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 = '440' 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 = '440' 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 CA071026004Actuator · malfunctioned(CAN) DURING APPROACH WHEN LANDING GEARS SELECTED DOWN, THE LANDING GEARS UNLOCK LIGHT CAME ON, HOWEVER, NO NOSE WHEEL DOWN LIGHT CAME ON. THE CREW CONFIRMED VISUALLY GEAR NOT DOWN. AFTER A FEW CYCLES GEAR UP AND GEAR DOWN AND EMERGENCY UPLATCH RELEASE TO NO ASDR CA070816001Connector · unsecure(CAN) ENGINE NR 1 RPM UNSTABLE, REDUCED RPM TO 13,600. AIRCRAFT DIVERTED TO NEAREST AIRPORT. ENGINE WAS SHUTDOWN IN FINAL APPROACH, DUE TO RPM REDUCTION TO 13500 RPM. MAINTENANCE WAS SENT ON SITE AND FOUND THAT OIL PROPELLER FILLER PLUG WAS NOT SECURED PROPESDR CA070824007Door · inoperative(CAN) AIRCRAFT WAS DISPATCHED FOR FIRE ACTION. AFTER DEPARTURE, THE RT OIL TEMPERATURE GAUGE WAS OBSERVED TO BE AT THE BOTTOM OF THE RED ARC, APPROXIMATELY 100 DEGREES C. THE FLIGHT CREW IMMEDIATELY SHUTDOWN THE RT ENGINE AS A PRECAUTION AND RETURNED TO BASE. SDR CA070727009Lever · distorted(CAN) UPON SELECTION OF (GEAR DOWN), THE LOCKING ARM OF THE LANDING GEAR SELECTOR HANDLE STUCK IN THE EXTENDED POSITION, PREVENTING ASSOCIATED FUNCTION OF DEPRESSING THE GEAR WARNING LIGHT SWITCH. THE RESULT WAS NO GEAR DOWN INDICATING LIGHTS ON THE ANNUNCIATSDR RDS12120061Axle · crackedWHEN REMOVING NOSE AXLE TO C/W AD83-01-02 FOR THE 12,000 HOUR MAGNETIC PARTICLE TESTING. A CRACK AROUND THE AXLE FLANGE THAT THE BEARING SPACER RIDES AGAINST WAS NOTICED. REMOVED AND REPLACED WITH NEW AXLE, RETURNED AIRCRAFT TO SERVICE.SDR CA060617001Steering Sys · malfunctionedAFTER T/O, DURING L/G RETRACTION, NOSE WHEELS ENTERED W/W IN A RT TURN ATTITUDE, EVIDENT FROM WEAR MARKS ON TIRES AND RUBBER ON INTERIOR WALLS OF W/W. WHEN A/C LANDED, NOSE WHEELS WERE STILL TURNED TO THE RIGHT, UNKNOWN TO AIRCREW. CAPT TRIED TO STRAIGHTEN NSDR CA060516008Wire Harness · chafedDURING INSTALLATION OF ELT REMOTE SWITCH WIRING, ROUTING OF THE WIRE BEHIND THE FORWARD RT EQUIPMENT SHELF, SEVERAL WIRES WERE FOUND CHAFING INTO THE WIRE BUNDLE THAT RUNS VERTICALLY BEHIND THE SHELF. THE WIRES WERE CHAFING ON THE BACK EDGE OF THE FLOOR. THSDR CA060302012Wire Harness · misinstalledAIRCRAFT ON A TEST FLIGHT AND DURING AN RPM DECAY TEST, THE LT ENGINE POWER LEVER WAS REDUCED BELOW 1400 HP. THE RPM THEN STARTED TO DECAY BELOW PRESCRIBED LIMITS. DUE TO THIS, THE CREW ELECTED TO SHUT DOWN THE ENGINE. THE PROBLEM ONLY OCCURRED BELOW 1400 HSDR CA050823007Hook · failed(CAN) WITH AN AIRCRAFT MECHANIC AND 2 FLIGHT ATTENDANTS ON BOARD, THE REAR SERVICE DOOR OPEN WARNING LIGHT CAME ON AT 14,000 FEET. AIRCRAFT DEPRESSURIZE AND RETURN TO DEPARTURE. INVESTIGATION REVEALED THAT LOWER REAR HOOK WAS NOT GOING IN PLACE PROPERLY, DOOSDR CA050823005Bearing · failed(CAN) WITH AN AIRCRAFT MECHANIC AND 2 FLIGHT ATTENDANTS ON BOARD, NR 1 ENGINE FLAMED OUT IN DESCENT, AIRCRAFT LANDED SAFELY AT AIRPORT. AFTER EVALUATION, THE POWER SECTION ACCESSORIES GEARBOX WAS FOUND AT FAULT, TOWER SHAFT BEARING (RR. IPC 72-60-00 FIG. 3 ISDR CA050727004Selector · failedON APPROACH TO AIRPORT, THE THREE (3) MLG DOWN GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION, THE HORN DID NOT SOUND AND THE RED GEAR UNSAFE LIGHT EXTINGUISHED. MAINTENANCE WAS UNABLE TO DUPLICATE THE SNAG ON GROUND, THE (LANDING) GEAR LEVER SWITCH WAS SDR JRAA587060705Longeron · corrodedINTERGRANULAR CORROSION WAS FOUND ON THE LONGERON CHANNEL AT FUSELAGE BUTTOCK LINE 0, WING STATION 403.0. THIS CORROSION NOTED ON THE LT SIDE, 10 INCHES FORWARD OF THE REAR LOWER WING SPAR. ACCESS THROUGH THE LT WING IB DRY BAY PANEL. (K)SDR CA050527007Switch · inoperativeON FINAL APPROACH TO MONTREAL, THE RT MAIN LANDING GEAR DOWN ANNUNCIATION LIGHT FAIL TO INDICATE. AFTER INVESTIGATION, THE DOWN MICROSWITCH WAS FOUND INOPERATIVE, UNIT REPLACED AND ADJUSTED IAW MAINTENANCE MANUAL. GEAR SWING C/O SERVICEABLE, AIRCRAFT RETURN SDR VGC2005F00001Unknown · unknownNR 2 FUEL PUMP FAILED. RT DC GENERATOR OFF LINE, FOLLOWED BY LT DC GENERATOR OFF LINE. (ELECTRIC ODOR NOTED). TRU TO EMERGENCY SELECTED FOR DC BUSS POWER. PRECAUTIONARY LANDING MADE. (K)SDR CA041104001Drain · obstructed(CAN) ON DEPARTURE, CARGO SMOKE DETECTOR LIGHT CAME ON WITH NO ODOR OR SMOKE IN COCKPIT. EMERGENCY DECLARE AND RETURNED AFTER 10 MINUTES AIR TIME. LIGHT EXTINGUISH DURING TAXI. CARGO CONTAINER AND A/C INSPECTED, NOTHING UNUSUAL DETECTED. PROBLEM TREATED LIKE ASDR CA051006001Fitting · cracked(CAN) AIRCRAFT RETURN TO BLOCK AFTER LOSS OF HYDRAULIC FLUID. AFTER INVESTIGATION MAINTENANCE FOUND FROM LT ENGINE DRIVE HYDRAULIC PUMP PRESSURE LINE AND AC HYDRAULIC PUMP, T-FITTING AT FS 319 CRACKED. THE FITTING WAS REPLACED, SYSTEM REPLENISHED AND LEAK CHSDR CA041004004Pump · out of adjust(CAN) AIRCRAFT DISPATCH LIKE USUAL FROM HANGAR WITH 28 PASSENGER ONBOARD AND CAME BACK DUE TO FUEL UNBALANCE AND ONE PASSENGER HAD REPORT SEEING FUEL COMING OUT OF RT HAND TANK OVERWING FUEL CAP AND CREW REALIZED IT HAD TAKEN OFF WITH FUEL CROSS-FEED OPEN. MASDR CA041005002Door · out of rig(CAN) AIRCRAFT DISPATCH WITH 29 PASSENGER ABOARD AT 13:32 GMT AND CAME BACK AT 14:14 WITH C2 DOOR OPEN. MAINTENANCE DISCOVERED THAT THE C2 DOOR COULD BE CLOSE IMPROPERLY IN SOME OCCASION AND NO DAMAGE WAS FOUND. MAINTENANCE CLOSE THE DOOR AND CONFIRM THE LOCK SDR CA040823002Circuit Breaker · sticking(CAN) DURING CRUISE THE OIL TEMPERATURE ON THE LT ENGINE CLIMBED TO LIMITS. THE OIL COOLER DOOR WAS NOT OPERATING. THE ENGINE WAS SHUT DOWN AND THE PROPELLER WAS FEATHERED AS A PRECAUTION. THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATION BY MAINTENANCE THE CISDR CA040819013Line · ruptured(CAN) AC WAS ORBITING OVER FIRE. A LOUD SURGING SOUND WAS HEARD. A CHECK OF HYDRAULIC RESERVOIR INDICATED THAT NO HYDRAULIC FLUID WAS REMAINING. FLAPS WERE SELECTED FROM 15 TO 0 DEGREES. HYD BYPASS WAS SELECTED UP. RETARDANT LOAD WAS JETTISONED. AC RETURNED SDR 2004F00349Check Valve · corrodedBAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PART REPLACED. (M)SDR 2004F00347Tube · corrodedBAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSOIN ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) JRAASDR 2004F00346Transmitter · corrodedDUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. TRANSMITTER REPLACED. (M)SDR 2004F00344Door · corrodedBAK - DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. DOOR REPLACED. (M)SDR 2004F00343Bellmouth · corrodedDURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION AND SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M)SDR CA040804001Gasket · missing(CAN) DURING DESCENT THE LT ENGINE ZONE 2 FIRE ALARM ACTIVATED.SDR CA040806001Actuator · failed(CAN) DURING CRUISE THE FLIGHT CREW NOTICED THAT THE OIL TEMPERATURE ON THE LT ENGINE WAS CLIMBING. THE CREW TRIED TO MANUALLY CONTROL THE OIL TEMP BUT WAS UNSUCCESSFUL. THE ENGINE WAS SHUT DOWN AND THE PROP WAS FEATHERED AS A PRECAUTION. THE AIRCRAFT RETURSDR CA040719006Turnbuckle · shearedDURING INSPECTION MAINTENANCE CREW NOTED THAT THE RIGHT HAND ENGINE OUTBOARD EXHAUST SUPPORT TURNBUCKLE HAD SHEARED CAUSING THE TAILPIPE TO REST ON THE BOTTOM OF THE EXHAUST SHROUD INSTEAD OF BEING SUPPORTED IN THE CENTER. THE TURNBUCKLE WAS REPLACED WITH A SSDR CA040702003Bar · broken(CAN) DURING CRUISE THE FLIGHT CREW NOTICED SEVERE SURGING ON THE NR 1 ENGINE. THE FUEL FLOW WAS ALSO DROPPING AND SURGING. THE ENGINE WAS SHUT DOWN AND THE PROPELLER WAS FEATHERED. THE AIRCRAFT RETURNED TO DEPARTURE. DURING INVESTIGATION MAINTENANCE CREW FOUNSDR CA040628005Door · failed(CAN) DURING CLIMB OUT THE FLT CREW NOTICED THE OIL TEMPERATURE RISING TO THE RED LINE. THE OIL COOLER SWITCH WAS SELECTED FROM (AUTO) TO (MANUAL) OPEN WITH NO RESOMNSE. THE OIL TEMPERATURE CONTINUED TO CLIMB. THE ENGINE WAS SHUT DOWN ANDTHE PROP WAS FEATHEREDSDR MV1R04231Switch · intermittentLT MLG DOWN AND LOCKED LIGHT INTERMITTENT. PERFORMED GEAR SWING AND PROBLEM VERIFIED. LT MAIN GEAR SWITCH INTERNAL WIRING LOOSE AT MOUNTING LUGS. INSTALLED NEW LOCK WASHERS AND RE TORQUED. RETRACTION CHECKS NORMAL IAW MM.SDR JRAA0520042Floorbeam · corrodedDURING A SCID INSPECTION 53-20, CORROSION WAS FOUND ON FLOORBEAM AT STA 681.0 RT SIDE AT BELTFRAME. AN AREA OF APPROX 3 INCHES X 5 INCHES ON THIS FLOORBEAM WAS FOUND CORRODED AT BELTFRAME ATTACH POINT AROUND RIVETS. THE CORROSION HAD PROGRESSED THROUGH 50 PESDR JRAA0520041Floorbeam · corrodedDURING A SCID INSPECTION 53-20, A MISSING RIVET HEAD WAS FOUND AT STA 712.0. RT SIDE AT THE FLOORBEAM TO BELTFRAME ATTACH POINT. CORROSION WAS FOUND UNDER RIVET HEAD. NO OTHER RIVETS WERE FOUND TO BE CORRODED AT THIS TIME. RIVET REPLACEMENT IN PROGRESS AT SDR 15HA0358005Smoke · detectedCREW NOTICED SMOKE IN THE COCKPIT AND CARGO COMPARTMENT JUST AFTER RT ENG WAS STARTED IN PREP FOR THE REGULARLY SCHEDULED FLIGHT. ENG WAS SHUTDOWN AND INSPECTED. NOTHING OUT OF ORDINARY WAS DISCOVERED. MECHANIC HAD CREW DISCONNECT EDC AND ENG WAS RESTARTED.SDR 15HA0458004Compressor · damagedDURING THE DESCENT, AT APPROX 12,000 FT, THE CREW HEARD A LOUD BANG A MOMENT LATER, THE LT FIRE WARNING LIGHT ILLUMINATED AND THE CREW (E) HANDLED THE ENGINE. THE AC MADE AN UNEVENTFUL LANDING. INSPECTION OF THE LT ENGINE HAS REVEALED THE PRESENCE OF A PIECSDR 2004FA0000219O-Ring · cutAT CRUISE FLIGHT NR 1 PROP EXPERIENCED RPM FLUCTUATIONS. AS A PRECAUTIONARY MEASURE, PROP WAS FEATHERED. PILOT LANDED UNEVENTFULLY. FOUND REGULATOR TO PROP, OIL TRANSFER TUBE, O-RING CUT. INSTALLED NEW O-RING. GROUND RUN FUNCTIONAL AND LEAK CHECKS GOOD.SDR CA040113011Drive Assy · stripped(CAN) AFTER PROPS WENT OUT OF SYNC, ENG DRIVEN COMP LOW OIL LIGHT ILLUMINATED. EDC DISCONNECT WAS SELECTED, FLUCTUATING GB OIL PRESSURE WAS OBSERVED. PRESS FLICKERED FROM 200 PSI TO 120 PSI ABOUT EVERY 5 SECONDS. SHUTDOWN CARRIED OUT, AC RETURNED TO BASE OEI.SDR CA030718003Actuator · misoverhauled(CAN) RECIEVED ACTUATOR THROUGH OUR SUPPLIER. UPON INSTALLATION, FOUND IT BINDING. REMOVED IT AND FOUND THAT TWO SEPERATE CABLES THIS UNIT HAS WERE GOING THROUGH THE SAME PULLEY WHICH LEFT THE OTHER PULLEY NOT IN USE AND BINDING THE UNIT AS WELL AS DAMAGING TSDR I5HA0358003Engine · malfunctionedON THE TAKEOFF ROLL DEPARTING CVG, EN ROUTE TO CLE THE LEFT ENGINE WOULD ONLY PRODUCE 888 DEGREES, NOMINAL IS 971 DEGREES. THE PILOT ABORTED THE TAKEOFF. THE TEMPERATURE DATRUM (TD) SYSTEM WAS NULLED AND FULL POWER WAS THEN AVAILABLE. THE TD SYSTEM WAS DEFESDR 15HA0358002Line · brokenWHILE EN ROUTE BETWEEN CVG AND PIT, THE CAPTAIN NOTICED A DROP FROM 65 PSI TO 50 PSI IN THE LEFT POEWR SECTION OIL PRESSURE, FLUCTUATING REDUCTION GEARBOX OIL PRESSURE AND A THREE GALLON DROP IN OIL QTY. THE CAPTAIN PULLED THE LEFT 'E' HANDLE AND SECURED THE SDR NQ52003F00000Support Bracket · crackedAPPROX .2500 CRACK DETECTED IN WEB/FLANGE RADIUS OF AFT TEE OF SUPPORT BRACKET ASSEMBLY FOR ATTACHMENT OF MAIN ENTRANCE DOOR ACTUATOR. THIS TEE BRACKET IS ATTACHED TO THE FORWARD FACE OF FUSELAGE BELTFRAME AT FS 176.50, STRINGER L-26 AND IS APPROX 4 INCHES LOSDR BKJ2003F00000Brake Assy · leakingDURING LANDING CHECK, UPON ARRIVAL TO AIRPORT. PILOTS NOTICED LOW HYDRAULIC RESEVOIR LEVEL. TOWER WAS NOTIFIED AND A NORMAL LANDING WAS MADE. AS A PRECAUTION, THE AIRCRAFT WAS TOWED TO PARKING. INSPECTION REVEALED A LEAKING BRAKE ASSEMBLY.SDR CA021007011Windshield · failed(CAN) ON CLIMB OUT OF YUL, LT WINDSHIELD SHATTERED. AIRCRAFT DEPRESSURIZED AND CAME BACK TO MONTREAL. UNABLE TO ESTABLISH THE REASON FOR WINDSHIELD SHATTERED. WINDSHIELD REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR CA021104006Wire · chafed(CAN) PILOT REPORTED THAT BETA LIGHT WAS 'ON' DURING TAKEOFF ATTEMPT, PILOT ABORT TAKEOFF. MAINTENANCE INVESTIGATION FOUND THAT, BETA LIGHT AND THE FEATHER SOLENOID ENERGIZE. FURTHER INVESTIGATION FOUND THAT WIRING WAS CHAFING ON THE RT RADIO RACK AFT OF THE SDR NQ52002F00000Intercostal · crackedSLIGHT SURFACE CRACKING DETECTED IN THE RADIUS OF INTERCOSTAL (TEE) PN3403310252-21 (FORWARD RIGHT ESCAPE HATCH FRAME). INTERCOSTAL IS PART OF FUSELAGE BELTFRAME ASSEMBLY AT FS 334.749 AND PROVIDES THE FORWARD, VERTICAL SEATING SURFACE FOR THE ESCAPE HATCH.SDR CA020624006Socket · burned(CAN) DURING CLIMBOUT, THE FLIGHT ATTENDANT HAD INFORMED THE CAPTAIN THAT SMOKE WAS EMITTING FROM AN OVERHEAD ISLE LIGHT (NUMBERS 3 AND 4) IN ROWS 4 AND 5. THE OVERHEAD LIGHT SWITCH HAD ALREADY BEEN PLACED IN THE OFF POSITON AT THIS POINT. WHEN THE FLIGHT ATSDR CA010809006Pump · failed(CAN) EMERGENCY LANDING WITH SMOKE IN COCKPIT. FOUND ELECTRIC HYDRAULIC PUMP BYPASSING THRU CASE DRAIN AND PUMP DEVELOPING 2,700 PSI ONLY. AFTER INSPECTION AIRCRAFT WAS FERRIED TO MAINTENANCE BASE WITH GEAR DOWN AND PUMP OFF. AC PUMP REPLACED. MULTIPLE GEAR RESDR CA010726038Insulator · damaged(CAN) FOUND INSULATOR MISSING ON SERVICE CHECK NEW PART INSTALLED. NO OTHER PROBLEM FOUND AND A/C RETURNED TO SERVICE. LT ENGINE REAR SCAVENGE PUMP INSULATOR WAS MISSING IT HAD BEEN REPORTED BY GROUND PEOPLE THAT A PART FALL FROM AIRCRAFT ON APPRAOCH TO LAND ISDR 20010312CW015Engine · failedINTERNAL ENGINE FAILURE IN CRUISE FLIGHT, UNKNOWN SPECIFIC CAUSE PENDING TEARDOWN.SDR CA010103011Receptacle · shorted(CAN) FOLLOWING TAKEOFF NR1 AND NR2 V.H.F. UNABLE TO TRANSMIT OR RECEIVE. AIRCRAFT LANDED AT AIRPORT. CAPTAINS MICROPHONE JACK REPLACED. SYSTEMS TESTED SERVICEABLE. AIRCRAFT RELEASED FOR FLIGHT WITH NO FURTHER REPORT.
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