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 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.SDR WI5R201907100001Blade · fracturedWHILE TROUBLE SHOOTING FOR AN UNUSUAL NOISE DURING ENGINE SHUT DOWN, A BORESCOPE INSPECTION FOUND DAMAGE AND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR 2019FA0000224Blade · severedON 02-JUL-2019,CAPTAIN REPORTED THE RH ENGINE(SN 211516) OPERATION PARAMETERS WERE ABNORMAL, THE ITT READING ON RT WAS SIGNIFICANTLY HIGHER THAN LT. ALSO RT N2% WAS 0.7% HIGHER THAN LH. THESE SYMPTOMS WERE THE SAME AS THE LAST ENGINE CHANGE ON LT ENGINE IN AUGSDR WI5R2019062700008Blade · damagedWHILE CLIMBING OUT ON A RECENT FLIGHT, THE CREW REPORTED HEARING A BANG FOLLOWED BY AN ENGINE VIBRATION AT A POWER SETTING OF APPROX. 90% N1 ALONG WITH A SQUEALING IN FLIGHT.
A POST FLIGHT BORESCOPE INSPECTION CONFIRMED DAMAGE TO MULTIPLE 3RD STAGE IPC BLADESSDR WI5R201906270001Blade · missingDURING TROUBLE SHOOTING FOR A REPORTED "WHINE" NOISE WHEN N1 IS ABOVE 71%, A FIELD 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 WI5R20190621002Blades · fracturedDURING TROUBLE SHOOTING FOR AN UNUSUAL NOISE DURING FLIGHT, A FIELD BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE REVEALED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR WI5R201906210001Blades · fracturedDURING TAKE-OFF ROLL (APPROXIMATELY 4 SECONDS AFTER T.O. POWER SETTING ACHIEVED), A LOUD NOISE WAS HEARD AND THE AIRCRAFT VEERED TO THE LEFT (AIRCRAFT SPEED ~25KNOTS). THE PILOT IMMEDIATELY REDUCED POWER AND NOTED THAT THE LEFT ENGINE’S (ESN 211323) ITT WAS ISDR WI5R20190614001Rotor · fracturedDURING ENGINE SPOOL DOWN, CREW NOTED A SCRAPPING NOISE. AFTERWARDS, N1 WAS DIFFICULT TO ROTATE BY HAND.
FIELD BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE.
DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND OSDR WI5R201906070001Rotor · fracturedSERVICE CENTER CALLED TO REPORT AN UNUSUAL NOISE WHEN ROTATING N1 BY HAND. BORESCOPE INSPECTION FOUND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND ONE MISSING 3RD STAGE IP BLADE.SDR WI5R2019052200001Rotor · fracturedAPPROXIMATELY 30 MINUTES INTO A 2.5 HOUR FLIGHT, A LOUD BANG WAS REPORTED. FIELD BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE. REPAIR STATION DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND ONE MISSING 3RD SDR WI5R2019050300000Rotor · fracturedDURING TROUBLE SHOOTING FOR ELEVATED ITT TRENDS, A BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE DETERMINED THERE WERE TWO MISSING 3RD STAGE IP BLADES.SDR WI5R2019031500001Rotor · damagedDURING TROUBLE SHOOTING FOR ELEVATED ITT TRENDS, A BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND ONE MISSING 3RD STAGE IP BLADE.SDR WI5R2019022800001Rotor · fracturedDURING FLIGHT, THE CUSTOMER REPORTED A 'BANG'. FIELD TROUBLESHOOTING INDICATED THE N1 SPOOL WAS DIFFICULT TO ROTATE AND THERE WAS DAMAGE NOTED ON THE 3RD STAGE IP ROTOR BLADES. DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND ONE MISSING 3RD STAGE IP BLSDR WI5R201902010001Rotor · fracturedDURING FINAL APPROACH, THE CUSTOMER REPORTED A 'BANG' WITH AN ACCOMPANIED YAW. FIELD TROUBLESHOOTING SUGGESTED A MISSING IPC BLADE AND POTENTIAL DAMAGE TO COMPONENTS DOWNSTREAM OF THE IPC ROTOR. DISASSEMBLY OF THE ENGINE IN THE REPAIR STATION CONFIRMED FIELD FSDR WI5R2019012300001Rotor · fracturedDURING TROUBLESHOOTING FOR A REPORTED COMPRESSOR STALLS DURING FLIGHT AND RAPID ITT INCREASE, A BORESCOPE INSPECTION REVEALED SOME MISSING IPC BLADES AND FOD DAMAGE TO COMPONENTS DOWNSTREAM OF THE IPC ROTOR. DISASSEMBLY CONFIRMED 6 MISSING BLADES.SDR 2019FA0000023Compressor · damagedPILOT REPORTED A LOUD BANG SOUND FOLLOWED BY AIRCRAFT YAWING ON APPROACH. AFTER LANDING, THE RIGHT ENGINE FAN WAS TURNED THROUGH BY HAND AND A METAL TINGING SOUND COULD BE HEARD. BORESCOPE INSPECTION REVEALED MISSING IP COMPRESSOR BLADE MISSING. THIS IS THE 3RSDR WI5R201901170001Rotor · fracturedDURING TROUBLESHOOTING FOR A REPORTED N1 SLOW ROTATION, A BORESCOPE INSPECTION REVEALED A MISSING IPC BLADE AND FOD DAMAGE TO COMPONENTS DOWNSTREAM OF THE IPC ROTOR. INSPECTION OF THE ENGINE IN THE REPAIR STATION HAS CONFIRMED THE CONDITION.SDR 2019FA0000009Compressor · damagedPILOT REPORTED LEFT ENGINE START SLIGHTLY SLOWER THAN NORMAL ACCOMPANIED BY ABNORMAL SOUND. ALL ENGINE PARAMETERS WERE NORMAL AND A TAKEOFF POWER CHECK WAS GOOD. THE AIRCRAFT WAS FLOWN TO MAINTENANCE BASE AND PILOT NOTED ONLY A VERY SMALL SPLIT IN ITT INDICATISDR WI5R2019010700001Rotor · fracturedDURING PRE-BUY INSPECTION A MISSING 3RD STAGE IP ROTOR BLADE WAS DISCOVERED. DISASSEMBLY OF THE ENGINE CONFIRMED TWO MISSING 3RD STAGE BLADES.SDR WI5R201812120001Rotor · fracturedDURING TROUBLESHOOTING FOR SUDDEN ITT SPLIT BETWEEN LH AND RH ENGINES, BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IPC ROTOR BLADE AND POTENTIAL DAMAGE TO THE HPC ROTOR. DISASSEMBLY OF THE ENGINE CONFIRMED A MISSING 3RD STAGE BLADE.SDR 2018FA0000526Precooler · degradedIN ON OF PRE BUYS INSPECTIONS WE CAME ACROSS SEVER DELAMINATION & WARPING FROM THE HEAT CREATED BY THE BYPASS AIR IN THE PRE-COOLER EXHAUST DUCTS. THESE WAS FOUND ON BOTH OF OUR PYLONS. I HAVE REACHED OUT TO OTHER OPERATORS AND THEY HAVE ALSO ACKNOWLEDGED THSDR WI5R201811190001Rotor · fracturedDURING SHUTDOWN AN UNUSUAL SQUEAL WAS NOTED. INVESTIGATION REVEALED THE N1 SPOOL COULD NOT ROTATE AND BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE.
DISASSEMBLY OF THE ENGINE CONFIRMED TWO MISSING 3RD STAGE BLADES.SDR AMYR2018111500001Compressor Blade · brokenTROUBLESHOOTING A SUDDEN HIGH ITT SPLIT BETWEEN LT AND RT ENGINE AS REPORTED BY THE PILOT. PER LMM 71-00-00 FAULT ISOLATION FOR HIGH ITT, PERFORMED A BORESCOPE OF HP AND IP COMPRESSOR AND FOUND SIGNIFICANT DAMAGE TO BOTH HP AND IP COMPRESSORS. APPEARS THERE WASDR WI5R201811090001Blade · fracturedDURING TAKE-OFF A LOUD BANG WAS REPORTED. POST FLIGHT BORESCOPE INSPECTION REVEALED A MISSING 3RD STAGE IP BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED ONE MISSING 3RD STAGE BLADE.SDR WI5R2018102900000Blade · fracturedDURING TAKEOFF, THE PILOT REPORTED A LOUD BANG AND A 50 DEG C ITT SPLIT. BORESCOPE INSPECTION INDICATED A MISSING 3RD STAGE IP BLADE. IN ADDITION, A ZONE 2 ITT EXCEEDANCE WAS RECORDED IN THE FADEC FILES, 915.6 DEG C FOR 2.8 SECONDS. DISASSEMBLY OF THE ENGINSDR WI5R2018100500000Rotor · fracturedTHE CUSTOMER NOTED A CONSTANT RATTLING NOISE DURING ENGINE SPOOL DOWN. FIELD BORESCOPE INSPECTION REVEALED A LIBERATED 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED A MISSING 3RD STAGE BLADE.SDR WI5R2018092800002Rotor · fracturedDURING TROUBLESHOOTING FOR ITT, N2, AND FUEL FLOW SPLITS WITH THE SISTER ENGINE, BORESCOPE INSPECTION REVEALED A MISSING 3RD STAGE IP BLADE AND DAMAGE TO THE HPT BLADES. DISASSEMBLY OF THE ENGINE CONFIRMED A MISSING 3RD STAGE BLADE.SDR WI5R201809280001Rotor · fracturedDURING CRUISE A POPPING NOISE WAS REPORTED FOLLOWED BY AN ENGINE VIBRATION AND RISE IN ITT. BORESCOPE INSPECTION REVEALED A MISSING 3RD STAGE IP BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED A MISSING 3RD STAGE BLADE.SDR AMCR20180712004Tee Fitting · crackedTHE T-FITTING TO THE OXYGEN SYSTEM PRESSURE GAUGE AND TRANSDUCER HAS A CRACK ON ONE END. THE CRACK WAS FOUND VISUALLY AFTER IT WAS DETECTED ON TWO OTHER CJ4 AIRCRAFT.SDR WI5R201806290001Rotor · fracturedIN A PROACTIVE TREND ANALYSIS, THIS ENGINE WAS FLAGGED FOR N2 AND ITT SHIFTS. FIELD BORESCOPE INSPECTION INDICATED DAMAGE TO THE IP AND HPC COMPRESSORS. DISASSEMBLY OF THE ENGINE CONFIRMED A MISSING 3RD STAGE BLADE.SDR AMCR20180628003Tee Fitting · crackedBASED ON AN OBSERVATION WITH ANOTHER AIRCRAFT RECENTLY IN WHICH A CRACKED O2 TEE FITTING WAS FOUND, MAINTENANCE CHECKED THE FITTING ON THIS AIRCRAFT AT FIRST OPPORTUNITY. EVEN THOUGH THERE WERE NO LEAKS PRESENT, 2 OUT OF 3 PORTS ON THIS FITTING WERE FOUND CRACSDR AMCR20180620002Tee Fitting · crackedMAINTENANCE, SUSPECTING A LEAK IN THE O2 SYSTEM, OBSERVED MORE-THAN-USUAL O2 LOSS OVERNIGHT. SUBSEQUENT INVESTIGATION FOUND THREE CRACKS IN THE ALUMINUM T-FITTING NEAR THE BOTTLE, WHICH CONNECTS THE O2 TO THE PRESSURE GAUGE AND THE TRANSDUCER. IT APPEARS THE FSDR WI5R201804170001Rotor · fracturedMAINTENANCE PERSONNEL REPORTED HEARING 2 COMPRESSOR STALLS WHEN THE AIRCRAFT TOOK OFF. A ZONE 1 EXCEEDANCE WAS RECORDED AND 4 DAYS LATER A ZONE 2 EXCEEDANCE WAS RECORDED. A BORESCOPE INSPECTION FOUND A MISSING IPC ROTOR BLADE AND DAMAGE TO THE HPC ROTOR AND SDR 2018FA0000132Vane · departedDURING ROUTINE INSPECTION, ENGINE TREND DATA WAS DOWNLOADED AND SENT IN FOR ANALYSIS. NOTED A ZONE 2 OVERTEMP ON THE RIGHT ENGINE AND BORESCOPE REVEALED DAMAGE TO THE HP COMPRESSOR BLADES FROM FOD. FURTHER INSPECTION REVEALED THAT A INTERSTAGE COMPRESSOR VANSDR WI5R201803290002Compressor · damagedENGINE WAS RETURNED TO THE REPAIR STATION FOR BIRD INGESTION. POST EVENT BORESCOPE INSPECTION REVEALED DAMAGE TO THE IP AND HP COMPRESSOR. DISASSEMBLY DID NOT FIND ANY EVIDENCE OR BIRD INGESTION. THE IP ROTOR WAS MISSING A 3RD STAGE BLADE.SDR WI5R20180226001Blade · fracturedENGINE WAS REMOVED DUE TO HIGH 1E LP VIBRATIONS. DISASSEMBLY OF THE ENGINE CONFIRMED A MISSING 3RD STAGE IP COMPRESSOR BLADE.SDR WI5R2017110700001Blade · missingTHE ENGINE WAS RETURNED TO THE REPAIR STATION DUE TO DAMAGE NOTED ON THE HP COMPRESSOR ROTORS. DISASSEMBLY DISCOVERED TWO MISSING 3RD STAGE IP COMPRESSOR BLADES. THERE WAS NO EVIDENCE OF UPSTREAM FOREIGN OBJECT DAMAGE.SDR WI5R.20171102Rotor · fracturedDURING FL400, THE PILOT REPORTED POP NOISE AND FELT A SMALL YAW FOLLOWED BY A SLIGHT LOW PITCH SOUND. POST FLIGHT BORESCOPE INSPECTION FOUND DAMAGE TO THE IP AND HP ROTOR BLADES. DISASSEMBLY CONFIRMED A MISSING 3RD STAGE IP COMPRESSOR BLADE. THERE WAS NO EVSDR 2019FA0000008Compressor · damagedPILOT REPORTED JUST AFTER TAKEOFF A LEFT ENGINE HIGH ITT. PILOT RETURNED TO AIRPORT AND A BORESCOPE INSPECTION WAS PERFORMED. INSPECTION FOUND TWO MISSING BLADES FROM IP COMPRESSOR ROTOR AND SUBSEQUENT DAMAGE TO THE HP COMPRESSOR.SDR WI5R20170630002Rotor · fracturedDURING TROUBLE SHOOTING FOR HIGH ITT, FIELD BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE HAS CONFIRMED THE FIELD FINDING.SDR WI5R201706300001Rotor · fracturedDURING TAKEOFF, REPORTED A POPPING NOISE. POST FLIGHT FIELD BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE HAS CONFIRMED THE FIELD FINDING.SDR WI5R201705010001Blade · fracturedTHE ENGINE WAS RETURNED TO THE REPAIR STATION FOR DAMAGE TO HPC ROTOR NOTED DURING A BORESCOPE INSPECTION. THE OPERATOR NOTED A 30 INCREASE IN ITT AND 200 RPMS IN N2. FIELD BORESCOPE INSPECTION REVEALED DAMAGE TO THE HPC ROTOR. THE ENGINE WAS RETURNED TO THSDR WI5R201704250001Blade · failedFJ44-4A, ENGINE WAS RETURNED TO THE REPAIR STATION FOR A MISSING 3RD STAGE IP COMPRESSOR BLADE. FIELD TROUBLE SHOOTING FOR AN UNUSUAL NOISE DURING ENGINE SHUTDOWN DISCOVERED DAMAGED 3RD STAGE IP BLADES. DISASSEMBLY REVEALED THE 3RD STAGE IP ROTOR BLADE WAS MSDR WI5R201701170001Blade · fracturedENGINE WAS SQUAWKED FOR HIGH 1E N1 VIBRATION DURING POST CHECK 3 ON WING MAINTENANCE. DISASSEMBLY REVEALED ONE LIBERATED 3RD STAGE BLADE ON THE IP ROTOR.SDR AMCR20161031003Wire · corrodedCREW EXPERIENCED AN AILERON TRIM FAIL. INVESTIGATION REVEALED NO CONTINUITY IN TRIM WIRE FROM THE AILERON TRIM ACTUATOR. VISUAL INSPECTION REVEALED A NICK IN WIRE NEXT TO CONNECTOR WITH APPARENT CORROSION. STRIPPING THE WIRE BACK FROM CONNECTOR PIN FOUND CORROSDR 2016FA0000380Tat Probe · failedENGINE CONTROL SYS FAULT LT - RT EICAS MESSAGE DISPLAYED IN CRUISE FLIGHT AT FL320. CREW TURNED AROUND AND RETURNED TO ORIGIN AIRPORT AND LANDED WITHOUT INCIDENT. DETERMINED FAILURE OF TT2 SENSOR ON NR 2 ENGINE. SENSOR CHANGE AND AIRCRAFT OPERATED WITHOUT FSDR 2016F00162Elbow · brokenAT DEPARTURE. AIRCRAFT STARTED ROLLING ON TAXIWAY AND BRAKE TEST PERFORMED. BRAKE PRESSURE LOW AND ANTISKID FAIL ALARM WARNING ON. FLIGHT CREW NOTICE THAT THE NORMAL BRAKING IS INOPERATIVE, THE CBD ACTIVATES THE EMERGENCY BRAKING, RETURN TO BLOCKS. AIRCRAFT SDR WI5R2016050200001Blade · fracturedENGINE WAS SQUAWKED FOR SQUEALING NOISE DURING ENGINE SHUTDOWN. FIELD BORESCOPE INSPECTION REVEALED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY REVEALED ONE LIBERATED 3RD STAGE BLADE ON THE IP ROTOR.SDR YMHA2016FA0000189Sensor · dirtyPILOT DECLARED AN EMERGENCY AND LANDED, DUE TO A FORWARD BAGGAGE COMPARTMENT SMOKE DETECTOR LIGHT AND AUREL WARNING. AFTER LANDING AND EVACUATING AIRPLANE THE FORWARD BAGGAGE AREA WAS OPENED UP AND INSPECTED FOR SMOKE OR THE ODOR OF SMOKE, NONE WAS FOUND. HASDR AMCR2016033101Carbon Seal · wornUPON POSTFLIGHT INSPECTION, FOUND OIL POOLING BELOW RT ENGINE DRAIN MAST. REMOVAL OF COWL REVEALED OIL ON THE ALTERNATOR QAD AND DRIPPING FROM SEAL CAVITY. FOUND THE LT ENGINE WITH OIL ALSO, BUT LESS OF IT. CARBON SEAL WAS CHANGED ON RT ENGINE, THEN THE LT
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