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 = '750' 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 = '750' 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 DXTA2011072604671Spacer · out of positionAFTER TAKEOFF, MLG HANDLE WOULD NOT MOVE TO THE UP POSITION. FOUND SPACER FOR SWITCH STRIKER IN WRONG POSITION, REPOSITIONED SPACER, OPS CHECKED GOOD IAW MM 32-20-02.SDR DXTA2011072504666Actuator · malfunctionedON TAKEOFF, GEAR HANDLE UP & RED UNLOCK LIGHT STAYED ILLUMINATED AS WELL AS NLG GREEN DOWNLOCK LIGHT. COULD HEAR NLG STILL EXTENDED. PUT HANDLE DOWN & RECEIVED 3 GREEN NORMAL INDICATIONS. INSTALLED A REPAIRED NLG ACTUATOR, LEAK & OPS CHECKED NORMAL.SDR DXTA2011072504668Pump · leakingDURING FLIGHT AT FL410, LEFT HYD QTY AT 22 PERCENT. NOTICED 1 PERCENT DROP EVERY 3 MINUTES. AT 19 PERCENT, AMBER CASS MESSAGE HYD VOLUME LOW ILLUMINATED. CONDUCTED CHECKLIST. HAD TO BLOW DOWN GEAR FOR LANDING AND USE THE EMERGENCY BRAKE UNTILL STOPPED. R SDR DXTA2011071804660Control Cable · damagedRT BRAKE GRABS DURING INITIAL APPLICATION. R & R BRAKE CABLE IAW MM 32-42-02. OPS CHECKED GOOD.SDR DXTA2011071404662Module · failedAFTER TAKEOFF, GEAR FAILED TO RETRACT AFTER GEAR HANDLE MOVED TO UP POSITION, INDICATION WAS 3 GREEN AND 1 RED. R & R MLG CONTROL MODULE IAW MM 24-53-00. OPS CHECKED GOOD.SDR DXTA2011071304658Actuator · malfunctionedON INITIAL FLIGHT CONTOL CHECK, LT RUDDER FELT HARD TO PUSH. SUBSEQUENT CHECKS ON GROUND, IT PERFORMED NORMALLY. ON ROTATION PF IN RT SEAT SAID THE PLANE WAS HARD TO CONTROL AND LT RUDDER REQUIRED RUDDER TRIM OVER HALF DISPLAY TO FLY STRAIGHT AND LEVEL. R & SDR DXTA2011071004647O-Ring · leakingIN CRUISE FLIGHT AT FL400, DURING CRUISE CHECKLIST, NOTED HYD VOL WAS 20 PERCENT AND DECREASING. ONCE HYD VOL A CAS ILLUMINATED FOLLOWED APPROPRIATE CHECKLIST AND LANDED WITHOUT INCIDENT. DETERMINED HYD LEAK FROM RUDDER PCU UPPER UNIT HAD O-RING CUT ON PRESSUSDR DXTA2011070904651Adc · malfunctionedCLIMBING OUT OF 15,000 MSL, 270KIAS, AURAL OVER-SPEED SOUNDED. NO CAS MESSAGES PRESENT. PULLED AND RESET WARN AUDIO 1 AND WARN AUDIO 2 WITH NEGATIVE RESULTS. INSTALLED AIR DATA COMPUTER NR 1 REF MM 34-11-01. COMPLIED WITH LEAK TESTS IAW THE MM 34-90-10 ASDR DXTA2011070904649Manifold · inoperativeDURING TAKEOFF AND AFTER LANDING GEAR SELECTED UP, THE UNLOCK LIGHT REMAINED ON AND THE GEAR FAILED TO RETRACT. ON OCCASION GREEN GEAR LIGHTS CAME AND WENT. COMPLETED GEAR WON'T RETRACT CHECKLIST. EICAS INTERMITTENTLY DISPLAYED AMBER SPEEDBRAKES ON SYNOPTIC.SDR DXTA2011063004637Acm · seizedSMOKE IN THE COCKPIT WHILE PARKED ON RAMP. APU ON, NORMAL BLEED, BOTH PAC'S ON HIGH, ISOLATION VALVE OPEN. ACM SEIZED. REMOVED COCKPIT ACM AND INSTALLED REPAIRED ACM. OPS AND LEAK CHECKED GOOD. WORK DONE IAW MM 21-51-00.SDR WTXR23926.2.15Hinge Bracket · corrodedTHE UPPER AND MIDDLLE RUDDER HINGE BRACKETS WERE FOUND TO BE SEVERLY CORRODED. BRAKET PN'S: 6731009-4 & 6731008-8. CORROSION FOUND DURING THE PAINT PROCESS. BRACKETS WERE REPLACED WITH NEW UPON DISCOVERY. STRUCTURAL DAMAGE REPORT WAS SUBMITTED TO MFG.SDR DXTA2011062404634Steering Unit · malfunctionedNOSE GEAR DID NOT RETRACT AFTER GEAR HANDLE WAS SELECTED UP. MAIN GEAR RETRACTED. NOSE GEAR GREEN LIGHT REMAINED ILLUMINATED AND RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PURSUANT TO THE ABNORMAL CHECKLIST, LANDING GEAR HANDLE WAS SELECTED DOWN. MAIN GEASDR DXTA2011062204629Brake Sys · malfunctionedON LANDING ROLL OUT RT BRAKE IS GRABBING FOLLOWED BY A LOUD LONG "SQUEAK" AND VIBRATION. ON POST FLIGHT INSPECTION, THE BRAKE IS VERY HOT AND SMOKING. INSPECTED AND VERIFIED METERING VALVE WAS HITTING STOPS. CHECKED BRAKE HYD PRESSURES ON THE LT AND RT BRSDR CVGA1117203Warning System · activatedCYAN MESSAGE "ACFT MAINTENANCE" ON THE GROUND.SDR DXTA2011062004627Seal · leakingGEAR HANDLE WOULD NOT COME OUT OF THE DOWN POSITION AFTER TAKE OFF. COMPLIED WITH SL 750-37-39, NOSE LANDING GEAR STRUT SEAL REPLACED DUE TO LEAKAGE. SERVICED AS REQUIRED, LEAK AND OPS CHECKED NORMAL.SDR DXTA2011062004626Acm · failedAT FL430 SMELLED AND SAW SMOKE IN THE COCKPIT. TROUBLESHOT TO FAILED ACM ON AFT ECU. GAINED ACCESS AND REMOVED FAILED PART. INSTALLED REPAIRED ACM IAW MM 21-51-00. SYS OPS AND LEAK CHECK GOOD. REPLACED BOTH WATER SEPARTOR COALESCER CLOTHS PN 246451-3 WITH NESDR CA110616004Pump · failedDURING CRUISE FLIGHT, CREW NOTED A HYD VOLUME LOW (B SYS) ANNUNCIATION ON THE EICAS. FLIGHT CREW FOLLOWED CHECKLIST PROCEDURES AND OFFLOAD HYD B SYS. ACFT DIVERTED, WHERE A PAN CALL WAS INITIATED. ACFT LANDED WITHOUT INCIDENT. A VISUAL INSP OF THE ACFT REVESDR DXTA2011061704622Wire · damagedLANDING GEAR WOULD NOT RETRACT. LANDING GEAR HANDLE WOULD NOT RELEASE OR MOVE. REPAIRED DAMAGED WIRING AT NOSE GEAR SQUAT SWITCH IAW WIRING MANUAL 20-10-01- PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKED GOOD IAW MM 32-00-01.SDR DXTA2011061504616Actuator · leakingUNLOCK LIGHT REMAINED ILLUMINATED AFTER THE GEAR HANDLE WAS SELECTED TO THE UP POSITION. THE NOISE APPEARED TO BE COMING FROM THE NOSE GEAR. SERVICED NLG STRUT IAW MM 12-10-38. R & R NLG ACTUATOR IAW MM 32-30-03.SDR DJFA2011029Entertain Sys · failedAFTER LANDING, CREW REPORTED BURNING ODOR IN THE AFT CLOSET/ LAVATORY AREA. NO SMOKE WAS NOTED. MX ISOLATED THE ODOR TO THE CABIN ENTERTAINMENT SYS CONTROL MODULE. THE UNIT WAS REPLACED.SDR DXTA2011060604610Pitch Control · bindingELEVATOR PITCH EXCESSIVELY HEAVY. MANUAL PITCH CHANGES ALMOST FELT AS IF THE SYS WAS BINDING.SDR CVGA 11 155 1Warning System · activatedDURING PREP FOR TAKEOFF, ICAS MESSAGE (CYAN: YD FAIL UPPER B), NO TAKEOFF INITIATED, RETURNED TO RAMP.SDR CVGA 11 158 1Unknown · failedAMBER EICAS MESSAGE: PITCH FEEL FAIL.SDR DXTA2011060604604Unknown · smokePOWERED UP APU. WHEN BLEED AIR IS TURNED ON THE CABIN FILLS UP WITH SMOKE. COCKPIT & CABIN ACM OPS & LEAK CHECKED GOOD IAW MM 21-61-00. NO SMOKE NOTED.SDR DXTA2011060204603Acm · odorTHERE WAS A DISTINCT ODOR OF BURNED WIRES IN THE COCKPIT JUST PRIOR TO LANDING THAT QUICKLY DISSAPATED. NO ABNORMAL ELECTRICAL INDICATIONS WERE NOTED AND NO CIRCUIT BREAKERS WERE TRIPPED. AFTER ACM & WATER SOCK REPLACEMENT, RAN AIR CONDITIONING SYS USING ASDR DXTA2011060204602Strut · dischargedGEAR WOULD NOT RETRACT WITH THE GEAR HANDLE IN THE RETRACT SELECTION POSITION. FOUND LOWER BARREL UNDER SERVICED ON NOSE GEAR. SERVICED NOSE STRUT IAW MM 12-10-38. INSPECTED NOSE LANDING GEAR AND MAIN LANDING GEAR. NO DEFECTS NOTED.SDR DJFA2011025Roll Pin · sheared** SUPPLEMENTAL INFORMATION ** PRIOR TO FLIGHT, CREW REPORTED LEFT SPOILERON NOT MOVING WITH FLIGHT CONTROL INPUT. MAINTENANCE PERSONNEL DISCOVERED TWO ROLL PINS SHEARED ON THE AILERON-ROLL SPOILER MIXER ASSEMBLY. THE SPOILER MIXER ASSEMBLY WAS REPLACED.SDR DXTA2011052704593Wheel · wornDURING TAKEOFF ROLL, AT APPROX 50 KNOTS, A SEVERE VIBRATION DEVELOPED IN THE NOSE GEAR AND THE TAKEOFF WAS ABORTED. R & R NOSE WHEELS IAW MM 32-41-01. TORQUED, SERVICED AND SAFTIED AS REQUIRED.SDR 2011F00120Door · out of adjustLOSS OF BAGGAGE COMPARTMENT PRESSURE RESULTING CHANGE IN CABIN PRESSURE. PILOTS DONNED OXYGEN MASK. NORMAL DECENT TO LOWER ALTITUDE. COMPLIED WITH ABNORMAL CHECKLIST. ISOLATED BAGGAGE COMPARTMENT. CONTINUED FLIGHT TO DESTINATION. LANDED WITHOUT INCIDENT. CHESDR DXTA2011051204578A/C Pack · fumesFUMES IN CABIN, TROUBLESHOT TO LT PACK (COCKPIT). R & R AFT COCKPIT ACM, OPS AND LEAK CHECKED GOOD. ACM WOULD NOT NOT COOL BELOW 79 DEGREES, ALSO R & R WATER SEPARATE COALESER. OPS CHECKED GOOD IAW MM 21-51-00.SDR CVGA 11 130 2Warning System · activatedABORTED TAKEOFF (<65KTS) DUE TO RED NO TAKEOFF ON EICAS.SDR DXTA2011051004576Fire Warning · false activation"FIRE DETECT FAIL R" AMBER CAS MESSAGE DISPLAYED DURING FLIGHT AND REMAINED UNTIL ACFT SHUTDOWN. VERIFIED INDICATION IS STILL PRESENT. OPENED LOWER COWLING. NOTED FIRE LOOP CONTACTING IN MULTIPLE LOCATIONS. REMOVED FIRE DETECTOR ASSY, INSTALLED NEW ASSY. SDR DXTA2011050404572Strut · damagedGEAR UNLOCK LIGHT (RED) ILLUMINATED IN FLIGHT WHILE CLIMBING OUT OF 38,000 FT. AT THE SAME TIME WE HEARD A THUD NOISE COME FROM THE NOSE GEAR COMPARTMENT AREA. UNLOCK LIGHT REMAINED ILLUMINATED FOR ABOUT 30 THEN EXTINGUISHED 10 MIN FROM LANDING. LANDING GEARSDR DXTA2011050204570Line · failedWHEN SELECTING GEAR HANDLE TO UP, HYD A SYSTEM QUANTITY WENT TO ZERO. GEAR DID NOT RETRACT. MANUAL GEAR EXTENTION WAS PERFORMED. VERIFIED "A" RESERVIOR DEPLETED. FOUND RT MLG RETRACT LINE BURST CAUSING LOSS OF ALL FLUID. REMOVED PRESSURE LINE FROM HYD PUMSDR CNQR528863Shaft · shearedHYD VOLUME LOW (A) CAS MESSAGE ILLUMINATED. VERIFIED ZERO QUANTITY ON THE EICAS SYS. THE HYD PUMP FAIL (A) CAS MESSAGE CAME ON. THE CREW ACCOMPLISHED THE CHECKLIST INCLUDING THE GEAR BLOW DOWN AND EMERGENCY BRAKING.SDR Z5FA20110426001Pump · failedENROUT, CREW NOTICED "A" SYS HYD FAILURE. CREW FOLLOWED AFM EMERGENCY PROCEDURES AND DIVERTED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. SYS WAS TROUBLESHOT TO A LT ENGINE HYD PUMP FAILURE. REPLACED LT ENGINE HYD PUMP, CASE DRAIN FILTER, PRESSURE FILTESDR Z5FA042611N442WP1Hydraulic System · failedENROUTE, CREW NOTICED "A" SYS HYD FAILURE. CREW FOLLOWED AFM EMERGENCY PROCEDURES AND DIVERTED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT IS CURRENTLY IN MX.SDR DXTA2011042704565Steering Unit · malfunctionedAFTER TAKEOFF, MLG CAME UP & NLG STAYED DOWN. CONFIRMED BY TOWER. PUT HANDLE DOWN & BOTH MLG CAME DOWN. LANDED NORMAL. TURNED NOSE WHEEL LT & RT, CYCLED GEAR TO CHECK NOSE WHEEL CENTERING. PERFORMED 10 CENTERING CYCLES & DURING 1 CYCLE WHEEL CENTERED BUT SDR DXTA2011042604562Fuel Cell · leakingWING TANK OVERFILL LT CAS MESSAGE. FUEL VENTED FROM LT WING TANK AT CRUISE FL 270 & NO TURBULENCE FOR APPROX 15 MINUTES. NORMAL CLIMB IN LIGHT TURBULENCE. YAWED ACFT TO STOP VENTING, NO SUCCESS. VENTING STOPPED AT APPROX 18000 FT. FUEL ABOARD 10000 LBS AT SDR DJFA2011015Actuator · shearedAFTER ENGINE START, THE CREW REPORTED PITCH AND ROLL CONTROL FELT AS THOUGH IT WAS BINDING. MX FOUND THE PITCH FEEL ACTUATOR TO BE SHEARD AT THE ROD END. THE PTICH FEEL ACTUATOR WAS REPLACED.SDR I5EA201101Control Module · failedDURING ARRIVAL, THE AUTOPILOT DISCONNECTED AND THE EICAS INDICATED A PRIMARY PITCH TRIM FAIL. CREW REVERTED TO THE SECONDARY TRIM SYS AND SHORTLY AFTERWARD RECEIVED A SECONDARY TRIM FAIL MESSAGE. CREW DISCONTINUED APPROACH IN ORDER TO RUN THE JAMMED STABILIZSDR DXTA2011042504559Warning Light · illuminatedSTATIC TAKEOFF, AFTER 4 SECONDS OF TAKEOFF ROLL, RECEIVED 2 AMBER REV ON FLIGHT MODE INDICATOR. CAS MESSAGES FADEC REV ADC L/R ALSO RECEIVED. NOTICED WHEN STARTING NR 2 ENGINE, MOMENTARILY RECEIVED AMBER REV ON LT OPPOSITE SIDE FLIGHT MODE INDICATOR. DISCONNSDR DXTA2011042104552Brake · dirtyAFTER LANDING, FELT BRAKES HANGING UP. WHILE TAXIING, PULLED POWER BACK AND PLANE CAME TO A COMPLETE STOP. WHILE PULLING INTO RAMP, BRAKES WERE NOT BINDING AS BAD. DURING POST FLIGHT INSPECTION, LT MAIN BRAKES WERE COLD TO THE TOUCH AND THE RT MAIN BRAKES WERSDR DXTA2011041804549Carbon Seal · leakingON SHORT FINAL, HAD BRIEF EXHAUST LEAK, SMOKEY ODOR FROM COCKPIT OVERHEAD VENT. RAN APU AND TURNED ON BLEED AIR. THERE IS A NOTICEABLE OILY ODOR IN COCKPIT AND CABIN. STARTED ENGINES AND TURNED OFF APU. ODOR WENT AWAY. BOROSCOPED AREA AND FOUND OIL LEAKINSDR DXTA2011041804548Drive Unit · failedFLAP FAIL AMBER CAS DURING APPROACH AND LANDING. FLAPS FAILED AT APROX 2 DEGREES WITH SLATS OUT. FOUND FLAP CONTROL BITE CODE 2. TESTED FLAP PDU IAW MM 27-50-00 CLUTCH TORQUE AMFRAME FAILED- 112 AMPS MAX. FLAP PDU R & R IAW MM 27-52-00 (R35). REMAINDER OF SDR DXTA2011041104543Brake · weakBRAKES ARE VERY "MUSHY" WHEN PRESSURE IS APPLIED. BRAKES ARE ALSO GRINDING WHEN STOPPING. BLED BRAKES NOTED SMALL AMOUNTS OF AIR REMOVED FROM SYS. USED COMPRESSED AIR TO REMOVE CARBON DUST FROM BRAKE STACKS. TAXIED ACFT. BRAKES ARE FIRM, NO GRINDING NOISE SDR DXTA201041104542Steering Unit · inoperativeAFTER TAKEOFF, UPON GEAR RETRACTION, THE NOSE GEAR DID NOT RETRACT AND THE RED UNLOCK LIGHT REMAINED ILLUMINATED. JACKED ACFT AND CYCLED NOSE GEAR, OPS CHECKED GOOD. LOWERED GEAR AND TURNED NOSE GEAR AND ATTEMPTED TO RETRACT. NOSE WOULD NOT CENTER OR RETRACSDR DXTA2011040904540Landing Gear · failedTHE NOSE GEAR FAILED TO EXTEND WHEN THE GEAR HANDLE WAS PLACED DOWN. A UNUSUAL GRINDING NOISE WAS HEARD DURING GEAR EXTENTION. BLOW DOWN AND D-RING FAILED TO DROP GEAR. LOW FLYBY CONFIRMED NOSE GEAR STILL IN WHEEL WELL. ON GO AROUND GEAR DOORS OPENED. APPLISDR DXTA2011040604539Control Valve · inoperativeAFTER GEAR RETRACTION, THE GEAR UNLOCK LIGHT REMAINED ILLUMINATED FOR ABOUT 30 SECONDS LONGER THAN NORMAL, ACCOMPANIED BY EXCESSIVE NOISE COMING FROM THE NOSE GEAR AREA. COMPLIED WITH THE LANDING GEAR WILL NOT RETRACT CHECK LIST, AND GEAR EXTENDED NORMALLY. FSDR DXTA2011040104535Actuator · inoperativeAFTER LANDING GEAR RETRACTION, GEAR UNLOCK LIGHT REMAINED ILLUMINATED ABOUT 25 SECONDS LONGER THAN NORMAL, ACCOMPANIED WITH LOUD WIND NOISE THEN FOLLOWED BY THE SOUND OF THE NOSE GEAR LOCKING UP AND A SLOW REDUCTION IN NOISE AS THE NOSE GEAR SLOWLY CLOSED AND
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