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 = '525A' 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 = '525A' 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 CVGA2018091805002Firewall · crackedINSPECTION REQUIREMENTS OF DOCUMENT 18, TASK 54-51-00-210 REVEALED RT ENGINE PYLON FIREWALL BOX ASSEMBLY IS CRACKED ON THE FORWARD PART OF THE BOX FROM THE OUTBOARD EDGE TO THE INBOARD RADIUS OF THE FIREWALL BOX APPROX .750" IN LENGTH, P/N 6312204-65. SERVICE SDR DBCA2018090400054Motor · failedDURING LIVE LEG PILOT NOTED AIR CONDITIONING WASN'T WORKING. LANDING IN CZBM WAS UNEVENTFUL. TECHNICIANS TROUBLESHOT TO BAD CURRENT LIMITER AND VCCS MOTOR. REMOVED AND REPLACED MOTOR. OPERATIONS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR WI5R201808031116Rotor · fracturedENGINE HAD LIBERATION OF AN IP ROTOR BLADE AND DAMAGE TO THE HPC ROTOR. THE COMPRESSOR STALLED DURING OPERATION. FIELD BORESCOPE INSPECTION REVEALED A LIBERATED IP BLADE AND DAMAGE TO THE HPC ROTOR.SDR 3EJA 201808100001Warning Light · illuminatedGEAR UNLOCK LIGHT AFTER TAKEOFF. CHECKLIST FOLLOWED, CLEARED THE LIGHT.SDR CVGA20180608002Indicator · no indicationRIGHT MAIN GEAR LIGHT WOULD NOT ILLUMINATE WITH GEAR HANDLE SELECTED DOWN. EMERGENCY GEAR EXTENSION WAS PERFORMED PRIOR TO LANDING AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED AND TAXIED IN WITHOUT INCIDENT.SDR E07A201803270001Display · defectiveWHILE ENROUTE, THE AIRCRAFT MULTIFUCTION DISPLAY WENT BLANK. CREW COMPLIED WITH A SCREEN REVERSION, AND DIVERTED . MAINTENANCE DETERMINED THE MFD TO BE DEFECTIVE. REPLACED MFDSDR CA190301008Transducer · failed(CAN) CREW: SHORTLY AFTER DEPARTURE ON AN EMPTY LEG, HAD A LEFT HAND LOW OIL PRESSURE INDICATION WITH NO ASSOCIATED MASTER WARNING. AFTER RUNNING THE CHECKLISTS WE RETURNED TO XXXX, WITH THE ENGINE IN THE IDLE POSITION. NO OTHER ISSUES. MAINTENANCE: OIL PX TRSDR CVGA20180302001Clamp · loosePRESSURIZATION LEAK IN AREA OF MAIN CABIN DOOR. AUDIBLE NOISE CAME ABOUT QUICKLY, CABIN ALTITUDE BEGAN TO RISE AND CONTINUED TO RISE UNTIL STABILIZED AT 10,000 MSL (0 DIFF). DOOR SEAL ANNUNCIATOR NEVER ILLUMINATED. WHILE TROUBLESHOOTING, FOUND A LOOSE HOSE CLASDR E07A201802280001Actuator · failedDURING TAXI CREW WAS PERFORMING PRETAKEOFF CHECKS AND RECEIVED HYD FLOW LOW L/R. CREW RETURNED TO RAMP. HYDRAULIC FLUID WAS FOUND LEAKING OUT OF LT WING IN THE SPEED BRAKE AREA. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND THE LT SPEED BRAKE ACTUATOR WAS FOUSDR XMXR2018021500001Precooler · leakingPNEUMATIC SYSTEM RT BLEED AIR PRE-COOLER P/N 9914402-4 OR 8161-2 S/N S4883T0680 FOUND AREAS ON PRE-COOLER ASSEMBLY THAT HAVE BEEN LEAKING BLEED AIR INTO PYLON AREA. PART HAS A LIFE LIMIT OF 3500 HOURS OR 108 MONTHS WHICHEVER OCCURS FIRST. DEFECTIVE PART ONLY HSDR CVGA20171128001Landing Gear · malfunctionedGEAR WOULD NOT RETRACT WHEN GEAR HANDLE SELECTED UP. EMERGENCY WAS DECLARED. OPENSDR WI5R2017111600001Blade · failedDURING TROUBLESHOOTING FOR HIGH ITT, THE ENGINE WAS BORESCOPE INSPECTED AND FOD WAS DISCOVERED ON THE HPC ROTOR. DISASSEMBLED REVEALED THIS WAS SECONDARY DAMAGE. ONE OF THE THIRD STAGE IP ROTOR BLADE FROM IPC ROTOR ASSEMBLY LIBERATED AT THE ROOT. DISASSEMBLSDR WI5R201710110001Blade · missingENGINE WAS RETURNED TO THE REPAIR STATION FOR DAMAGE TO THE IPC AND HPC ROTOR. THE DAMAGE WAS DISCOVERED DURING TROUBLESHOOTING FOR BLEED ODOR AND HIGH OIL CONSUMPTION. THE ENGINE WAS DISASSEMBLY DISCOVERED A MISSING THIRD STAGE IP ROTOR BLADE. IN ADDITION,SDR 2017F00158Door Seal · rupturedCREW INITIATED DESCENT FROM FL390. PASSING THROUGH FL380 THEY NOTICED A HISSING NOISE COMING FROM THE MAIN CABIN DOOR AREA, SHORTLY FOLLOWED BY A "DOOR SEAL" ANNUNCIATOR. THE CABIN ALTITUDE STARTED TO RISE RAPIDLY SO THEY INITIATED AN EMERGENCY DESCENT AND LEVSDR E07A2017083100001Intercooler · blew outDURING CRUISE, CREW NOTICED HIGH ITT ON THE LT ENGINE AND THEN RECEIVED CAS WARNING OF DUCT OVERTEMP. DIVERTED AND LANDED WITHOUT INCIDENT. FOUND THE LT BLEED AIR DUCT INTERCOOLER HAD A HOLE IN IT.SDR CVGA20170815001Connector · damagedPOWER BRAKE LOW PRESSURE INDICATION UPON APPROACH. DIVERTED TO UTILIZE A LONGER RUNWAY. EMERGENCY WAS DECLARED. LANDED UNEVENTFULLY. MAINTENANCE FOUND PUSHED PIN AT LANDING GEAR HANDLE CONNECTOR.SDR 2017FA0000341Rivet · looseTHE INBOARD LEADING EDGE RIVETS, LH AND RH, LOOSEN AND WEAR. SOME STEMS AND COLLARS FALL OUT. REPLACED APPROXIMATELY 150 RIVETS, ON EACH WING. THIS ACFT HAS A TOTAL TIME OF 4518 HOURS AND 4149 LANDINGS.SDR 2017F00157Door Seal · rupturedCREW NOTICED A "DOOR SEAL" ANNUNCIATOR IN CRUISE FOLLOWED BY A HISSING NOISE. THEY INITIATED A DESCENT TO FL300 AND THE NOISE STABILIZED, CABIN PRESSURE WAS NORMAL. ON LANDING IT WAS DISCOVERED THAT THE INFLATABLE DOOR SEAL HAD RUPTURED IN THE TOP AFT CORNER. SDR CVGA20170728001Cap · missingLOW OIL PRESSURE INDICATION DURING CRUISE FLIGHT AT FL210 APPROXIMATELY 15 MINUTES AFTER TAKEOFF. QRH CHECKLIST COMPLETED. N2 REDUCED TO <80% AS PER QRH. OIL PRESSURE INDICATED IN NORMAL RANGE. EMERGENCY DECLARED AND ELECTED TO RETURN TO DEPARTURE. OIL PRSDR 7S1A20170616Outflow Valve · failedEXPERIENCED CABIN ALTITUDE CLIMBING ENROUTE TO FL 430. REQUESTED DESCENT AND DIVERTED TO UNSCHEDULED LANDING. TROUBLESHOT PROBLEM AND FOUND DEFECTIVE PRIMARY OUTFLOW VALVE, INTERMITTENT CONTROL SOLENOID. REPLACED PRIMARY OUTFLOW VALVE WITH OVERHAULED UNIT PARSDR WI5R201702270001Shaft · separatedENGINE WAS RETURNED TO THE REPAIR STATION DUE TO METAL IN THE OIL. DURING FLIGHT, THE CUSTOMER NOTED A 40 DEGREE C ITT SPLIT BETWEEN ENGINES ACCOMPANIED BY CABIN BLEED-ODOR. POST FLIGHT, THE ENGINE IN QUESTION WAS GROUND TESTED FOR TROUBLE SHOOTING. SHORTLYSDR 2016F00241Signal Cond Unit · failedON CLIMB OUT AT APPROX. 1000FT FUEL QTY GAUGES BLANKED OUT AND STARTED BEHAVING ERRATICALLY WITH QUANTITY DISPLAYING BETWEEN EMPTY AND FULL. PILOT ELECTED TO DIVERT TO A MAINTENANCE FACILITY AND MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING REVEALED THE FUEL QTYSDR 2016FA0000576Uplock Hook · crackedCREW HAD A GEAR UNSAFE WARNING LIGHT IN CRUISE FLIGHT AND HYDRAULIC PRESSURE WAS FLUCTUATING WITH EXCESSIVE AIRFRAME VIBRATION. AIRCRAFT MADE AN UNEVENTFUL LANDING AT DESTINATION AIRPORT. ON LANDING, INSPECTION REVEALED FRACTURED LT MLG UPLOCK HOOK.SDR 2016F00215Uplock Hook · brokenON CLIMB OUT, LANDING GEAR UNSAFE RED LIGHT CAME ON AND VIBRATION WAS FELT. MADE UNEVENTFUL LANDING AT SAME AIRPORT AND DISCOVERED RT UP-LOCK HOOK BROKEN.SDR 3EJA20161025001Fcu · failedAIRCRAFT ON APPROACH AT 5000FT. PF RETARDED THROTTLES TO IDLE TO SLOW DOWN AND RT ENGINE FLAMED OUT. SECURED ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED UNEVENTFULLY. MANUFACTURER DETERMINED THAT THE FCU IS THE CAUSE OF THIS PROBLEM.SDR VIBR20161014001Seat Track · crackedDURING INTERIOR REFURBISHMENT, TWO SEAT TRACKS WERE FOUND TO BE CRACKED AT THE ROLLERS.SDR 9JLA2016101711306Uplock Switch · defectiveAFTER TAKEOFF THE CREW REPORTED THAT THERE WAS THREE LOUD POPS DURING THE LANDING GEAR RETRACTION FOLLOWED BY A NORMAL GEAR UP INDICATIONS. THE CREW ELECTED TO REPEAT A LANDING CYCLE WITH SAME RESULTS. THE CREW RETURNED BACK TO THE AIRPORT FOR INVESTIGATE. THESDR 3EJA20161004002Landing Gear · malfunctionedINITIALLY GEAR RETRACTED FINE, ABOUT 5 MINUTES INTO FLIGHT HYDRAULIC PRESSURE LIGHT CAME ON AND RED GEAR UNLOCKED LIGHT CAME ON. JET SHOOK BAD, SELECTED GEAR DOWN, THREE GREEN INDICATED SHAKING WENT AWAY. LANDING UNEVENTFUL.SDR 2016FA0000460Engine · overheatedDURING CLIMB, THE LT ITT JUMPED INTO THE RED ON THE INDICATOR. PILOT IMMEDIATELY REDUCED POWER AND DIVERTED. ON INITIAL EXAMINATION FOUND PAINT ON LT STUB WING AND SURROUNDING AREA INDICATING HEAT DAMAGE. ALSO OBSERVED PYLON SKINS WARPED AND RIPPLED.SDR CVGA20160804001Uplock · crackedWHILE BEING VECTORED BY ATC FOR VISUAL APPROACH TO DESTINATION, THERE WAS AN UNCOMMANDED FREE FALL EXTENSION OF AT LEAST 1 OF THE LANDING GEAR AND A THUMPING RESULTING FROM THE HYDRAULIC SYSTEM TRYING TO RETRACT IT BACK INTO POSITION. RECOGNIZING THE SITUATIOSDR CVGA201607250001Engine · flamed outLEFT ENGINE FLAMED OUT AT 3,000 FT DURING APPROACH, CREW WAS ABLE TO RE-START ENGINE SUCCESSFULLY AND LANDED WITHOUT ANY ISSUES. NO EMERGENCY DECLARED.SDR CVGA20160705001Uplock Hook · crackedTHROUGH 6000, LOUD VIBRATION, SIGNIFICANT YAW. RIGHT MLG INDICATION DOWN AND LOCKED. THIS WAS ON APPROACH TO MGN. OTHER GEAR SELECTED DOWN AND CAME DOWN LIKE THEY SHOULD. WITH OTHER GEAR SELECTED DOWN, AIRCRAFT DIVERTED TO PLN WITHOUT ISSUE. UPON INVESTIGATIOSDR W9BA2016F00148Engine · shutdownDESCENDING THROUGH 10,000 MSL, THE THROTTLES WERE RETARDED TO IDLE. THE RT ENGINE IMMEDIATELY ROLLED BACK AND SHUTDOWN. LEFT THROTTLE WAS ADVANCED TO MAINTAIN AIRSPEED AND ALTITUDE. IGNITIONS WERE TURNED ON IAW THE CHECKLIST AND THE RT ENGINE STARTED BACK USDR CVGA2016FA0000308Cowling · separatedDURING THE DESCENT, AT ABOUT 20,000 FT, THE BOTTOM COWLING FOR THE NR 1 ENGINE DETACHED FROM THE ACFT. AFTER DETACH AND THE SUBSEQUENT TURBULENCE, THE CREW DISABLED AUTOPILOT AND HAND FLEW THE ACFT ALL THE WAY TO THE GROUND. INSPECTION OF THE ACFT UPON LANDISDR 2016FA0000081Cowl Door · departedTHE LT ENGINE LOWER COWL SEPARATED SHORTLY AFTER TAKEOFF. POST FLIGHT INSPECTION REVEALED THE THREE MOST INBD FORWARD FASTENERS MISSING. ALL OTHER FASTENERS REMAINED INSTALLED IN THEIR RECEPTACLES AFTER SEPARATION WITH THE EXCEPTION OF TWO RANDOM MISSING FASSDR CA160111013Connector · burned(CAN) EMERGENCY LIGHTS POWER SUPPLY, BATTERY FAILED INSPECTION, DURING INSPECTION BURNING ODOR NOTED. ASSY WAS INVESTIGATED AND FOUND MAIN CONNECTOR TO BATTERY PACK WAS BURNED.SDR CA150730012Brushes · worn(CAN) CREW REPORTED THAT THE AIRCONDITIONING SEEMED WEAK AND WAS NOT COOLING THE AIRCRAFT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE VCS COMPRESSOR MOTOR DAMAGED DUE TO OVER WORN BRUSHES. MORE DETAILED INSPECTION TO BE COMPLETED ONCE THE MOTOR IS REMOVED.SDR CVGA20150723005Unknown · odorDURING DESCENT, REPORTED A STRONG BURNING SMELL ALONG WITH A LT BLEED OVERHEAT WARNING. NO EMER WAS DECLARED & CONTINUED TO PLANNED AIRPORT. THE SMELL & WARNING DIMINISHED & THE ACFT LANDED SAFELY. TROUBLESHOOTING WAS UNABLE TO FIND A FAULTY OR DISCREPANCY.SDR 3EJA2015FA0000327Landing Gear · malfunctionedDURING DECENT, A HYDRAULIC PRESSURE LIGHT ILLUMINATED AND RED GEAR UNLOCK LIGHT STEADY FLASHED WITH ASSOCIATED THUMPING. PULLED GEAR CONTROL CIRCUIT BREAKER AND HYDRO LIGHT EXTINGUISHED BUT RED "GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. RIGHT MAIN GEAR DOWN SDR 2015FA0000263Anti-Skid Valve · failedTHE ANTI-SKID CONTROL VALVE FAILED WHEN LANDING CAUSING RT TIRE TO BLOW OUT AND ACFT VEERING OFF SIDE OF RUNWAY. THIS UNIT WAS SENT TO MFG AND FAILED BENCH CHECK.SDR 3EJA2015F00072Controller · inoperativeCABIN LOST PRESSURE DESCENDING OUT OF FL430. CABIN HELD AT 14,000 DIFFERENTIAL THROUGH THE MID 20'S. NO ASSOCIATED NOISE, SLOW DEPRESS.SDR 3EJA2015F00065Cabin Pressure · malfunctionedCABIN PRESSURIZATION ISSUE DURING DESCENT. TROUBLESHOOTING ACFT NATURE OF FAILURE UNKNOWN.SDR 3EJ2015F00000Cabin Pressure · unknownCABIN PRESSURIZATION ISSUE UPON INITIAL DECENT FROM FL430 IN ROUTE. DESCENDED TO FL 10,000 AND LANDED UNEVENTFUL. OPENSDR CA150414005Line · chafed(CAN) ON VISUAL INSPECTION OF EMPANAGE TAIL SECTION, IT WAS NOTED THAT THE DE-ICE LINE WAS MOUNTED IN SUCH A FASHION THAT IT WAS RUBBING AGAINST THE LIGHTNING HOLE. THE LINE WAS CHAFED AND RENDERED UNSERVICEABLE.SDR WI5R2015032500001Blade · missingDURING OPERATION A "HOOTING" SOUND WAS PRESENT FROM IDLE THOUGH MCT POWER SETTING. A FIELD BORESCOPE INSPECTION REVEALED 1 OF THE IP COMPRESSOR BLADES HAD LIBERATED. THE REPAIR STATION INVESTIGATION HAS CONFIRMED THE FIELD FINDINGS. THERE WAS NO EVIDENCE OF SDR E07A20150305001Display · malfunctionedCREW NOTICED SMOKE COMING FROM BEHIND INSTRUMENT PANEL WHILE PREFORMING PREFLIGHT WITH ELEC & AVIONIC POWERED ON. CREW TURNED OFF BATTERIES & DISCOUNTED APU. DETERMINED RT FLIGHT DISPLAY WAS SMOKING. INSTALLED OVERHAULED UNIT. ACFT WAS RETURNED TO SERVICE.SDR WI5R201502050001Blade · missingDURING INSPECTION, ENGINE 3RD IP COMPRESSOR BLADES WAS FOUND LIBERATED AT THE MIDSPAN. ADDITIONAL DAMAGE WAS NOTED ON THE LE OF THE HPC ROTOR.SDR CVGA20140905001Door Seal · damagedDURING DECENT THROUGH THE ACFT BEGAN TO DEPRESSURIZE. AN EMER DESCENT WAS PERFORMED IAW THE CHECKLIST.SDR WI5R2014071100001Blade · damagedENGINE WAS RETURNED TO THE REPAIR STATION FOR DAMAGE NOTED ON THE HPC ROTOR BLADES. THE ENGINE WAS BEING BORESCOPE INSPECTED FOR TAP BLUE ENROLLMENT AND NO OPERATIONAL ISSUES WERE NOTED. DISASSEMBLY REVEALED HPC ROTOR, PN 60442, SN LC2613 LIBERATED THE OUTERSDR WI5R2014071000001Rotor · damagedDURING BORESCOPE INSPECTION FOR TAP ENROLLMENT, DAMAGE WAS NOTED ON THE LEAD EDGE OF THE HPC ROTOR. DISASSEMBLED REVEALED THIS WAS SECONDARY DAMAGE. 1 OF THE 3RD STAGE IP ROTOR BLADE FROM IPC ROTOR ASSY 61968, AU01065 LIBERATED AT THE ROOT.
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