENG/4 AMDT8.SDR YHLR200300001Lead · unbondedFOUND MOD-17 NOT PERFORMED IAW SB VHF251-SB17. GROUND STRAP FROM ANTENNA CONNECTOR P2 TO GROUND PLANE OF POWER AMPLIFIER ASSEMBLY A3. 2A(2) WAS NOT ACCOMPLISHED. UNIT HAD BEEN MARKED FOR MOD-17, AND WAS TAGGED BY REPAIR STATION, DATED 11/05/2002. MOD-17 COMPLESDR AUS20030982Rib · corroded(AUS) LT AND RT TRAILING EDGE FLAP SUPPORT RIBS CORRODED AT HINGE BRACKETS. MINOR EXTERNAL CORROSION ON FLAPS RESULTED IN FLAPS BEING DESKINNED AND INSPECTED UPON WHICH THE SERIOUS INTERNAL CORROSION WAS FOUND.SDR AUS20030981Rib · corroded(AUS) LT AND RT TRAILING EDGE FLAP SUPPORT RIBS CORRODED AT HINGE BRACKETS. MINOR EXTERNAL CORROSION ON FLAPS RESULTED IN FLAPS BEING DESKINNED AND INSPECTED UPON WHICH THE SERIOUS INTERNAL CORROSION WAS FOUND.SDR AUS20030980Rib · corroded(AUS) LT AND RT TRAILING EDGE FLAP SUPPORT RIBS CORRODED AT HINGE BRACKETS. MINOR EXTERNAL CORROSION ON FLAPS RESULTED IN FLAPS BEING DESKINNED AND INSPECTED UPON WHICH THE SERIOUS INTERNAL CORROSION WAS FOUND.SDR AUS20030979Rib · corroded(AUS) LT AND RT TRAILING EDGE FLAP SUPPORT RIBS CORRODED AT HINGE BRACKETS. MINOR EXTERNAL CORROSION ON FLAPS RESULTED IN FLAPS BEING DESKINNED AND INSPECTED UPON WHICH THE SERIOUS INTERNAL CORROSION WAS FOUND.SDR AUS20030958Rib · corroded(AUS) LT AND RT TRAILING EDGE FLAP SUPPORT RIBS CORRODED AT HINGE BRACKETS. MINOR EXTERNAL CORROSION ON FLAPS RESULTED IN FLAPS BEING DE-SKINNED AND INSPECTED UPON WHICH THE SERIOUS INTERNAL CORROSION WAS FOUND.SDR AUS20030957Rib · corroded(AUS) LT AND RT TRAILING EDGE FLAP SUPPORT RIBS CORRODED AT HINGE BRACKETS. MINOR EXTERNAL CORROSION ON FLAPS RESULTED IN FLAPS BEING DE-SKINNED AND INSPECTED UPON WHICH THE SERIOUS INTERNAL CORROSION WAS FOUND.SDR AUS20030937Hub · unserviceable(AUS) PROPELLER HUB DAMAGED IN AREA OF PRELOAD PLATE SHELF. PROPELLER HAD BEEN REMOVED AND DISMANTLED FOLLOWING GROUND STRIKE.SDR AUS20030881Hinge · corroded(AUS) RUDDER HINGE BRACKET CORRODED (RUSTED).SDR AUS20030783Actuator · cracked(AUS) NOSE LANDING GEAR ACTUATOR CRACKED AND LEAKING. INVESTIGATION FOUND A CRACK IN THE CYLINDER BODY END CAP THREAD ROOT LOCATED APPROXIMATELY THREE THREADS FROM THE SEALING CHAMFER.SDR AUS20030550Heater · miswired(AUS) HEATER INCORRECTLY WIRED. INVESTIGATION FOUND THAT THE OVERHEAT CUTOUT AND COMBUSTION PRESSURE SWITCH HAD NOT BEEN WIRED UP. THIS ALLOWED THE HEATER TO SOURCE FUEL AND IGNITION WITHOUT AIRFLOW AND OVERHEAT PROTECTION.SDR 2002FA0001370Pin · looseAIRCRAFT TAXIED TO A PARKING SPOT AFTER LANDING. THE NOSE GEAR PIN ROTATED IN THE GEAR LEG CAUSING AN INTERFERENCE WITH THE DOWN LOCK HOOK TO ENGAGE WITH THE PIN, NOT ALLOWING THE NOSE GEAR TO BE DOWN AND LOCKED. THE DOWN LOCK HOOK ENGAGES TO THE FLAT OF THE DSDR 2002FA0001289Frame · crackedTHE LEFT FRAME WAS NOTED TO HAVE CORROSION PREVENTATIVE OOZING IN THE EXACT AREA OF THE INSPECTION, IN A LINE THAT APPEARED AS A CRACK. THE AREA WAS CLEANED AND A CRACK WAS APPARENT BY USING A GOOD LIGHT AND 10 POWER GLASS. A DYE CHECK OF THE AREA FAILED TO SDR AUS20021276Frame · cracked(AUS) LT MAIN LANDING GEAR ``A`` FRAME CRACKED. FOUND DURING INSPECTION IAW AD/BEECH76/18 AMDT1.
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