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 = '400A' 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 = '400A' 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 RK270Downlock Switch · faultyMLG DID NOT EXTEND WITH NORMAL SYSTEM. EXTENDED GEAR WITH AUX SYSTEM. INSTALLED NEW NLG DOWNLOCK/NOT LOCKED SWITCH.SDR 2002FA0001195Rivet · erodedHIGH TURBINE BLADE RETAINING RIVETS AND COLLARS APPEAR TO BE SUFFERING EROSION, CAUSING RIVET TAILS TO FALL BELOW THE .050 INCH PROTRUSION AS OUTLINED IN MFG MM. IF LEFT IN SERVICE THIS SITUATION COULD CAUSE THE HIGH TURBINE BLADES TO SHIFT AND/OR FAIL, CAUSISDR S3898Rivet · erodedHIGH PRESSSURE TURBINE BLADE RETAINING RIVETS AND COLLARS APPEAR TO BE SUFFERING EROSION CAUSING RIVET TAILS TO FALL BELOW THE .050 INCH PROTRUSION AS OUTLINED IN THE MFG SB. IN ITS CURRENT CONDITION ALL 71 EA. RIVETS (PN 311588901) COLLARS (PN 311683801) ARE SDR 61820022Contactor · burnedHORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT.SDR 6182002Contactor · burnedHORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT.SDR 071602Relay · failedTAIL DE-ICE INOP.SDR 2002FA0000919Downlock Switch · failedNOSE LANDING GEAR DOWNLOCK LIGHT DID NOT COME ON AFTER DEPLOYMENT OF LANDING GEAR. GEAR CYCLED SEVERAL TIMES AND STILL NO DOWN AND LOCK LIGHT ILLUMINATION. TOWER FLY BY PERFORMED AND CONFIRMED DEPLOYMENT. AIRCRAFT LANDED SAFELY. NEW SWITCH INSTALLED.SDR 613023Contactor · failedHORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT.SDR 613022Contactor · failedHORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT.SDR 613021Contactor · failedHORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT.SDR 81TJ42002Skin · chafedFUSELAGE BELLY SKIN CHAFED JUST AFT OF NOSE LANDING GEAR AREA.SDR 81TJ41902Skin · chafedLEADING EDGE SKIN PANEL OF RIGHT PYLON HAS CHAFED HOLE FROM CONTACT WITH COWLING.SDR 81TJ41802Skin · crackedRIGHT UPPER MIDDLE ENGINE PYLON SKIN DUE TO CRACKING AT LOCATION OF PRE-EXISTING REPAIR OF HOLE AND CRACK IN SKIN.SDR DJFA0127Contactor · failedHORIZONTAL STAB ANTI-ICE INOPERATIVE. HORIZONTAL STAB ICE FAIL WARNING LIGHT COMES ON IMMEDIATELY WHEN HORIZONTAL STAB ANTI-ICE IS TURNED ON. RECYCLED CIRCUIT BREAKERS AND SWITCHES NUMEROUS TIMES. GROUND CHECKS OK. NUMEROUS FAILURES (73) OF THIS PART ON OUSDR 0127Nut · looseAIRCRAFT WAS ON DESCENT INTO MSP, AFTER REDUCING POWER THE ENGINE KEPT SPOOLING DOWN AT THAT POINT THE PILOTS SHUT THE ENGINE DOWN. ACFT LANDED WITH NO FURTHER PROBLEMS. INVESTIGATION REVEALED THE HMU LEVER NUT HAD LOOSENED UP ENOUGH TO ALLOW THE LEVER TO SLSDR 0128Uplock · out of adjAIRCRAFT DURING APPROACH NOSE GEAR DEPLOYED. GEAR WAS CYCLED AND THEN DEPLOYED WITH THREE GREEN LIGHTS. FOUND NOSE GEAR UPLOCK HOOK OUT OF ADJUSTMENT AND NOSE STRUT UNDER SERVICED. UPLOCK HOOK WAS REGID AND NOSE GEAR WAS SERVICED.SDR RASFTYRK195Mount Bracket · crackedCRACK FOUND IN LT FORWARD ENGINE MOUNT BRACKET WHILE PERFORMING FLUORESCENT PENETRANT INSPECTION AS PER RAYTHEON AIRCRAFT SAFETY COMMUNIQUE NR 189.SDR RASFTYRK198Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF.SDR 0122Switch · out of adjAIRCRAFT WAS DEPARTING DENVER, AT 90 KTS THE DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF AND MAINTENANCE INSPECTED DOOR SWITCH AND ADJUSTED. NO FURTHER PROBLEMS WERE NOTED.SDR RASFTYRK183Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF.SDR RASFTYRK180Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF.SDR RASFTYRK178Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 50 PERCENT THROUGH THE LOWER HALF.SDR RASFTYRK189Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 80 PERCENT THROUGH THE LOWER HALF.SDR 2002FA0000013Mount · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT TO BE CRACKED.SDR 2001F00640Connector · dirtyRIGHT ENGINE ELECTRONIC FUEL CONTROL (EFC) ANNUNCIATOR ILLUMINATED. OBTAINED FERRY PERMIT FROM ROC TO PTK. CLEANED WIRING CONNECTORS AT ENGINE TEMPERATURE SENSOR CONNECTOR, ELECTRONIC ENGINE CONTROL (EEC) WIRING CONNECTOR AND EEC FIREWALL WIRING CONNECTOR. SDR 2001F00642Warning Light · malfunctionedMOMENTARY ELECTRONIC FUEL CONTROL (EFC) LIGHT ON RIGHT ENGINE. RAN UP ENGINE, PERFORMED CHECK, COULD NOT DUPLICATE PROBLEM. (M)SDR AUS20011056Bolt · loose(AUS) LT MAIN WHEEL TIE BOLTS LOOSE. TIRE DEFLATED.SDR RK287Computer · failedRUDDER BOOST FAIL ON TAKEOFF ROLL. MASTER CAUTION FOLLOWED BY RUDDER BOOST FAIL ANNUNCIATOR.SDR 0120Switch · out of adjPILOTS HAD TO SHUT DOWN THE NR 1 ENGINE DUE TO A LEFT T/R DEPLOY LIGHT CAME ON. IT WAS A PRECAUTIONARY SHUTDOWN. DURING DESCENT THE T/R LIGHT WENT OUT AND THE PILOT RESTARTED THE ENGINE AND LANDED WITH NO FURTHER INCIDENCES. ADJUSTED THE T/R DEPLOY SWITCH ASDR FE62002F00000Converter · failedCONVERTER FAILED AND BEGAN TO MELT THE SIDEPANEL CARPET (WHICH WAS LYING ON TOP OF IT). AT THIS TIME THE CAUSE OF THE FAILURE IS UNCERTAIN.SDR 2001FA0000233Bolt · broken1 MAIN WHEEL TIE BOLT BROKE AND DEPARTED AIRCRAFT, RESULTING IN UNSEATING OF WHEEL HALF SEALING O-RING AND SUBSEQUENT LOSS OF AIR PRESSURE. BOLT WAS MAGNAFLUXED 14 HOURS PREVIOUS WITH NO DEFECTS NOTED.SDR 0118Valve · failedAIRCRAFT WAS AT 35,000 FT WHEN THERE WAS A SOUND OF RUSHING AIR ACCOMPANIED BY SMOKE IN THE CABIN AND THE COCKPIT. THE PILOT DECLARED AN EMERGENCY AND DESCENDED TO THE NEAREST AIRPORT (LAS) AND LANDED WITHOUT INCIDENT. THE PROBLEM WAS THAT THE EMERGENCY PRESSDR 0117Brake Assy · obstructedDURING TAXI AT FCI THIS AIRCRAFT EXPERIENCED A VIBRATION AND THEN THE LT BRAKE LOCKED UP. THE BRAKE WAS REMOVED AND DETERMINED THAT A SMALL SCREW HAD WEDGED ITSELF BETWEEN THE BRAKE PADS AND THE DISC AND BROKE SEVERAL OF THE BRAKE PADS LOOSE WHICH CAUSED THE SDR ERYARK71Brake · failedBRAKE FAILURE AFTER RETURN FROM RAYTHEON MAINTENANCE CENTER, FTY, FOR 3 PREVIOUS BRAKE FADING OCCURRENCES WITH 3 DIFFERENT PILOTS.SDR 00115Float · defectiveAIRCRAFT HAD A LOW FUEL PRESSURE INDICATION DURING LANDING. AIRCRAFT LANDED WITH NO PROBLEMS. FOUND FUEL LOW PRESSURE FLOAT DEFECTIVE. REPLACED FLOAT, OPS CHECKED OK.SDR 20010417AP004Rod · missingCABIN DOOR WILL NOT OPEN FROM INSIDE OR OURSIDE. AFT PINS DO NOT RELEASE WHEN HANDLE IS MOVED. FOUND THE ACTUATING ROD MISSING THE ROD END COTTER PIN. REINSTALLED THE PIN AND COTTER PINNED. OPERATION CHECK NORMAL.SDR DJFA00117Sensor · failedAIRCRAFT WAS FLYING AT FL330, HEARD A LOUD BANG AND THE CABIN RATE NEEDLE FLUCTUATED. SUSPECTED LOST PRESSURIZATION. INITIATED AN EMERGENCY DESCENT PROCEDURES. CABIN STARTED FILLING WITH BLACK SMOKE. ALSO NOTICED THE ACM FAIL LIGHT CAME ON. DECLARED AN EMSDR DJFA00116Cowling · buckledCOWLING BUCKELED, RIGHT SIDE LOWER INBOARD.SDR DJFA00115Cowling · buckledCOWLING BUCKELED, RIGHT SIDE LOWER INBOARD.SDR 00114Cowling · bentCOWLING ON LEFT HAND ENGINE BOTTOM INBOARD SIDE WAS BENT BACK DURING FLIGHT. THE CAUSE IS UNKNOWN, THESE COWLINGS ARE KNOWN TO HAVE THIS TYPE OF PROBLEM.SDR ERYA682D3Throttle Cable · frozenDURING FLIGHT FROM KLGA TO CYYZ AT FLIGHT LEVEL 310, THE RIGHT ENGINE THROTTLE FROZE IN POSITION. THE AIRCRAFT DECENDED TO 14000 FT. DURING THE APPROACH, THE THROTTLE WAS STILL FROZEN SO THE RIGHT ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. THE AIRCSDR RK180Bleed Valve · failedWHILE IN CRUISE FLIGHT FROM KBCT TO KBVT AT FL410 THE FLIGHT HEARD A LOUD BANG FOLLOWED BY OSCILLATIONS ON THE ROLL AXIS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED AT KLACY WITH NO FURTHER PROBLEMS. REPLACED RT ENGINE BLEED ACTUATOR VALVE PER PWCSDR 20001227SH009Contactor · failedTHIS CONTACTOR, PN 128-384054-5, WHEN INSTALLED IN THE K-251 POSITION OF THE HORIZONTAL STABILIZER DEICE SYSTEM CAUSES THE SYSTEM TO FAIL WHEN THE AIRCRAFT IS AT AN ALTITUDE THAT A MINUS 10 DEGREES OR COLDER RAM AIR TEMPERATURE IS ACHIEVED. (X)SDR 20001214SH026Drain Line · leakingLEAK DISCOVERED DURING A PITOT/STATIC LEAK TEST, THAT ONLY EVIDENCED ITSELF ABOVE 180 KNOTS. FOUND LEAK AT EPOXY GLUE THAT IS APPLIED TO ITS SIDE AT MFG. CONTACTED BEECH/BOMBARDIER, WHO, IN TURN, CONTACTED THE PART MFG. THEY ADVISED REPAIR OF LEAK IS AS EASSDR AU001081Connector · burned(AUS) BATTERY AIRCRAFT SIDE CONNECTOR POSITIVE TERMINALS BURNT AND MELTED. (X)SDR 20001207SH006Switch · out of adjFLAP ASYMMETRY LIGHT ILLUMINATED DURING LANDING. ADJUSTED LEFT FLAP FOLLOW-UP SWITCH OUTPUT VOLTAGE TO ASYMMETRY DETECTOR IAW WITH THE RAYTHEON 400/400A MM. OPERATIONAL CHECK GOOD. (X)SDR 20001018SH002Circuit Board · failedAFTER AIRCRAFT IS POWERED AND THE TRIM SYSTEM IS OPERATED FOR A FEW MINUTES, BOTH ROLL TRIM SURFACES STOP TRIMMING IN THE RIGHT WING LOW DIRECTION. REPLACING ROLL TRIM PC BOARD CORRECTS CONDITION. (X)SDR 20000911SH043Flux Detector · leakingUNIT LEAKED OIL OUT, GIVING HEADING ERRORS. (X)SDR 20000522SH008Sign · burnedFASTEN SEAT BELT/NO SMOKING SIGN BURNT. COULD HAVE CAUSED A FIRE. SUBMITTER STATED SHOULD BE INSPECTED AT 1500 HOURS. (X)SDR 20000426SH023Structure · noisyTHE FLIGHT CREW HAS REPORTED THAT AS THEY CLIMBED OUT TO ALTITUDE, THEY GET A LOUD BANGING NOISE IN THE AIRFRAME. THESE EVENTS HAPPENED AT 26,000 FEET, 28,000 FEET, 33,000 FEET AND AT 35,000 FEET, CABIN DIFF AT EACH OF THESE ALT WAS 6.5. WHEN THEY CAME BACK D
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