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 = 'P180' 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 = 'P180' 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 2025FA0000443Brake · seizedDURING AN AIRCRAFT JACKING PROCEDURE FOR UNRELATED MAINTENANCE, MAINTENANCE PERSONNEL NOTICED THAT THE RIGHT-HAND (RH) WHEEL WAS NOT ABLE TO SPIN NORMALLY DUE TO HIGH FRICTION. THE BRAKE WAS SENT OUT FOR EVALUATION AND WAS FOUND TO HAVE BEEN OVERHEATED, WHICH SDR 2024FA0000068Relay · overheatedDURING MAINTENANCE, IT WAS NOTED THAT RELAY K62 HAD BECOME EXCESSIVELY WARM AT SOME POINT AND THE HEAT SHIELDING ON WIRE H202A10 THAT IS CONNECTED TO THE RELAY TERMINAL A1 WAS ALSO MELTED. NO EVIDENCE OF FIRE AFFECTING SURROUNDING AREA. JUST THE OVERHEATING SDR PAZR202305100001Adc · inoperativeAPPLIED POWER TO AIRCRAFT AND VERIFIED THE #1 ADC SHOWS AS FAILED. PUSHED THE SELF TEST BUTTON ON FRONT OF UNIT, NO SIGN OF SELF TEST WAS SEEN. REMOVED #1 ADC UNIT AND VERIFIED POWER AND GROUNDS TO UNIT. ALL POWER AND GROUNDS CHECKED GOOD.SDR 9JLA2023021034502Unknown · unknownDURING POST FLIGHT MAINTENANCE CHECKS THE TECHNICIAN NOTED A CRACK IN THE RIGHT ENGINE UPPER COWL MATERIAL THAT WAS APPROXIMATELY 3 INCHES LONG. THE CRACK IS POSITIONED 39 INCHES AFT OF THE LEADING EDGE OF THE RIGHT COWL INLET LIP ON THE INBOARD SIDE OF THE COSDR 2021F00214Windshield · usedTHIS WAS IN A PIAGGIO AVANTI II AIRCRAFT. THE OUTER PANE OF THE CO-PILOT'S WINDSHIELD CRACKED IN FLIGHT.SDR 9JLA2021080425175Sensor · defectiveTHE FLIGHT CREW REPORTED THAT PROPELLER SYNC FAULTED, THE CREW ADVISED, WHEN ENGAGED THE LEFT PROP WOULD SPEED-UP 25 TO 30 RPM. THE DISCREPANCY WAS DEFERRED FOR CONTINUED OPERATIONS. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE LEFT PROP SYNCHRO PHASER SDR 3FPY20190711005Actuator · faultyAIRCREW REPORT: PITCH TRIM INDICATION INTERMITTENT. PITCH TRIM ACTUATOR OUTPUT SIGNAL FOR PITCH TRIM INDICATOR ERRATIC - INDICATION INACCURATE (FAILED COMPLETELY DURING FAULT FINDING). PITCH TRIM ACTUATOR REPLACED WITH OVERHAULED COMPONENT AND TESTED SERVICEABSDR 2019FA0000133Brake Assy · lockedUPON LANDING AT THE KRVS AIRPORT, THE RIGHT MAIN WHEEL/BRAKE WAS COMPLETELY LOCKED UP AND FAILED TO ROTATE WHATSOEVER. THIS WAS AFTER A SIMILAR EVENT AT KEDC. UPON LANDING AT KEDC, THE RIGHT MAIN WHEEL "APPEARED" TO LOCK UP MOMENTARILY CAUSE A FLAT SPOT ON TSDR CA190428001Seal · leaking(CAN) OIL ODOR NOTED IN CABIN DURING CLIMB, VISIBLE SMOKE/HAZE NOTED IN CABIN AT TOP OF CLIMB, ENGINE POWER REDUCED AND SMOKE/HAZE CLEARED AND OIL ODOR REDUCED. AIRCRAFT RETURNED TO BASE WITH NO FURTHER INCIDENT. POST FLIGHT INVESTIGATION REVEALED OIL CONTAMISDR 2019F00022Pulley · failedDURING A SCHEDULED 200FH INSPECTION AS REQUIRED BY CHAPTER 05-00-00, THE LEFT LOWER RUDDER PULLEY, IT WAS NOTICED THAT THE LOWER LEFT RUDDER PULLEY WAS APPROXIMATELY 1/4" HIGHER THEN THE RIGHT PULLEY. UPON REMOVAL OF THE PULLEY, THE BEARING AND RACE WAS FROZENSDR 2018FA0000108Downlock Switch · malfunctionedON DEPLOYMENT OF GEAR , NO GREEN LIGHT NOTED AT RIGHT MAIN GEAR ANNUNCIATOR, AND NO RED UNSAFE LIGHT NOTED AT RIGHT GEAR ANNUNCIATOR. HYDRAULIC POWER PACK WENT TO LOW MODE AFTER GEAR DEPLOYED BUT WARNING HORN COULD NOT BE SILENCED WITH GEAR SELECTED DOWN. WHENSDR 2017FA0000226Brake Assy · bindingAIRCRAFT HAD THE LEFT WHEEL GO FLAT AFTER LANDING ROLLOUT. THIS IS THE SECOND TIME THAT IT HAS HAPPENED IN THE LAST TWO WEEKS. UPON INSPECTION OF THE WHEEL, IT WAS NOTICED THAT THE THERMAL FUESES WERE OPEN. AFTER CONSULTATION WITH THE AIRCRAFT MANUFACTURER,SDR 2016F00231Door · out of adjustDURING CLIMB OUT, THE AIRCRAFT FAILED TO PRESSURIZE. THE SOUND OF RUSHING AIR WAS HEARD. FOLLOWED THE CHECKLISTS AND COULD NOT GET THE PLANE TO PRESSURIZE. A DECISION WAS MADE TO RETURN FOR LANDING AND AN EMERGENCY DECLARED. DURING A POST FLIGHT INSPECTION, SDR 2016FA0000551Handle · failedATTEMPTED OPENING THE EMERGENCY EXIT FROM THE EXTERIOR OF AIRCRAFT. EMERGENCY EXIT HANDLE FAILED.SDR CA160301004Heater · malfunctioned(CAN) AFTER LANDING, EXTERNAL FUEL LEAK WAS NOTICED. (THIS IS THE 3RD EVENT). THE FUEL WAS INSIDE THE RIGHT HAND ENGINE NACELLE, ON WING, FUSELAGE AND EVEN INSIDE THE LANDING GEAR VANE. PIAGGIO DID A GROUND RUN, AND REPORTED, ABOVE IDLE POWER, A FUEL SPRAY FROSDR CA160113002Actuator · loose(CAN) DURING INSPECTION, NOTICED ROD END JAM NUTS NOT SECURE ON RUDDER TRIM ACTUATOR.SDR CA160119021Engine · malfunctioned(CAN) THE OPERATOR REPORTED THAT 4 TIMES OUT OF 5, THE ENGINE WILL NOT GO IN REVERSE. CYCLING THE CONTROLS HAD NO EFFECT. TROUBLESHOOTING IS ON-GOING WITH RIGGING TESTING AND PROPELLER GOVERNOR SWAP.SDR CA151125004Hose · collapsed(CAN) FOUND DURING A SCHEDULED INSPECTION RIGHT BLEED AIR PRE-COOLER OVERHEATED AND RT ENGINE BLEED AIR SUPPLY HOSE INTERIOR WALL COLLAPSED.SDR CA151125005Anti-Ice Valve · malfunctioned(CAN) LEFT WING ANTI-ICE VALVE FAILED TO CLOSE WHEN SELECTED "OFF". INVESTIGATION FOUND "BUTTEFLY" TURNING ON SHAFT DUE TO STRIPPED SPLINES.SDR CA150414004Hinge Pin · sheared(CAN) ENGINE ANTI-ICE DIVERTER DOOR HINGE PINS SHEARED. DOOR WAS FOUND LOOSE IN COWL. TECH SUPPORT HAS SEEN THIS IN THE PAST. DAMAGE POSSIBLY CAUSED BY ICE BUILD-UP.SDR J72A20150323001Warning Light · illuminatedDURING CRUISE FLIGHT AT 37,000FT, DOOR SEAL ANNUNCIATOR LIGHT ILLUMINATED. CABIN WAS STARTING TO CLIMB. MADE AN UNSCHEDULED LANDING. COULD NOT DUPLICATE PROBLEM. REPLACED DOOR SEAL CHECK VLV & REGULATOR AS PRECAUTIONARY MEASURES.SDR CA150325012Engine · flamed out(CAN) FOLLOWING THROTTLE REDUCTION TO IDLE DURING DESCENT THE ENGINE FLAMED OUT. THE PILOT WAS ABLE TO RESTART THE ENGINE WHICH FLAMED OUT AGAIN TWICE WHILE BRINGING THROTTLE TO IDLE. ALL EVENTS OCCURRED IN EEC MODE.SDR CA150313013Blade · separated(CAN) IAW "AVIATION OCCURRENCE REPORT" DATED MARCH, 11, 2015: AFTER LANDING ON RUNWAY 23, WHILE ON TAXIWAY P, SMOKE ODOR WAS DETECTED BY CAPTAIN AND WAS VERIFIED TO BE PRESENT WITH THE FIRST OFFICER. THE SMOKE ODOR APPEARED TO INCREASE AS WAS ACCOMPANIED WITHSDR J72A2015F00030Bulkhead · corrodedDURING "D" CHECK, VISUAL INSPECTION ON THE LOWER AFT FUSELAGE JOINT TO TAIL CONE AREA REVEALED CORROSION ON AFT FUSELAGE CANTED BULKHEAD AND LOWER SKIN AREA.SDR J72A20150211Duct · crackedLEFT WING ANTI-ICE DUCT ASSEMBLY HAS CRACKS WHICH EXCEED MM SRM LIMITS. REPAIRED DUCT ASSEMBLY.SDR J72A20150211001Duct · crackedRIGHT WING ANTI-ICE DUCT ASSEMBLY HAS CRACKS WHICH EXCEED MM SRM LIMITS. REPAIRED DUCT ASSEMBLY IAW 337 DATED 11/30/2014.SDR J72A2015021100001Bulkhead · corrodedDURING D CHECK INSPECTION, THE CANTED BULKHEAD LOCATED AT FS 8154 AT THE 6 O'CLOCK POSITION HAS CORROSION THAT EXCEEDS MM SRM LIMITS. THE CAUSE OF THE PROBLEM SEEMS TO BE THE BUILDUP OF WATER ENTRAPPED AFT OF THE BULKHEAD. THE DRAIN HOLE IS LOCATED TO FAR AFSDR J72A2015F00032Bulkhead · corrodedDURING D-CHECK INSPECTION, THE CANTED BULKHEAD LOCATED AT FS 8154 6 O'CLOCK POSITION HAS CORROSION THE EXCEEDS MM SRM LIMITS. CAUSE OF PROBLEM SEEMS TO BE WATER ENTRAPMENT AFT OF THE BULKHEAD AND THE DRAIN HOLE LOCATED TO FAR AFT OF THE CANTED BULKHEAD TO DRAISDR CA141223007Governor · failed(CAN) CREW DETERMINED PROPELLER CONTROLS NOT FUNCTIONING. IAW JLB ENTRY RT PROPELLER LOSS OF RPM. ENGINE SHUTDOWN PERFORMED IAW CHECKLIST. LANDED AIRCRAFT SAFELY. PROPELLER GOVERNOR REPLACED, AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT.SDR 2014FA0000561Bushing · wornFOUND VERTICAL PLAY IN LT AND RT ELEVATOR HINGES. NOTED BOLTS WERE TIGHT BUT GRIPPED OUT. REMOVED HORIZONTAL COLLARS AND STINGER TO GAIN ACCESS TO ELEVATOR ATTACHMENTS. REPLACED BOLTS WITH SHORTER PN NAS6404A20 AND USED ORIGINAL WASHERS; LETTER DATED SEPTEMBSDR CA140130008Valve · frozen(CAN) AFTER LIFTOFF, CABIN DOOR LIGHT ILLUMINATED. CREW MAINTAINED FL 10 AND COMPLETED TRIP WITHOUT INCIDENT. 3 WAY VALVES FROZEN, AIC SAT ON RAMP APPROXIMATELY 6 HOURS -30C - TIS OF AIC C/O NFF SYSTEM DRAINED IAW AMM, AIC DEPARTED NEXT MORNING. NO ISSUES WISDR 2013FA0000763Actuator · inoperativeAFTER ROTATION, THE PRIMARY PITCH TRIM WAS NOT WORKING. TRIM CLACKER WAS CLACKING BUT, THERE WAS NO MOVEMENT OF THE STABILIZER. SWITCHED TO SECONDARY HORIZONTAL PITCH TRIM WHICH WAS OPERATIONAL. MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING REVEALED THE MOTSDR V2JA2013F00133Brake Disc · brokenRIGHT WHEEL WAS REMOVED FOR SN VERIFICATION, AS WHEEL CAME OFF, BRAKE PAD PARTS AT KEY WAY FELL OUT.SDR V2JA0602134154986Display · failedIN FLIGHT, CAPTAINS PFD WENT BLANK, WITHIN A FEW SECONDS A STRONG BURNING ODOR FILLED THE COCKPIT.SDR V2JA0523134153420Fitting · leakingHYDRAULIC PUMP FAILED ON APPROACH. FOLLOWED CHECKLIST HAND-PUMPED GEAR DOWN. "HYD PRESS" CAUTION LIGHT ILLUMINATED, ASSOCIATED PRESSURE BETWEEN 0-200 PSI, DIVERTED.SDR V2JA052313DEF130Seal · damagedMASTER CAUTION (DOOR SEAL) AT 34,000. RAN CHECKLIST WITH F/O FOR DESCENT TO 30,000 FT. AT 30,000 FT AIRCRAFT WAS STABLE. AFTER ABOUT 5 TO 10 MINUTES A LOUD DOOR SEAL NOISE WAS NOTED AND CABIN BEGAN TO CLIMB RAPIDLY. AN EMERGENCY DESCENT WAS PERFORMED AS ASDR CA130603006Control System · malfunctioned(CAN) THE LEFT PROPELLER RPM DECAYED UNCOMMANDED TO FEATHER AT 1000` AGL. THE FAILURE OCCURRED AS THE POST TAKE OFF POWER REDUCTION WAS PERFORMED. THE CREW WAS UNABLE TO RECOVER THE PROPELLER TO NORMAL RPM AND, THEREFORE, THE PILOT SHUT DOWN AND SECURED THE LHSDR CA130527011Spring · weak(CAN) PROPELLER RPM DECAYED TO UNCOMMANDED FEATHER AT 1000` AGL AFTER TAKE OFF. PROPELLER FAILURE OCCURRED AFTER THE POST TAKE OFF POWER REDUCTION. UNABLE TO RECOVER PROPELLER TO NORMAL RPM. PRIOR TO THE FAILURE, THE PROPELLER GOVERNOR HAD BEEN REINSTALLED AFSDR V2JA0504134142480Adc · failedBOTH ADC FAILED IN FLIGHT. ADC 1 FAILED FIRST, REVERTED TO ADC 2 WHICH FAILED 15 MINUTES LATER.SDR V2JA0504134151771Autofeather Sys · malfunctionedCREW REPORTS UNCOMMANDED AUTOFEATHER ON LEFT ENGINE.SDR V2JA2013043049004Door · out of adjustCARGO DOOR LIGHT ON IN FLIGHT. ADJUSTED BAGGAGE DOOR IAW AMM 52-30-00. OPS CHECKED GOOD.SDR 2013FA0000256Wire Harness · misinstalledRT FUEL QTY NOT DECREASING DURING RUN-UP. GROUND RUN-UP FINDING DATED 25-04, 2013. FOUND LT AND RT FUEL QUANTITY INDICATION SYSTEM CROSSED WITH EACH OTHER UNDERNEATH CENTER PEDESTAL FLOOR AT FS 500. WIRING BUNDLES REROUTED WITH THEIR RELATIVE INDICATORS TO TSDR V2JA2013050447914Landing Gear · failedAFTER TAKEOFF, WHEN GEAR SELECTED UP, HYD IN HIGH DUTY, 3 GREEN AND NO RED IN-TRANSIT. AFTER CYCLING THE LANDING GEAR HANDLE, LANDING GEAR RETRACTED NORMALLY. AFTER NOSE GEAR WAS LOWERED TO THE GROUND, FOLLOWING LANDING TOUCHDOWN, ACFT VEERED TO THE RT WITH SDR V2JA2013033083417Switch · out of adjustPILOT DISCREPANCY: BAG DOOR LIGHT IN FLIGHT. ADJUSTED AND OPS CHECKED BAGGAGE DOOR SWITCHES IAW P-180 LL MM 52-70-00, NO DEFECTS NOTED.SDR V2JA20121218006Warning Light · illuminatedCARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF, PERFORMED LT ENGINE SECURING CHECKLIST, LIGHT EXTINGUISHED AFTER THE ENGINE WAS SECURED, THEN ILLUMINATED AGAIN AND STAYED ON UNTILL SHORT FINAL, THEN EXTINGUISHED.SDR V2JA201212180005Engine · failedCLIMBING OUT OF FL260 TO FL310, RT TORQUE DROPPED 20 PERCENT AND IMMEDIATELY ROSE BACK TO 97 PERCENT. A SLIGHT HIGH FREQUENCY VIBRATION WAS THEN NOTICED BY CREW. CLIMB WAS CONTINUED TO FL310. AT FL310 OIL PRESSURE DROPPED BELOW 90PSI ON THE RT ENGINE WITH AUSDR V2JA20121218004Autofeather Sys · activatedUNCOMMANDED AUTO FEATHER ON FINAL.SDR V2JA0208134143337Switch · dirtyUNCOMMANDED AUTOFEATHER IN FLIGHT ON LAST LEG. POWER LEVERS, AND ALL ENGINE PARAMETERS WERE EQUAL. FOUND SWITCH DIRTY.SDR V2JA20121218003Propeller · faultyUNCOMMANDED AUTO-FEATHER OF RT ENGINE ON FINAL.SDR CA130212008Oil System · low pressure(CAN) AFTER AN AIRCRAFT MAINTENANCE, DURING FLIGHT TESTING, 1 PROCEDURE CALLS FOR AN IN-FLIGHT SHUTDOWN AND RELIGHT. DURING THE RELIGHT ATTEMPT THE ENGINE NR 2 OIL PRESSURE WAS INDICATING 12 PSI. THE PILOT SHUTDOWN THE ENGINE AND LANDED SAFELY AT THE AIRPORT
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