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 = '441' 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 = '441' 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 2001FA0000483Fcu · faultyENGINE WOULD NOT OPERATE NORMALLY IN COMPUTER MODE. ENGINE SPEED WAS NOT BEING REGULATED PROPERLY BY FUEL CONTROL TORQUE MOTOR ENGINE OPERATED NORMALLY IN MANUAL MODE. OVERHAULED FUEL CONTROL WAS INSTALLED AND ENGINE OPERATED NORMALLY IN BOTH COMPUTER AND MANSDR 2001FA0000482Fcu · misrepairedUNIT WAS INSTALLED AFTER REPAIR BY MFG. UPON APPLYING POWER TO THE FUEL CONTROL AIRCRAFT HAD THE LEFT MONOPOLE FAIL LIGHT ILLUMINATED. FOUND THE WIRING AT THE FUEL CONTROL ELECTRICAL CONNECTOR MISSOLDERED, RESOLDERED WIRING AT THE CONNECTOR UNIT OPERATIONALLSDR 2001FA0000481Fcu · faultyENGINE WOULD NOT REDUCE FUEL FLOW IN EITHER COMPUTER MODE OR MANUAL MODE TO ALLOW A NORMAL LANDING. THE AIRCRAFT HAD TO BE LANDED SINGLE ENGINE INSTALLING A REPAIRED FUEL CONTROL UNIT CURED THE FAULT.SDR 2001FA0000187Angle · crackedDURING A SCHEDULED INSPECTION, THE LEFT CANTED RIB CAP P/N 5722206-1 WAS FOUND CRACKED APPROXIMATELY 1 INCH AFT OF THE FORWARD WING SPAR. WHILE REPAIRING THIS CRACK THE UPPER WING TO FUSELAGE CLOSEOUT ANGLE P/N 5720001-3 WAS FOUND CRACKED. THESE CLOSEOUT ANGSDR AUS20010858Switch · out of adj(AUS) NOSE LANDING GEAR ACTUATOR POSITION SWITCH INCORRECTLY ADJUSTED.PERSONNEL/MAINTENANCE ERROR.SDR 2001FA0000186Rib · crackedDURING A SCHEDULED INSPECTION THE LEFT AND RIGHT CANTED RIB CAPS P/N 5722206-1 AND 5722206-2 WERE FOUND CRACKED APPROXIMATELY 1 INCH BEHIND THE FORWARD SPAR. WHILE ACCOMPLISHING THE REPAIR TO THIS AREA, ANOTHER CRACK WAS FOUND IN THE LEFT WING/FUSELAGE CLOSEOSDR AUS20010843Hinge · mismanufactured(AUS) LOWER RUDDER HINGE BRACKET INSTALLED UPSIDE DOWN. FOUND DURINGINSPECTION IAW CESSNA CQB00-2 R1. MANUFACTURING ERROR.SDR 2001FA0000150Rib · crackedDURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE RH CENTER WING CANTED RIB CAP P/N: 5722206-2 (RH CWS26.85) HAD A VISUALLY SUSPECT AREA ALONG THE BEND RADIUS BETWEEN THE CENTER WING MAIN SPAR (FS177.45) AND FS188.95". FURTHER INSPECTION USING FLUORESCENT PSDR AUS20010798Pump · cracked(AUS) LT ENGINE OIL PUMP HOUSING CRACKED.SDR CA010813013Harness · chafed(CAN) DURING INVESTIGATION OF INTERMITTENT BOOST PUMP FOUND CHAFED SPOT ON WIRE HARNESS INSIDE FUEL TANK. MAGNIFIED VIEW SHOWED EVIDENCE OF ELECTRICAL CONTACT BETWEEN WIRE AND STRUCTURE OF FUEL TANK.SDR AUS20010746Wheel · worn(AUS) MAIN LANDING GEAR WHEEL INNER HALF WORN IN BEARING BORE. BEARING SPINNING IN HUB.SDR AUS20010699Wire · broken(AUS) FLAP SELECTOR LOOM WIRE BROKEN FROM CRIMP TO FLAP MICROSWITCH.SDR 2001FA0000046Cam · mismanufacturedRECEIVED A NEWLY OVERHAULED P.P.C. FROM MANUFACTURER, WAS UNABLE TO RIG. FOUND P.P.C. CAM HAD THE RIGHT PN BUT THE WRONG CAM PROFILE MANUFACTURE IN IT. REF: SB TPE331-72-0904.SDR 2001FA0000001Cam · mismanufacturedAFTER INSTALLING NEWLY OVERHAULED ENGINE ON AIRCRAFT, FOUND THAT THE -30 P.P.C. COULD NOT BE RIGGED. REMOVED P.O.C. AND FOUND THAT THE CAM INSIDE, ALTHOUGH MARKED CORRECTLY (P/N 897602-1), THE CAM WAS MANUFACTURED WRONG. IT HAS THE WRONG CAM PROFILE. REF: SSDR 2001FA0000002Cam · mismanufacturedAFTER INSTALLING NEWLY OVERHAULED ENGINE ON AIRCRAFT, FOUND THAT THE -30 P.P.C. COULD NOT BE RIGGED. REMOVED THE P.P.C. AND FOUND THAT THE CAM INSIDE, ALTHOUGH MARKED WITH THE CORRECT P/N (8976021) WAS MANUFACTURED WRONG. IT HAS THE WRONG CAM PROFILE. REF: SDR 20010515AP002Rib · crackedDURING A SCHEDULED INSPECTION, THE LEFT WING CENTER SECTION CANTED RIB CAP (CWS 26.85 INCHES) WAS FOUND CRACKED. THE CANTED RIB UPPER CAP (P/N: 5722206-1) WAS CRACKED AFT OF THE AFT MAIN SPAR AT FS 177.45, IN THE BEND RADIUS, AND RAN AFT APPROXIMATELY 1.375 INSDR 20010515AP001Rib · crackedDURING A SCHEDULED INSPECTION, THE LEFT WING CENTER SECTION CANTED RIB CAP (CWS 26.85 INCHES) WAS FOUND CRACKED. THE CANTED RIB UPPER CAP (P/N: 5722206-1) WAS CRACKED AFT OF THE AFT MAIN SPAR AT FS 177.45, IN THE BEND RADIUS, AND RAN AFT APPROXIMATELY 1.375 INSDR AUS20010545Duct · deteriorated(AUS) AIRCYCLE MACHINE DUCT DETERIORATED.SDR AU010363Tire · leaking(AUS) LT MAIN WHEEL TYRE CONTAINED A SLOW LEAK FROM ONE OF THE SIDEWALL VENT HOLES.SDR CA010426031Exciter · failed(CAN) ENGINE WOULD NOT START. FOUND IGNITION EXCITER UNSERVICEABLE. REPLACED UNIT.SDR 20010508CW017Trunnion · crackedNOSE GEAR TRUNNION INSPECTION/ REPLACEMENT. COMPLIED WITH CQB 00-3 AND FOUND BOTH PIVOT LUGS TO HAVE CRACKS AT THE FILLETS, REPLACED TRUNNION ASSEMBLY.SDR 20010410AP005Skin · corrodedFOUND FUEL LEAK COMING FROM BEHIND THE RT WING DE-ICE BOOT. AFTER PEELING BACK BOOT TO LOCATE LEAK, NOTED SEVERAL AREAS OF HEAVY CORROSION ON LEADING EDGE. FERRIED AIRCRAFT TO FACILITY FOR LEADING EDGE REPLACEMENT. SUSPECT DE-ICE BOOT WAS INSTALLED USING IMSDR 20010410AP003Boot · leakingNOTED FUEL LEAK FROM BEHIND RT WING DE-ICE BOOT. AFTER PEELING BOOT BACK TO RESEARCH LEAK, NOTED NUMEROUS AREAS OF HEAVY CORROSION. AIRCRAFT WAS FERRIED TO FACILITY FOR REPLACEMENT OF LEADING EDGE ASSEMBLY.SDR AU010040Pin · cracked(AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED.SDR AU010020Pin · cracked(AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED. FOUND DURING INSPECTION IAW CESSNA SB CQB00-3.SDR AU010011Wire · chafed(AUS) LT FUEL TANK BOOST PUMP WIRING CHAFED THROUGH TO BARE WIRE.SDR AU001240Mount · broken(AUS) RT ENGINE INBOARD MOUNT BROKEN. ENGINE HAD DROPPED APPROXIMATELY38.1MM (1.5IN).SDR AU001258Wheel · broken(AUS) ELEVATOR TRIM WHEEL POINTER GROOVE BROKEN.SDR CA010110019Light · burned out(CAN) CONNECTOR ON BACK OF COPILOTS VSI POST LIGHT OVERHEATED WHICH CAUSED SMOKE IN COCKPIT. CB WAS PULLED AND SMOKE DISIPATED.SDR 20001109SH011Rib · crackedDURING A PHASE INSPECTION, FOUND A 1.1 INCH CRACK IN LEFT WING CANTED RIB. CRACK STARTING AFT OF THE FORWARD SPAR AND EXTENDED AFT ALONG THE RIB RADIUS. SUBMITTER STATED CESSNA NO LONGER WILL ALLOW STOP DRILLING OF THIS CRACK, SO THE RIB WAS REPLACED. (X)SDR 20001109SH024Rib · crackedDURING A PHASE INSPECTION, FOUND THE CRACK IN THE RIGHT CANTED RIB HAD PROGRESSED BEYOND THE PREVIOUSLY INSTALLED STOP DRILLS. AIRCRAFT WAS RETURNED TO THE OPERATOR WITH A ''FERRY PERMIT'' FOR REPAIR. (X)SDR 20001109SH012Rib · crackedDURING A PHASE INSPECTION, FOUND A .9 INCH CRACK IN RIGHT WING CANTED RIB TOP CAP. CRACK STARTS AFT OF FORWARD SPAR AND EXTENDS AFT. FOR MANY YEARS, CESSNA HAS ALLOWED THESE CRACKS TO BE STOP DRILLED, BUT NO LONGER WILL ACCEPT THIS REPAIR. NO PARTS ARE AVAISDR AU000994Clamp · loose(AUS) AIR CYCLE MACHINE TO WATER SEPARATOR DUCT CLAMP LOOSE. INVESTIGATION FOUND THE CLAMP WAS THE INCORRECT SIZE. CORRECT CLAMP PN AN737TW-91. UNAPPROVED PART. (X)SDR 20001011SH003Governor · malfunctionedA MECHANIC INSTALLED A NEW PROP GOVERNOR, P/N 897160-9, ON THE RIGHT ENGINE OF A CESSNA 441. WHILE PERFORMING ROUTINE GROUND RUNS AND LEAK CHECKS IT WAS NOTED THAT OIL WAS LEAKING FROM THE TORQUE MOTOR, SPECIFICALLY THE EXIT POINT FOR THE WIRES. GOVERNOR TIMESDR 20001011SH002Governor · malfunctionedPILOT REPORTED THAT AFTER ENGINE SHUT-DOWN OF A NORMAL FLIGHT, OIL WAS NOTICED LEAKING PROFUSELY FROM THE RIGHT COWLING. FURTHER INVESTIGATION REVEALED THE OIL LEAK WAS ORIGINATING FROM THE PROP GOVERNOR BASE FLANGE SEAM. IT WAS VERIFIED BY A MECHANIC THATSDR AU000945Valve · stuck(AUS) AIR CYCLE MACHINE BYPASS VALVE STICKING IN THE ''OPEN'' POSITION. (X)SDR AU000819Wire · broken(AUS) LANDING GEAR HYDRAULIC SELECTOR VALVE WIRE BROKEN AT TERMINAL CONNECTOR. (X)SDR AU000818Switch · faulty(AUS) RIGHT MAIN LANDING GEAR UPLOCK MICROSWITCH FAILED. LEFT MAIN LANDING GEAR UPLOCK MICROSWITCH INTERMITTENT IN OPERATION. (X)SDR PNSA0901Transducer · malfunctionedTORQUE INDICATION WENT TO ZERO DURING DESCENT. AFTER UNEVENTFUL LANDING, REPLACED TORQUE TRANSDUCER. OPERATIONAL CHECK OK. (X)SDR AU000642Hose · failed(AUS) HYDRAULIC HOSE LOCATED IN THE RIGHT WING LEADING EDGE FRACTURED ON THE BOND RADIUS. (X)SDR AU001069Panel · failed(AUS) METAL FLOOR PANELS INTERMITTENTLY OIL CANNING DURING PHASES OF PRESSURIZATION. (X)SDR AU000984Turbine · overheated(AUS) LEFT ENGINE UNCOMMANDED TORQUE REDUCTION COUPLED WITH HIGH EGT INDICATION. HOT SECTION OVERTEMP DAMAGE. (X)SDR 20000808SH011Switch · burnedSWITCH FAILED INTERNALLY CAUSING SMOKE IN THE COCKPIT. DUE TO THE FACT THE SWITCH WAS AT FAULT, IT DID NOT TRIP AND CONTINUED TO SMOKE UNTIL SHUT OFF BY THE PILOT. (X)SDR 20000919SH019Switch · intermittentFLOW SWITCH UNIT INOPERATIVE. BENCH CHECKED AND FOUND UNIT TO OPERATE INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR AU000525Actuator · faulty(AUS) NOSE LANDING GEAR ACTUATOR FAULTY. SUSPECT WORN DOWNLATCH PINS. (X)SDR AU000499Switch · intermittent(AUS) LEFT MAIN LANDING GEAR SQUAT SWITCH INTERMITTENT IN OPERATION.SDR AU000462Seal · leaking(AUS) LEFT ENGINE CARBON SEAL ALLOWING OIL TO LEAK INTO THE BLEED AIR SYSTEM AND CONTAMINATE THE COALESCER BAG IN THE AIR CYCLE MACHINE. SMOKE IN THE CABIN.SDR AU000447Bearing · failed(AUS) LEFT ENGINE STARTER/GENERATOR REAR BEARING FAILED. LEFT ELECTRICAL BUS CURRENT LIMITER ALSO FAILED.SDR 20000517SH013Canopy · crackedDURING A PHASE INSPECTION, FOUND A CRACK IN THE RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD WING SPAR AND RUNS AFT PARALLEL TO THE BEND LINE 1 INCH LONG. STOP DRILLED PER CESSNA INSTRUCTIONS. (X)SDR AU000390Brush Block · misinstalled(AUS) RIGHT ENGINE DE-ICE SYSTEM CENTER BRUSH BLOCK TERMINAL INCORRECTLY INSTALLED. PROPELLER AMMETER IN LINE TERMINALS MELTED.
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