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 = '76' 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 = '76' 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 99ZZZX2102Rib · crackedDURING THE NORMAL INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS WHERE THE INBOARD AILERON HINGE PLATES (PN 105-100011-51) AND THE OUTBOARD AILERON HINGE PLATES (P/N 105-100011-51) ATTACH. THE SAME PROBLEM HAS BEEN FOUND ON OTHER AIRCRAFT OF SAME MODSDR CA990119016Crankcase · cracked(CAN) ON A SCHEDULED ON CONDITION INSPECTION, A CRACK WAS FOUND AT THE NR 2 CYLINDER HOLD DOWN STUD.SDR 99ZZZX634Light · intermittentNOSE GEAR DOWN LIGHT INTERMITTENT. TROUBLESHOT SYSTEM. REPLACED LIGHT ASSEMBLY. PROBLEM RECURRED. CONTINUED TROUBLESHOOTING. SWAPPED LIGHT ASSEMBLY WITH RT MAIN. PROBLEM WENT WITH LIGHT ASSY. REPLACED RT MAIN LIGHT ASSY WITH NEW. PROBLEM RECURRED ON RSDR AU981099Motor · malfunctioned(AUS) LANDING GEAR ELECTRIC MOTOR FAULTY. INVESTIGATION FOUND WORN BRUSHES. PART TC: 7,900.SDR CA981019008Power Pack · failed(CAN) LANDING GEAR FAILED TO EXTEND USING NORMAL EXTENSION SYSTEM. PILOT USED EMERGENCY GEAR EXTENSION AND LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED WORN GEAR MOTOR BRUSHES AND COMMUTATOR. HYDRAULIC POWER PACK REPLACED.SDR AU980779Switch · failed(AUS) NOSE LANDING GEAR DOWN MICROSWITCH FAULTY.SDR AU981220Switch · intermittent(AUS) NLG DOWN LIGHT MICROSWITCH INTERMITTENT. PART TC: 5,463.SDR 98ZZZX2608Skin · corrodedDURING SPOT INSPECTION OF AIRCRAFT UNDERGOING ANNUAL INSPECTION, NOTED BAGGAGE DOOR OUTER SKIN CORRODED ON LOWER HALF OF DOOR. CORROSION FROM INSIDE OF DOOR HAS PERFORATED SKIN IN 8 PLACES. DOOR SKIN WAS LOOSE APPROXIMATELY ONE-THIRD OF DOOR PARAMETER: BONDSDR AU980568Spring · broken(AUS) LT ENGINE, NR 2 CYLINDER INLET VALVE PUSHROD SHROUD TUBE RETAINING SPRING BROKEN IN HALF AND LYING IN THE BOTTOM OF THE ROCKER BOX.SDR AU980534Electric Motor · faulty(AUS) LANDING GEAR ELECTRIC MOTOR FAULTY. INVESTIGATION FOUND POOR CONTACT WITH THE THERMAL TRIP FITTED IN SERIES TO THE MOTOR BRUSH HOLDER.SDR AU980442Rib · cracked(AUS) WING RIBS (3 OF 4) CRACKED. PART TC: 7,731.SDR 98ZZZX1926Actuator · failedDURING FLAP EXTENSION, PILOT HEARD LOUD 'POP' FROM UNDER REAR SEAT AREA, AND FLAPS SNAPPED UP TO FULLY RETRACTED POSITION. INSPECTION REVEALED THAT FLAP ACTUATOR TUBE ASSY (ITEM 33 ON ATTACHED) HAD UN-THREADED FROM BALL NUT ON JACK SCREW. UNIT RE-ASSEMBLED, SDR 98ZZZX1595Solenoid · leakingINTERMITTENT HEATER OPERATION FOUND FUEL SOLENOID LEAKING THROUGH SAME HOLE IN SIDE OF SOLENOID THAT THE WIRING COMES OUT OF. FUEL PUDDLED UP IN DRAIN PAN, THEN DRAINED OVERBOARD. FUEL OVERBOARD DRAIN IS LOCATED DIRECTLY IN FRONT OF EXHAUST.SDR 98ZZZX1418Prop Lever · jammedLEFT PROPELLER WAS FEATHERED IN-FLIGHT FOR TRAINING. UNABLE TO INITIALLY GET PROPELLER LEVER BACK FORWARD. FINALLY, WHEN LEVER BROKE LOOSE, A LOUD SNAP WAS HEARD. PROPELLER CAME OUT OF FEATHER. LANDING WAS UNEVENTFUL. UPON INVESTIGATION, FOUND BOTH PROP LSDR AU980330Actuator · broken(AUS) LT MAIN LANDING GEAR ACTUATOR ROD BROKEN AT THE END OF THE THREADED SECTION.SDR AU980188Piston · cracked(AUS) PISTON CRACKED.SDR 98ZZZX720Rib · crackedFOLLOWING A WINDSTORM THAT BROKE THE GUSTLOCK, AN INVESTIGATION OF THE FLIGHT CONTROLS REVEALED CRACKS ON BOTH THE INBD AND OTBD WING RIBS AT THE AILERON BRACKET RIVETS.SDR 98ZZZX719Rib · crackedFOLLOWING A WINDSTORM THAT BROKE THE GUSTLOCK, AN INVESTIGATION OF THE FLIGHT CONTROLS REVEALED CRACKS ON BOTH THE INBD AND OTBD WING RIBS AT THE AILERON BRACKET RIVETS.SDR 98ZZZX173Mount · mismanufacturedUPON ARRIVAL OF A NEW ENGINE MOUNT, DISCOVERED TWO OF THE WELD JOINTS WERE DEFECTIVE. THE GUSSET PLATES ON BOTH UPPER BRACE ARMS WERE NOT WELDED DOWN, ONLY TACK-WELDED TO THE BRACE ARMS. THE MANUFACTURER SAID THAT ALTHOUGH IT WAS NOT CORRECT, SEVERAL UNITS HSDR 98ZZZX149Solenoid · failedCOMPLAINT OF OVERHEAT AND SHUT DOWN OF HEATER DURING GROUND OPERATION. INVESTIGATION OF HEATER OPERATION SHOWED HEATER NOT SHUTTING DOWN WITH TEMP CONTROL SWITCH. FOUND FUEL SOLENOID NOT CLOSING. OVERTEMP SENSOR WOULD THEN POP. FOUND BLACK SEALANT INSIDE SSDR AU971522Spring · broken(AUS) RH ENGINE MAGNETO IMPULSE COUPLING SPRING BROKEN.SDR AU971545Torque Tube · separated(AUS) PILOTS SIDE CONTROL COLUMN TORQUE TUBE BROKE OFF AT RIVETED JOINT DURING FLIGHT.SDR 97ZZZX4813Bendix Drive · failedBENDIX DRIVER FAILED AFTER 194 HOURS, REPLACED WITH SAME, FAILED AFTER 62 HOURS, REPLACED WITH SAME, FAILED AFTER 396.6 HOURS. REPLACED WITH EBB142A. EBB142A FAILED TO EXTEND AT 258 HOURS, CLEANED AND LUBED PER MFG, FAILED TO EXTEND AFTER 21 HOURS.SDR 98ZZZX1057Shock Strut · jammedBOLTS ATTACHING THE UPPER SHOCK STRUT ASSY TO THE UPPER GEAR HOUSING HAD SEVERE STRESS IN THE THREAD AREA. THIS WAS CAUSED BY REPEATED OPERATIONS IN FLIGHT TRAINING. BOLTS FAILED ALLOWING GEAR LEG TO EXTEND AND UPON RETRACTION, JAMMED ON LOWER WING SKIN RESUSDR 98ZZZX51Fitting · crackedINSPECTION FOUND LEFT WING ATTACH FITTING CRACKED.SDR 98ZZZX44Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.SDR 98ZZZX43Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.SDR 97ZZZX4250Bolts · looseDURING 100-HOUR INSPECTION, THE CENTER SECTION WING BOLTS THAT ATTACH THE LOWER WING SPAR PLATE TO THE WING SPAR (I.E., 20 WING BOLTS) WERE ALL FOUND UNDERTORQUED BY ONE-HALF TO ONE FULL TURN. THE NAS464P5 BOLTS SHOULD BE TORQUED 100-140 INCH/POUND.SDR 98ZZZX49Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.SDR 98ZZZX48Fitting · crackedINSPECTION FOUND LEFT AND RIGHT WING ATTACH FITTINGS CRACKED.SDR 98ZZZX42Fitting · crackedINSPECTION FOUND LEFT WING ATTACH FITTING CRACKED.SDR 97ZZZX3698Hub · crackedPROPELLER WAS DISASSEMBLED TO CHECK FOR GREASE LEAK. HUB EDDY CURRENT INSPECTED PER INSTRUCTIONS SB 164, AND DEFECT NOTED IN ONE BLADE SOCKET. PHOTOS TAKEN OF HUB AND EDDY CURRENT TEST OF HUB. HUB RED TAG (REJECT) ALL OTHER PARTS GREEN (SERVICEABLE). HARTZSDR AU970656Gear · failed(AUS) MAGNETO DISTRIBUTOR GEAR TEETH MISSINGSDR AU970681Distributor · stripped(AUS) MAGNETO PLASTIC DISTRIBUTOR GEAR TEETH STRIPPEDSDR 97ZZZX2077Frame · crackedFORWARD SPAR ATTACH BRACKET AT STA 94.0, RT SIDE. DURING A ROUTINE INSPECTION, A CRACK WAS FOUND IN THE LOWER PORTION OF THE UPPER RADIUS FOR THE FORWARD SPAR SLOT CUT-OUT (APPROXIMATELY .25 INCH LONG). CAUSE: APPEARED TO BE STRESS RELEASE CRACK. ACT: 7,5SDR 97ZZZX2073Frame · crackedFORWARD SPAR ATTACH BRACKET AT STA 94.0 LEFT AND RIGHT SIDES. DURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE LOWER PORTION OF THE UPPER RADIUS FOR THE FORWARD SPAR SLOT CUT-OUT. LEFT FRAME WAS CRACKED .3750 INCH LONG, RT FRAME FOUND CRACKED .0625 INCH LSDR 97ZZZX2072Frame · crackedFORWARD SPAR ATTACH BRACKET AT STA 94.0 LEFT AND RIGHT SIDES. DURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE LOWER PORTION OF THE UPPER RADIUS FOR THE FORWARD SPAR SLOT CUT-OUT. LEFT FRAME WAS CRACKED .3750 INCH LONG, RT FRAME FOUND CRACKED .0625 INCH LSDR AU970622Accumulator · faulty(AUS) PROPELLER UNFEATHERING ACCUMULATOR LEAKING INTERNALLY CAUSING LOSS OF AIR CHARGE - SUSPECT WORN PISTON `O' RING SEALSSDR 97ZZZX2080Frame · crackedFORWARD SPAR ATTACH BRACKET AT STA 94.0, LEFT SIDE. DURING A ROUTINE INSPECTION, A CRACK WAS FOUND IN THE LOWER PORTION OF THE UPPER RADIUS FOR THE FORWARD SPAR SLOT CUT-OUT (APPROXIMATELY .1250 INCH LONG). CAUSE: APPEARED TO BE STRESS RELEASE CRACK. ACTT:SDR AU970253Seal · leaking(AUS) PROPELLER BLADE SEALS LEAKING GREASE - INVESTIGATION FOUND BLADE SEALS TO BE INCORRECT PART - SEALS HAD BEEN SUPERSEDED BY SEALS PNO Q4339 IN SL 148 DATED 18/3/83 - PERSONNEL/MAINTENANCE ERRORSDR AU970222Commutator · open circuit(AUS) LANDING GEAR MOTOR COMMUTATOR SEGMENT OPEN CIRCUIT DUE TO LOOSE CRIMP ON THE WINDINGSDR 97ZZZX1211A Frame · crackedWHEN INSPECTING LANDING GEAR A-FRAMES PER AD 91-14-14 AND BEECH SB 2361, THE RIGHT AND LEFT A-FRAMES WERE REMOVED FROM THE AIRCRAFT FOR FURTHER INSPECTION. A MAGNAFLUX INSPECTION OF THESE PARTS WAS PERFORMED AND THE A-FRAMES WERE FOUND CRACKED. THE MAGNAFLUXSDR 97ZZZX1210A Frame · crackedWHEN INSPECTING LANDING GEAR A-FRAMES PER AD 91-14-14 AND BEECH SB 2361, THE RIGHT AND LEFT A-FRAMES WERE REMOVED FROM THE AIRCRAFT FOR FURTHER INSPECTION. A MAGNAFLUX INSPECTION OF THESE PARTS WAS PERFORMED AND THE A-FRAMES WERE FOUND CRACKED. THE MAGNAFLUXSDR AU970175Pipe · corroded(AUS) HYDRAULIC PIPE CORRODED - LOSS OF HYDRAULIC FLUID FROM PIN HOLE LEAKSDR 97ZZZX848A Frame · crackedWHEN INSTALLING LANDING GEAR 'A' FRAMES PER AD 91-14-14 AND SB 2361 REV 3, THE RIGHT AND LEFT 'A' FRAMES WERE REMOVED FROM THE AIRCRAFT FOR FURTHER INSPECTION. A MAGNAFLUX INSPECTION OF THESE PARTS WAS PERFORMED AND THE 'A' FRAMES WERE FOUND CRACKED. THE MAGSDR 97ZZZX847A Frame · crackedWHEN INSTALLING LANDING GEAR 'A' FRAMES PER AD 91-14-14 AND SB 2361 REV 3, THE RIGHT AND LEFT 'A' FRAMES WERE REMOVED FROM THE AIRCRAFT FOR FURTHER INSPECTION. A MAGNAFLUX INSPECTION OF THESE PARTS WAS PERFORMED AND THE 'A' FRAMES WERE FOUND CRACKED. THE MAGSDR AU970299Latch · sticking(AUS) LH DOOR LATCH STICKING - SUSPECT CAUSED BY LACK OF LUBRICATIONSDR CA970107001Actuator · failed(CAN) IN LEVEL FLIGHT A LOUD BANG WAS HEARD FROM THE LEFT SIDE OF THE AIRCRAFT. THE GEAR WAS LOWERED AND A SUCCESSFUL LANDING COMPLETED. THE LEFT HAND ACTUATOR CYLINDER WAS FOUND TO HAVE FAILED AT THE ROD END.SDR CA970107002Brake Line · cut(CAN) BRAKE LINE FOUND CUT IN THE WING BY A CONTROL CABLE. REPAIRED AND RETURNED TO SERVICE.SDR 96ZZZX5440Downlock · malfunctionNOSE GEAR COLLAPSED DURING A TOUCH-AND-GO WHEN POWER WAS APPLIED FOR A TAKEOFF. INVEST REVEALED: LT FWD DRAG BRACE ATTACH BOLT LOOSE (COTTER PIN WAS INSTALLED), INCORRECT WASHERS WERE INSTALLED (BASED ON PARTS MANUAL). DOWNLOCK HOOK PIVOT BOLT WAS PARTIALLY
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