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 = '58' 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 = '58' 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 EWK2002F00000Line · corrodedDEEP CORROSION ON FUEL PRESSURE LINE AT CONJUNCTION OF FUEL LINE AND DEFROSTER HEAT DUCT. INSULATE FUEL LINE FROM HEAT DUCT. DANGER/POTENTIAL FOR FIRE.SDR FPI2002F00004Channel · crackedUPPER U-CHANNEL ON ENGINE FIREWALL, BOTH LEFT AND RIGHT HAND ENGINE NACELLES. CRACK DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION.SDR FPI2002F00006Channel · crackedUPPER U-CHANNEL ON ENGINE FIREWALL. CRACKS DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION.SDR FPI2002F00005Channel · crackedUPPER U-CHANNEL ON ENGINE FIREWALL, CRACKS DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION.SDR BSY2002F00001Switch · failedAIRCRAFT HAD ELECTRICAL SMELL IN COCKPIT. REMOVED AND REPLACED TAXI LIGHT SWITCH OPS CHECKS GOOD.SDR FPI2002F00002Starter · failedTHE STARTER DRIVE FAILED TO ENGAGE OR EVEN ATTEMT TO TURN ENGINE AFTER BRINGING INTO HANGER AND WARMING UP IT STILL DID NOT ENGAGE. INSPECTED ENGINE OIL FILTER, NO CONTAMINATES FOUND. CHANGED STARTER DRIVE. OPS CHECK GOOD.SDR FPI2002F00000Channel · crackedTHESE AIRCRAFT HAVE AN UPPER AND LOWER FIREWALL CHANNEL AND THE UPPER ALMOST ALWAYS CRACKS BELOW THE ENGINE MOUNT BOLTS. THIS AIRCRAFT HAD BOTH THE LEFT AND RIGHT NACELLES UPPER FIREWALL CHANNELS CRACKED AND HAD TO BE REPLACED WITH NEW.SDR AUS20011338Line · corroded(AUS) FUEL LINE EXCESSIVELY COORODED DUE TO WATER CONTAMINATION.SDR AUS20011337Valve · corroded(AUS) FUEL SYSTEM CHECK VALVE EXCESSIVELY CORRODED AND CONTAMINATED DUE TO WATER IN FUEL CROSSFEED LINE.SDR BSY2001F00023Cotter Pin · sheared(CLT)(MIR) RIGHT ENGINE SHUT DOWN IN FLIGHT. COTTER PIN SHEARED NUT BACKED OFF MIXTURE CABLE CAUSING MIXTURE TOO LEAN. REPLACED BOLT, NUT AND COTTER PIN. OPS CHECKED OK.SDR 2001FA0000621Roll Servo · malfunctionedOPERATOR THAT ROLL CONTROL BECAME RESTRICTED AND DIFFICULT DURING FLIGHT. INVESTIGATION REVEALED THAT THE PRIMARY ROLL SERVO WAS FOUND TO BE CAUSING RESTRICTION TO CAPSTAN. THIS SERVO WAS REMOVED AND HAS AUDIBLE SOUND OF OBJECTS FLOATING LOOSE INTERNALLY.SDR ERY2001F00000Crankcase · crackedENGINE OIL LEAK, FOUND 3 INCH LONG CRACK IN CRANKCASE ABOVE NR 3 CYLINDER, CRACK SEEMS TO ORIGINATE FROM UPPER CASE LEFT AND EXTEND DOWNWARD.SDR BSY2001F00016Throttle Arm · failedRT ENGINE STAYED AT 2100 RPM ON APPROACH, SHUT ENGINE DOWN. INSTALLED NEW CONTROL LEVER ARM TO SHAFT THROTTLE ASSEMBLY OPS CHECKS GOOD.SDR AUS20011264Line · chafed(AUS) CROSSFEED FUEL LINE LOCATED IN LT WHEEL WELL CHAFING ON UNDERCARRIAGE ACTUATOR CONTROL ROD. THE FUEL LINE HAD BEEN COVERED WITH A PLASTIC SLEEVE AFTER THE DAMAGE HAD OCCURRED. SUSPECT CAUSED BY INADEQUATE SECURING OF FUEL LINE. PERSONNEL/MAINTENANCE ERRSDR AUS20011263Line · chafed(AUS) FUEL CROSSFEED LINE LOCATED IN RT WHEEL BAY CHAFING ON UNDERCARRIAGE DOWNLOCK BACKUP CABLE. SUSPECT LINE INADEQUATELY SECURED. PERSONNEL/MAINTENANCE ERROR.SDR AUS20011262Seat · unserviceable(AUS) CABIN SEATS UNSERVICEABLE. PARTS MISSING. REAR SEAT LUMBAR SUPPORTS CRACKED. VARIOUS SEAT ASSEMBLIES MODIFIED. PERSONNEL/MAINTENANCE ERROR.SDR AUS20011261Brush Holder · cracked(AUS) TRAILING EDGE FLAP ACTUATOR MOTOR BRUSH HOLDER ASSEMBLIES CRACKED. EXCESSIVE HEAT THROUGH FIELD WINDINGS. INSUFFICIENT GREASE OF INCORRECT TYPE IN GEARBOX ASSEMBLY. UNAPPROVED PART.SDR AUS20011260Attach Fitting · corroded(AUS) TRAILING EDGE FLAP ACTUATOR INTERNALLY CORRODED. ATTACHMENT LUG ALSO CORRODED.SDR AUS20011259Actuator · misinstalled(AUS) LT MAIN LANDING GEAR ACTUATOR INCORRECTLY FITTED.SDR AUS20011258Fitting · cracked(AUS) LANDING GEAR ACTUATOR SUPPORT FITTING CRACKED.SDR AUS20011257Actuator · misinstalled(AUS) RT WING FLAP ACTUATOR INCORRECTLY INSTALLED.SDR AUS20011148Frame · cracked(AUS) RT EXIT FRAME CRACKED.SDR AUS20011150Worm Gear · cracked(AUS) LANDING GEAR GEARBOX / ACTUATOR HOURS UNKNOWN (2000 HOURS OVERHAUL). LANDING GEAR GEARBOX FOUND TO HAVE NO OIL. GEAR ACTUATOR WORM DRIVE PNO 35-810076-3 FOUND TO HAVE FATIGUE CRACKS (MECHANICAL HANDLE ATTACHMENT END).SDR AUS20011149Bracket · cracked(AUS) NOSE LANDING GEAR ALIGNMENT GUIDE BRACKET CRACKED.SDR AUS20011098Crankcase · damaged(AUS) ENGINE CRANKCASE HOLED IN AREA OF NR 5 AND NR 6 CYLINDERS.SDR YWB2001F00001Adapter · failedDURING ROUTINE INSPECTION FOUND METAL (STEEL) IN FILTER. REMOVED STARTER ADAPTER AND FOUND SHAFT GEAR NEEDLE BEARING PN 630890 IN ENGINE CASE HAD FAILED. NEEDLES FROM FAILED BEARING HAD ALSO DAMAGED CRANKSHAFT AND IDLER GEARS. SOME DAMAGE DONE TO ENGINE CASSDR YWB2001F00000Crankcase · crackedDURING ROUTINE INSPECTION AN OIL LEAK WAS NOTICED AFT OF NR 2 CYLINDER. FURTHER INVESTIGATION REVEALED CRACK IN CRANKCASE STARTING AT 7TH STUD LOCATION NR 2 CYLINDER RUNNING AFT APPROX 2 INCHES IN LENGTH ENGINE REMOVED FROM SERVICE.SDR AUS20011022Screw · misinstalled(AUS) LT AILERON ATTACHMENT SCREWS INCORRECTLY LOCATED. AILERON HAD PREVIOUSLY BEEN REMOVED FOR ACCESS AND SCREWS HAD MISSED THE ANCHOR NUTS DURING REPLACEMENT. PERSONNEL/MAINTENANCE ERROR.SDR BSY2001F00011Throttle Cable · broken(TFB) M.I.R. RIGHT ENGINE THROTTLE STUCK AT FULL THROTTLE. REMOVED AND REPLACED BROKEN THROTTLE CABLE.SDR AUS20011042Arm · cracked(AUS) LANDING GEAR RETRACTION MOTOR ARM CRACKED.SDR AUS20011123Fitting · damaged(AUS) LT REAR LOWER BATHTUB FITTING DAMAGED.SDR AUS20011122Control Cable · misinstalled(AUS) RT REAR RUDDER CABLE INCORRECTLY ROUTED. CABLE EXCESSIVELY WORN.SDR AUS20011121Windshield · cracked(AUS) WINDSHIELD CRACKED AND INCORRECTLY INSTALLED.SDR AUS20011120Impulse Coupling · missing(AUS) RT ENGINE RT MAGNETO IMPULSE COUPLING NOT INSTALLED.SDR AUS20010908Bolt · worn(AUS) ELEVATOR TRIM TAB ACTUATOR TO TRIM TAB ROD ATTACHMENT BOLTS WORN. FOUND DURING INSPECTION IAW AD/B55/59.SDR AUS20010758Hose · fouled(AUS) LT AND RT MAIN LANDING GEAR BRAKE LINES FOULING ON LANDING GEAR DOORS DURING RETRACTION. INVESTIGATION FOUND THAT THE BRAKE HOSES WERE APPROXIMATELY 53.975MM (2.125IN) LONGER THAN THOSE FITTED TO SIMILAR AIRCRAFT. IN ADDITION THE BRACKETS PNO 35-815264-1SDR AUS20010757Shaft · misinstalled(AUS) LANDING GEAR ACTUATOR MANUAL EXTENSION HANDLE SHAFT INSTALLED 120 DEGREES OUT OF POSITION PREVENTING CORRECT OPERATION OF HANDLE.SDR AUS20010756Uplock Cable · loose(AUS) RT MAIN LANDING GEAR DOWNLOCK CABLE LOOSE. FURTHER INVESTIGATION FOUND THAT THE UPLOCK BLOCK HAD BEEN CONTACTED BY THE UPLOCK ROLLER AND HAD BEEN MOVED OUT OF POSITION. UPLOCK CABLE RETAINING NUTS HAD TORN THROUGH NR 1 WING RIB.SDR BSY2001F00006Light · inoperativePHL MIR RIGHT MAIN GEAR, NO DOWN AND LOCK INDICATION. REMOVED AND REPLACED DOWN AND LOCK BULB. OPS CHECK GOOD.SDR AUS20010629Spar Cap · corroded(AUS) RH WING UPPER SPAR CAP CONTAINED PITTING CORROSION IN AN AREA LOCATED 355.6MM (14IN) OUTBOARD OF THE ENGINE NACELLE. THE PITTED AREA MEASURES APPROXIMATELY 152.4MM (6IN) SPANWISE AND 19.05MM(0.75IN) CHORDWISE. DEPTH OF CORROSION APPROXIMATELY 0.508MM(0.0SDR AUS20010621Pin · cracked(AUS) LH AND RH MAIN LANDING GEAR LOWER TORQUE LINK PINS CRACKED IN THE POSITIONING HOLES.SDR 2001FA0000157Snap Ring · damagedTHE AFOREMENTIONED AIRCRAFT ARRIVED FOR ENGINE OIL & FILTER CHANGE. UPON COMPLETION OF SERVICE, A PRE-ENGINE RUN / WALK AROUND INSPECTION WAS PERFORMED. DURING THIS WALK AROUND INSPECTION THERE WAS A CONSIDERABLE AMOUNT OF EXCESSIVE PLAY NOTED IN ONE OF THE RTSDR BSY2001F00002Relay · malfunctioned(MDW) M.I.R. GEAR SELECTED DOWN, NOTHING HAPPENED AT FIRST, THEN CAME DOWN, OK. MAINTENANCE JACKED AIRCRAFT, COULD NOT DUPLICATE. REMOVED AND REPLACED LANDING GEAR MOTOR AND DYNAMIC BRAKE RELAY FOR PRECAUTIONARY MEASURES.SDR BSY2001F00001Motor · malfunctioned(MDW) M.I.R. GEAR SELECTED DOWN, NOTHING HAPPENED AT FIRST, THEN CAME DOWN OK. MAINTENANCE JACKED AIRCRAFT, COULD NOT DUPLICATE. REMOVED AND REPLACED LANDING GEAR MOTOR AND DYNAMIC BRAKE RELAY FOR PRECAUTIONARY MEASURES.SDR 20010515AP003Control Cable · brokenRH THROTTLE CABLE BROKE IN FLIGHT. PILOT PERFORMED IN FLIGHT SHUTDOWN. INSPECTION REVEALED CABLE BROKE INSIDE FERRULE JUST BEFORE CRIMP ON ENGINE SIDE. THIS CONDITION WOULD BE IMPOSSIBLE TO DETECT BY NORMAL INSPECTION PROCEDURES.SDR AU010326Drag Brace · cracked(AUS) NOSE LANDING GEAR AFT DRAG BRACE CRACKED FROM SEALING RIVET.SDR 20010612CW011Fuel Line · leakingRT ENGINE CLIMBING OUT, AROUND 3000 FEET , NOTICED F/F DOWN TO 12 GPM FOUND FUEL LEAK BETWEEN FUEL LINE AND FUEL MANIFOLD. REPAIRED FUEL LEAK, OPS CHECKED GOOD.SDR 20010405CW001Rod Cap · failedDURING CRUISE FLT RT ENG NR 2 CYL PISTON CONN ROD BROKE LOOSE FROM CRANKSHAFT, PENETRATED UPPER CRANKCASE. NR2 CYL SEP FROM ENGINE, RESTED IN COWLING. THE FORCE OF CONNECTING ROD COMING THROUGH THE CASE BROKE LEFT MAGNETO OFF ITS BASE AND PUNCHED A HOLE IN SDR 20010501CW013Magneto · inoperativeLEFT ENGINE RUNNING ROUGH, FOUND LEFT MAGNETO DEAD. REMOVED AND REPLACED MAGNETO, CLEANED AND GAPPED PLUGS. GROUND RUN, OK.SDR 20010501CW009Wire · brokenGEAR WOULD NOT GO UP. FOUND BROKEN WIRE GOING TO UP LOCK SWITCH, REPAIRED WIRE. OPS CHECKS GOOD.
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