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 = '525C' 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 = '525C' 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 QREA202610140007Alternator · overheatedRIGHT AC GENERATOR FAILED IN FLIGHT WHICH CAUSED RH WINDSHEILD HEAT FAIL. AIRCRAFT WAS ENROUTE TO TXKF OCEANING FLIGHT FROM KHPN. EXITED ICING CONDITIONS AND RETURNED TO BASE AT KDXRSDR L4OA202609300216Outflow Valve · mismanufacturedTEXTRON ALERTED US THAT THE OUTFLOW VALVES ON SOME OF THEIR NEW DELIVERIES WERE PRODUCED BY A VENDOR WITH AN UNCERTIFIED TOOL. THE AFFECTED PARTS WERE ON 2 PLANES THAT WE HAVE TAKEN DELIVERY OF BUT NOT YET ON OUR 135 CERTIFICATE. THESE PARTS WERE ALSO ON 2 OTHSDR 2026FA0000013Ground Stud · looseRIGHT GENERATOR TAKES 100% OF THE LOAD ONCE IN CRUISE. IF CUSTOMER TURNS OFF THE RT GENERATOR IN FLT, THE LT GENERATOR TAKES THE LOAD WITH NO ISSUES. IF HE TURNS THE RT GEN BACK ONLINE, IT PARALLELS, THEN EVENTUALLY BACK TO THE 100% AMP SPLIT WITH THE RT GENERSDR 2025FA0000590Window Frame · corrodedDURING COMPLIANCE WITH SB525C-56-01 CORROSION FOUND ON ALL WINDSHIELD FRAMES AND SURROUNDING STRUCTURE REQUIRING REPLACEMENT OF ALL COCKPIT WINDSHIELD FRAMES AND ATTACHING SKINS.SDR WI5R2025063000437Compressor · damagedENGINE MODEL FJ44-4A, S/N 211135, FROM AIRCRAFT N503TF), WAS RETURNED TO THE REPAIR STATION FOR UNSCHEDULED REPAIR. OPERATOR STATED HE DETECTED A BLEED ODOR DURING CLIMB, PROMPTING A RETURN TO AIRPORT. LANDING UNEVENTFUL. TROUBLESHOT ISSUE WITH TECH, REPORTESDR 2025F00140Line · rupturedDURING INITIAL CLIMB OUT PASSING 22,000 FEET THE TAILCONE BLEED LEAK CAS ILLUMINATED. PILOTS RAN THE CHECKLIST AND WITH BLEED AIR SOURCE SELECTED TO LEFT ONLY THE CAS EXTINGUISHED. PILOTS LEFT THE SOURCE TO LEFT FOR REMAINDER OF FLIGHT AND LIGHT STAYED OFF. SDR 2025FA0000378Elec Connector · unsecureDURING CLIMB, WITH AUTOPILOT ENGAGED, CREW WAS ALERTED TO A RT WING OVERTEMP MESSAGE, FOLLOWED BY AUTOPILOT DOING UNCOMMANDED LT & RT ROLLS RAPIDLY, AUTOPILOT DISENGAGED BY CREW & THE ACFT FLOWN BY HAND. CREW NOTED THAT THE AILERON TRIM INDICATED FULL LT DEFLSDR 2025FA0000316Bearing · seizedAIRCRAFT WAS IN MAINTENANCE TO HAVE THE MAIN LANDING GEAR TRUNNION PIVOT BEARINGS LUBRICATED. DURING THIS MAINTENANCE IT WAS NOTED THAT THE RIGHT FORWARD TRUNNION PIVOT BEARING WOULD NOT EXCEPT GREASE AND THE TRUNNION PIVOT PIN RETAINING BOLT APPEARED TO BE SHSDR 2025F00084Bearing · corrodedAIRCRAFT 525C-0448 WAS BROUGHT TO TEXTRON MCO SERVICE CENTER FOR ROUTINE SCHEDULED MAINTENANCE AND TO ACCOMPLISH L/R FORWARD MLG TRUNNION INSPECTION. MAKING SURE THE BEARINGS GET LUBED AND VERIFY THEY ARE NOT SEIZED UP. THE CUSTOMER ALSO OWNS 525C-0447 WHICH HSDR 2025FA0000223Bearing · bindingCUSTOMER NOTES: AFTER SELECTING THE GEAR DOWN, THE LEFT MAIN GEAR DID NOT GO GREEN, AND THE RED UNSAFE LIGHT STAYED ILLUMINATED. THIS HAPPENED WHILE ON APPROACH TO LAND, CREW THEN RETRACTED THE FLAPS TO DO A GO AROUND AND SHORTLY AFTER RETRACTING THE FLAPS THESDR 2025FA0000219Bearing · seizedAIRCRAFT WAS IN MAINTENANCE TO HAVE THE MAIN LANDING GEAR INSPECTED DUE TO PRIOR ISSUES NOTED ON OUR OTHER AIRCRAFT. PER OUR REQUEST, AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR WAS CYCLED TO SEE IF THERE WERE ANY ISSUES, IE; BINDING OR NOISES COMING FROSDR 2025FA0000212Bearing · seizedON APPROACH FOR LANDING THE CREW SELECTED GEAR DOWN, THE NOSE AND THE RIGHT MAIN GEAR EXTENDED AND THERE WERE GREEN DOWN AND LOCKED INDICATIONS. THE LEFT MAIN EXTENDED BUT THE CREW DID NOT SEE A GREEN DOWN AND LOCKED INDICATION, INSTEAD THEY HAD A RED GEAR UNSSDR 9JLA20250325001Indication Sys · failedMOVED GEAR LEVER TO DOWN POSITION WITH NO INDICATION.SDR 2025FA0000209Bearing · seizedAIRCRAFT WAS IN MAINTENANCE TO HAVE THE MAIN LANDING GEAR ACTUATORS REPLACED DUE TO REACHING THEIR LIFE LIMIT. DURING THIS MAINTENANCE IT WAS NOTED THAT BOTH MAIN LANDING GEAR FORWARD TRUNNION PIVOT BEARINGS WERE SEIZED WHICH CAUSED RESISTANCE/BINDING WHEN RETSDR 2025FA0000208Bearing · seizedAIRCRAFT WAS IN MAINTENANCE TO HAVE THE MAIN LANDING GEAR ACTUATORS REPLACED DUE TO REACHING THEIR LIFE LIMIT. DURING THIS MAINTENANCE IT WAS NOTED THAT BOTH MAIN LANDING GEAR FORWARD TRUNNION PIVOT BEARINGS WERE SEIZED WHICH CAUSED RESISTANCE/BINDING WHEN RETSDR 2024FA0000526Start Button · deactivatedFLIGHT CREW REPORTED THAT THE RIGHT ENGINE SHUTDOWN DURING THEIR TAKEOFF ROLL. CREW ABORTED THEIR TAKEOFF AND TAXIED THE AIRCRAFT BACK TO A LOCATION TO FURTHER EVALUATE THE RIGHT ENGINE'S CONDITION. CREW CONTACTED JET OUT'S MAINTENANCE DEPARTMENT, IT WAS THEN SDR 2024FA0000215Bearing · failedALTERNATOR P/N 9914777-2 HAD A MAIN BEARING FAIL. THIS IS AN ON CONDITION PART WITH NO INSPECTION OR OVERHAUL LIMITS. ALTERNATOR LASTED ONLY 1615 HOURS BEFORE FAILURE OF THE MAIN BEARING. THE MAIN BEARING CAME APART UNDER NORMAL OPERATING CONDITIONS AND CAUSEDSDR 9PMA2023092600568Buss · false indicationON CLIMB OUT , DCU A , DCU B , AP PITCH CONTROL FAIL , IFIS MISCOMPARE AND AP FAIL . UPON ARRIVAL OF MX NO FAULT WAS FOUND . GAINED ACCESS TO THE FAULT HISTORY AND VERIFIED THERE WAS A DCU CHANNEL B FAULT IN THE AIR WITH A FDR-1 MODULES BUS INOP MESSAGE PRESENSDR 2023F00114Engine · unknownOIL PRESURE LOW R EICAS MESSAGE ON DEPARTURE FROM NEW YORK STEWART INTERNATIONAL AIRPORT (KSWF). FLIGHT DIVERTED BACK TO KSWF FOR A PRECAUTIONARY LANDING. RETURN FLIGHT, LANDING AND TAXI WERE UNEVENTFUL.SDR 2023FA0000157Actuator · draggingNOTICEABLE YAWING WITH SMALL DISPLACEMENT BUMPS LEFT & RIGHT WITH AUTOPILOT ON OR OFF. INSPECTION FOUND RUDDER BIAS ACTUATORS DRAGGING AND SEALS NEEDED CLEANED AND LUBRICATED.SDR 2022FA0000321None · noneEFIS MISCOMPARE AFTER TAKEOFF. RESULTING IN ERRONEOUS AIRSPEEDS AND ALTITUDES ON BOTH PFD’S AND STBY FD. EMERGENCY DECLARED DUE TO UNKOWN ALTITUDES AND RETURNED TO AUS. UPON INSPECTION FOUND MUD DAUBER NEST IN ALL STATIC PORTS. CONTACTED DUNCAN AVIATION FOR PUSDR 2021F00371Switch · activeEN ROUTE TO LAS FROM SLC WITH THE PATIENT ON BOARD. LEVELED OFF FL230 AND A MINUTE LATER THE FUEL PRESSURE LOW L INDICATOR CAME ON. WE (DAVID HALE AND SIC RICK JONES) FOLLOWED THE CHECKLIST WITH THE USE OF THE L STANDBY BOOST PUMP AND RETURNED TO SLC.”SDR 2021FA0000359None · nonePILOT NOTED HIGH OIL PRESSURE ON #2 ENGINE WITH INSTRUMENT READING 150 PSI AND RED IN COLOR WITH NO OTHER INDICATION OF ANY OTHER PROBLEMS. PILOT RETARDED #2 THROTTLE TO IDLE WITH NO CHANGE IN OIL PRESSURE READING AND APPROX 2.5 MINUTES LATER THE PILOT SHUTDOWSDR 2021F00216Alternator · failedLEFT AC ALTERNATOR BEARING FAIL-CAS MESSAGE SAID PRIMARY BEARING FAIL THIS ITEM WAS RECEIVED FROM OVERHAUL WITH OVERHEATING EVIDENCE STILL APPARENT VIA THE BROWN TINT ON THE PAINT ON THE CASE DIRECTLY FROM CESSNA. SOMEONE NEEDS TO CONTACT PACIFIC SCIENTIFIC SDR 2021FA0000200Smoke Detector · false indicationPILOT REPORTED SMOKE DETECTION WARNING INDICATION IN CRUISE, DIVERTED TO KHOU AND CONTACTED TEXTRON AVIATION. UPON INSPECTION CAME TO THE CONCLUSION THAT THE EXCESSIVE MOISTURE AND FOG PRESENT GAVE THE DETECTOR A FALSE INDICATION. NO DEFECTS NOTED AND AIRCRAFTSDR 4LSA2021052402081Engine · failedDURING TAKEOFF CLIMB OUT OF FLYING CLOUD AIRPORT (FCM), THE FLIGHT CREW HEARD A METAL GRINDING NOISE FOLLOWED BY HIGH INLET TURBINE TEMPERATURE (ITT) INDICATION AND A OIL FILTER BYPASS INDICATION FOR THE RIGHT ENGINE. FLIGHT CREW ELECTED TO SHUT RIGHT HAND ENGSDR 2021FA0000389None · inoperativePILOT REPORTS WEATHER RADAR FAULT IS PRESENT. COMPLIED WITH R&R OF WEATHER RADAR. OPS CHECKED OK. AIRCRAFT OK FOR RTS.SDR 2021FA0000080Generator · burnedREMOVED RH ENGINE AUX GENERATOR (AC ALTERNATOR) P/N 9914777-2 (94495-1), S/N 128 DUE TO WINDING RESIN MELTING FROM ALTERNATOR, RESIN SLINGING FROM INTERNAL FAN AND BEARING DRAG. UNIT REMOVED WITH 231.2HRS/144 LANDINGS SINCE OVERHAUL. PREVIOUS ALTERNATOR FAILURSDR AMCR20210318002Alternator · meltedBEFORE FLIGHT, ON INITIAL ENGINE RUNS, IT WAS NOTICED THAT THE LEFT ALTERNATOR FAIL CAS MESSAGE WAS ILLUMINATED. UPON INSPECTION THE CREW REPORTED SMELLING SMOKE FUMES.THE ALTERNATOR WAS REMOVED AND REVEALED THAT AN INTERNAL SHORT HAD OCCURRED CAUSING THE FAILSDR 2021FA0000381Tire · wornPILOT REPORTS TIRE IS WORN AND REQUIRES REPLACEMENT. COMPLIED WITH R&R OF TIRE. AIRCRAFT OK FOR RTS.SDR 2020FA0000550Battery · failedPILOT REPORTS ON START UP BATTERY VOLTAGE DROPPED BELOW MINIMUM REQUIRMENTS FOR PROPER START. UPON FURTHER INSPECTION FOUND MAIN SHIP BATTERY TO BE INOPERABLE. COMPLIED WITH REPLACMENT OF MAIN SHIP BATTERY. OPERATIONS CHECKED GOOD AND AIRCRAFT WAS OK FOR RESDR WI5R2020101400001Rotor · damagedAIRCRAFT OPERATOR REPORTED THE NR 1 ENGINE ON N81RC (525C-0217) MADE AN UNUSUAL NOISE DURING ENGINE SPOOL-DOWN. OPERATOR REPORTED NO ENGINE OPERATIONAL ISSUES, SYMPTOMS, OR OTHER ANOMALIES DURING THE PREVIOUS FLIGHT. DURING A SUBSEQUENT BORESCOPE INSPECTION SDR WI5R2020100100001Rotor · damagedFLIGHT CREW OF N159WG (525C-0216) REPORTED THAT ITT HAS GRADUALLY INCREASED ON RT ENGINE SERIAL NUMBER 211444 OVER THE PAST THREE MONTHS, RECENTLY TOUCHING THE RED BAND OF THE ITT DISPLAY DURING TAKEOFF. SUBSEQUENT BORESCOPE INSPECTION REVEALED DAMAGE TO HIGHSDR 2020FA0000543Strut · inoperativePILOT REPORTS HE COULD NOT OPERATE NUMBER 3 PASSENGER SEAT RECLINE. AFTER FURTHER INSPECTION FOUND NUMBER 3 SEAT RECLINE STRUT TO BE INOPERABLE. COMPLIED WITH REPLACEMENT OF NUMBER 3 SEAT RECLINE STRUT. PASSENGER SEAT OPERATIONS CHECKED GOOD, AIRCRAFT OK FOSDR WI5R2020082400002Rotor · damagedREVIEW OF HISTORICAL, ROUTINE FADEC DOWNLOADS PERFORMED BY THE ENGINE MANUFACTURER REVEALED A SLIGHT SHIFT IN INTER-TURBINE TEMPERATURE (ITT), OCCURRING APPROXIMATELY 25 HOURS PRIOR TO THE MOST-RECENT FADEC DOWNLOAD PERFORMED DURING A ROUTINE CHECK 1 & CHECK 2SDR WI5R2020082400001Rotor · damagedREVIEW OF HISTORICAL, ROUTINE FADEC DOWNLOADS PERFORMED BY THE ENGINE MANUFACTURER REVEALED A SLIGHT SHIFT IN INTER-TURBINE TEMPERATURE (ITT), OCCURRING APPROXIMATELY 25 HOURS PRIOR TO THE MOST-RECENT FADEC DOWNLOAD PERFORMED DURING A ROUTINE CHECK 1 & CHECK 2SDR 2020FA0000541Pcb · inoperativePILOT REPORTS ALL BACK LIGHTING ON RIGHT HAND SIDE OF COCKPIT WILL NOT TURN ON. UPON FURTHER INSPECTION FOUND PILOTS SIDE PRINTED CIRCUIT BOARD WAS INOPERABLE. REPLACED PILOTS SIDE PRINTED CIRCUIT BOARD. OPERATIONS CHECKED GOOD AIRCRAFT OK FOR RETURN TO SERSDR AMCR20200727021Alternator · shortedUPON TAXI TO HOME BASE HANGAR, CREW REPORTED A AMBER RH ALTERNATOR FAIL CAS MESSAGE. GROUND CREW SAW WHITE SMOKE COMING FROM RH ENGINE COWL. AN INSPECTION REVEALED THE AC ALTERNATOR HAD INTERNALLY SHORTED AND MELTED SOME OF ITS WINDINGS. PROCEDURES FOR CESSNA SDR WI5R2020070800001Compressor Blade · damagedFOLLOWING INCORPORATION OF SERVICE BULLETIN FJ44-72-127 (1ST LOW PRESSURE TURBINE NOZZLE UPGRADE) ON ENGINE, POST-MAINTENANCE VIBRATION SURVEY GROUND RUNS REVEALED N1 SPOOL VIBRATION LEVELS ABOVE LINE MAINTENANCE MANUAL LIMITS. ATTEMPTS TO TRIM-BALANCE THE ENSDR WI5R202005270002Rotor · fracturedCUSTOMER REPORTED AN UNUSUAL NOISE DURING THROTTLE TRANSITION TO POWER. ALL ENGINE INDICATIONS WERE NORMAL. ON-WING BORESCOPE INSPECTION OF LEFT-HAND ENGINE SERIAL NUMBER (ESN) 211417 REVEALED DAMAGE TO 3RD-STAGE INTERMEDIATE COMPRESSOR ROTOR BLADES AND ONE SDR WI5R2020032000000Rotor · damagedDURING INITIAL TAKEOFF ROLL, PILOT NOTED RUMBLING NOISE AND A SHUDDER IN THE FOOT PEDALS WITH NO ABNORMAL INSTRUMENT INDICATIONS.
PILOT ABORTED TAKEOFF AND RETURNED TO RUNWAY END. PILOT ATTEMPTED SECOND TAKEOFF WITH NORMAL ENGINE INDICATIONS.
AT 1,200 FEET, SDR WI5R202003060001Rotor · fracturedSUBSEQUENT TO THE 1ST LPT NOZZLE FIELD REPLACEMENT FOR SERVICE BULLETIN FJ44-72-127, THE ENGINE DID NOT PASS THE REQUIRED VIBRATION SURVEY FOR 1E LP.
BORESCOPE INSPECTION REVEALED A MISSING 3RD STAGE IP ROTOR BLADE AND A DAMAGED HPC ROTOR.
DISASSEMBLY OF THESDR WI5R20200203001Rotor · fracturedDURING POST FDU SWAP RUN ON THE ENGINE, TECHNICIANS HEARD A "BANG" , FOLLOWED BY BLACK SMOKE FROM THE EXHAUST, NO INDICATION FLUCTUATIONS WERE NOTED.
THE SUPPORTING SERVICE CENTER PERFORMED BORESCOPE INSPECTION AND FOUND MISSING 3RD STAGE IP ROTOR BLADE.
DISSDR WI5R20200117001Rotor · fracturedDURING OPERATION, A LOUD BANG AND INCREASE IN ITT WERE OBSERVED. FIELD BORESCOPE INVESTIGATION IDENTIFIED SEVERAL MISSING 3RD STAGE IP ROTOR BLADES.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT FIVE OF THE 3RD STAGE IPC ROTOR BLADES WERE MISSING.SDR WI5R20200110001Rotor · fracturedDURING FIELD TROUBLESHOOTING FOR A REPORTED ENGINE VIBRATION, BORESCOPE INSPECTION REVEALED POTENTIAL IP BLADE LIBERATION.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR WI5R20200108001Rotor · fracturedDURING FIELD BORESCOPE INSPECTION FOR N1 LAG AND ITT INCREASE AT T.O., A 3RD STAGE IP ROTOR BLADE WAS DISCOVERED MISSING.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR WI5R20191219001Rotor · fracturedDURING TAKEOFF AND CLIMB, SPARKS WERE REPORTED COMING FROM THE TAILPIPE. FIELD BORESCOPE INVESTIGATION IDENTIFIED A MISSING 3RD STAGE IP ROTOR BLADE.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT THREE OF THE 3RD STAGE IPC ROTOR BLADES WERE MISSING.SDR WI5R201910190001Blade · fracturedTREND DATA INDICATED A ABRUPT SHIFT IN ITT AND N2 PARAMETERS. FIELD BORESCOPE INVESTIGATION IDENTIFIED A MISSING 3RD STAGE IP ROTOR BLADE.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.
THE ROTOR (P/N 119345 S/SDR WI5R2019082200001Blade · fracturedWHILE TROUBLE SHOOTING FOR A REPORTED UNUSUAL VIBRATION IN FLIGHT, A BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR WI5R2019080100001Blade · fracturedWHILE TROUBLE SHOOTING FOR ITT AND N2 SPLITS WITH THE SISTER ENGINE, A BORESCOPE INSPECTION FOUND DAMAGE AND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE REVEALED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.
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