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 = '402C' 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 = '402C' 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 HYIA20130316001Spar · damagedDAMAGE WAS DISCOVERED ON THE FRONT UPPER SPAR CAP. OPENSDR HYIA20130308002Spar · crackedDURING A SCHEDULED MX EVENT, CRACKS WERE NOTED IN THE FORWARD AND AFT SPAR WEBS ON THE REAR SPAR. DAMAGE WAS LOCATED AT FLOOR SUPPORT ATTACH POINTS. ENGINEERING WAS REQUESTED AND RECEIVED AND REPAIRS ARE CURRENTLY UNDERWAY.SDR HYIA20130308001Spar Cap · crackedDURING A SCHEDULED MX EVENT CRACKS FOUND ON THE REAR SPAR WEB CRACKS AT FLOOR SUPPORT LOCATIONS. THERE WERE ALSO 5 MISS DRILLS IN THE TOP OF THE REAR SPAR THAT WERE NOTED. AFTER REVIEWING ENGINEERING REPAIR OPTIONS, THE DECISION WAS MADE TO REPLACE REAR SPAR SDR HYIA20130306001Switch · failedDURING CRUISE FLIGHT, CREW NOTICED A BURNING ODOR IN COCKPIT AND A SMALL AMOUNT OF HAZE OR SMOKE. DIVERTED AND MADE AN UNSCHEDULED LANDING. ON MX INSPECTION, AVIONICS MASTER SWITCH WAS FOUND DEFECTIVE. SWITCH R & R IAW MM.SDR HYIA20140414047Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20140414046Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20130213001Wire · chafedPILOT REPORTED THAT DURING CRUISE, SMOKE WAS NOTICED IN THE COCKPIT. AS A PRECAUTION THE PILOT ELECTED TO DEACTIVATE ELECTRICAL SYSTEMS AFTER DECLARING AN EMERGENCY. SAFELY LANDED AT DESTINATION. UPON MX INSPECTION, A WIRE WAS FOUND TO HAVE BEEN CHAFED BETWSDR HYIA20140414045Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414044Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20130124002Spar · damagedDURING A REGULARLY SCHEDULED MX EVENT, DAMAGE WAS DISCOVERED ON THE REAR SPAR WEBS IN BOTH FORWARD AND AFT POSITIONS. DAMAGE WAS MAPPED AND SENT. REPAIRS WERE CARRIED OUT IAW REPAIR PLANS SUPPLIED AND SUBSTANTIATED.SDR HYIA20130124001Spar · crackedDURING A SCHEDULED MX EVENT, CRACKS WERE DISCOVERED ON THE REAR SPAR WEBS FORWARD AND AFT AT FLOOR ATTACH POINTS. DAMAGE WAS MAPPED AND SENT. REPAIRS WERE CARRIED OUT IAW REPAIR PLANS SUPPLIED AND SUBSTANTIATED.SDR HYIA20120118002Governor · inoperativePILOT REPORTED THAT WHEN REDUCING POWER WHILE TRANSITIONING FROM CLIMB TO CRUISE, THE LT ENGINE PROPELLER RPM STAYED AT FULL RPM AND WOULD NOT REDUCE. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT. AFTER MX INSPECTION, THE DISCREPANCY WAS UNABLE TO BE SDR HYIA20130118001Turbocharger · failedPILOT REPORTED A GRADUAL POWER LOSS, ACCOMPANIED BY PARTIAL ENGINE STUTTER DURING FLIGHT IN THE RT ENGINE. THE PILOT LANDED SAFELY AT PLANNED DESTINATION AIRPORT AND BROUGHT THE ACFT IN FOR MX. UPON INSPECTION, THE ENGINE WAS FOUND TO BE EMPTY OF OIL. AS THSDR HYIA20140414043Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414042Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414041Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20121225001Caliper · inoperativePILOT REPORTED THAT DURING LANDING ROLLOUT, THE ACFT PULLED TO THE LT WHEN THE BRAKES WERE APPLIED. AFTER RELEASING BRAKE PRESSURE, THE RT BRAKE WAS APPLIED BY ITSELF WITH NO RESPONSE. THE PILOT WAS ABLE TO SAFELY STOP THE ACFT AND TAXI OFF THE RUNWAY. UPONSDR HYIA20121221001Governor · overspeedPILOT REPORTED THAT ON CLIMBOUT, THE RT PROP BECAME UNCONTROLLABLE AND WOULD OVERSPEED. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT. UPON MX INSPECTION, THE RT PROP AND PROP GOVERNOR WERE REPLACED IAW MM CHAPTER 61. THE PROP OPS AND LEAK CHECKED GOSDR HYIA20140414040Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20121220001Relay · shortedPILOT REPORTED THAT SHORTLY AFTER TAKEOFF THE ACFT HAD A COMPLETE ELECTRICAL FAILURE. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT AND LANDED THE ACFT SAFELY. WHEN INSPECTED BY MX A BATTERY RELAY WAS FOUND SHORTED TO GROUND. THE BATTERY RELAY WAS RESDR HYIA20140414039Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20121210001B-Nut · leakingTHE PILOT REPORTED A STEADY LOSS OF RT ENGINE OIL PRESSURE AFTER TAKEOFF. ENGINE SHUTDOWN AND FEATHERED BEFORE OIL PRESSURE REACHED THE RED LINE. DIVERTED BACK TO THE DEPARTURE. DURING MX INSPECTION, A LOOSE B-NUT WAS ALSO FOUND ON THE OIL PRESSURE LINE TSDR HYIA20121210002Latch · out of adjustPILOT REPORTED THAT AFTER TAKEOFF, DURING CLIMB, EMERGENCY EXIT DOOR LOCATED ON THE RT SIDE OF THE AFT, OPENED UNCOMMANDED. SAFELY RETURNED TO THE DEPARTURE. DURING INSPECTION, DOOR LATCHES WERE FOUND TO BE OUT OF ADJUSTMENT. LATCHES WERE ADJUSTED IAW MM.SDR HYIA20121205001Actuator · stuckPILOT REPORTED THAT DURING FLIGHT CONTROL CHECK ON TAXI OUT FOR DEPARTURE, THEY NOTED THAT THE AILERON TRIM WAS STUCK IN THE LT WING DOWN POSITION WHEN THEY ATTEMPTED TO ADJUST IT. THE PILOT RETURNED TO THE GATE. UPON MX INSPECTION, THE AILERON TRIM HINGE ANDSDR HYIA20121203003Spar · damagedDURING A ROUTINE MX INSPECTION DAMAGE WAS NOTED AT THE RT LOWER STUB WING IN THE AREA OF THE RT JACK POINT. INITIAL DAMAGE WAS IDENTIFIED AS A WRINKLING OF THE SKIN. SKIN WAS DERIVETED TO INSPECT UNDERLYING STRUCTURE (AFT CARRY THROUGH SPAR ASSY 5211173-2 ATSDR HYIA20121203002Beam · crackedDURING A SCHEDULED MX EVENT, THE RT ENGINE ASSY WAS REMOVED FOR A SCHEDULED TIME CHANGE. UPON REMOVAL, A CRACK WAS DISCOVERED AT THE RT NACELLE CROSSOVER BEAM IN THE AREA OF TURBOCHARGER BRACKET HOLE LOCATIONS. LOCATION OF CRACK RELATIVE TO RT NACELLE CROSSOVSDR HYIA20121203001Control Cable · separatedPILOT REPORTED THAT DURING THE CLIMB, THE LT PROPELLER RPM RATE BECAME UNCONTROLLABLE. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT AND LANDED SAFELY. UPON MX INSPECTION, THE C/A WAS TO RESECURE THE LT PROP CONTROL CABLE TO THE LT PROP GOVERNOR.SDR HYIA20140414038Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20140414037Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414036Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20140414035Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414034Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414033Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414032Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414031Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414030Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20121130001Spar Cap · crackedDURING A SCHEDULED MX EVENT, THE AFT CARRY THROUGH SPAR CAP WAS FOUND TO HAVE A CRACKED ANGLE AT LT FWD CENTER FLOOR STRINGER. THE C/A WAS TO FABRICATE AND INSTALL A DOUBLER AND SHIMS IAW DWG CAS-CAP13, REV 10-9-2012 FS186 REAR SPAR FLOOR SUPPORT FLANGE REPASDR HYIA20121126003Beam · corrodedSEVERE CORROSION WAS DISCOVERED BETWEEN RT NACELLE OTBD ENGINE BEAM AND LOWER NACELLE SKIN. RIGHT NACELLE OTBD BEAM HAT CHANNEL WHICH IS SANDWICHED BETWEEN BEAM AND LOWER NACELLE SKIN, IS SEVERELY CORRODED. REMOVED RT NACELLE OTBD ENGINE BEAM , PERFORMED DETSDR HYIA20121126002Bolt · missingPILOT REPORTED THAT DURING LANDING ROLLOUT, THE AIRPLANE YAWED TO THE RIGHT. THE PILOT WAS ABLE TO SAFELY TAXI THE ACFT OFF THE RUNWAY. UPON MX INSPECTION, IT WAS DISCOVERED THAT THE BOLT WAS MISSING FROM THE RT MLG TORQUE LINK AND THAT THE GEAR HAD SPUN 180SDR HYIA20121126001Wire · smokePILOT REPORTED THAT DURING CRUISE FLIGHT, SMOKE WAS SEEN COMING FROM BELOW THE YOKE. ON LANDING, MX INSPECTED THE ACFT AND REPLACED RING TERMINALS, WIRING, AND HARDWARE AT CABIN FAN SWITCH.SDR HYIA20121121001Attach Fitting · corrodedDURING A SCHEDULED MAINTENANCE EVENT, AT REMOVAL OF LT WING TO FACILITATE OTHER MX, THE LT AFT LOWER FUSELAGE FITTING WAS FOUND TO BE SEVERELY CORRODED. FITTING, PN IS 5011024-2, ASSUMED TO BE ORIGINAL FROM ACFT MFG WITH 31,645.5 HOURS TT IN SERVICE. REMOVEESDR HYIA20121120001Strap · corrodedDURING A REGULARLY SCHEDULED MAINTENANCE EVENT, THE LEFT LOWER NACELLE SKIN (PN 5654100-30) AND ASSOCIATED HEAT SHIELD WERE REMOVED FOR OTHER MAINTENANCE. AFTER REMOVAL, SEVERE CORROSION WAS FOUND AT LEFT SPAR STRAP INCLUDING SPAR CAP FASTENER FAILURE. VISUAL SDR HYIA20140414029Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414028Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20140414027Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20140414026Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20121108001Attach Fitting · crackedDURING REPLACEMENT OF WING SPAR STRAP ON RT WING, OTBD ENGINE BEAM FITTING WAS DISCOVERED TO BE CRACKED IN TWO LOCATIONS. OPENSDR HYIA20121028001Volt Regulator · failedPILOT REPORTED THAT DURING CRUISE FLIGHT, BOTH ALTERNATORS DROPPED OFF LINE AND A SMELL OF SMOKE WAS NOTED IN THE COCKPIT. THE ACFT SUBSEQUENTLY DIVERTED AND LANDED SAFELY. UPON MX INSPECTION, INITIAL C/A OF SUSPECTED OVER VOLTAGE RELAY SHORTING AGAINST PANESDR HYIA20121023001Doubler · crackedDURING A ROUTINE SCHEDULED MX EVENT, A CRACK WAS DISCOVERED IN THE RT FORWARD NLG TUNNEL WEB 00DOUBLER AT FS 44.00 IN THE AREA OF THE RT NLG TRUNNION BEARING BLOCK FORWARD MOUNT HOLE LOCATIONS. DETERMINED TO BE A REMOVAL AND REPLACEMENT OF OWNER PRODUCED WEB SDR HYIA20140414025Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A
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