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 DXTA2009081403757Igniter · failedDURING DESCENT TRIED TO START THE APU. GOT THE "APU FAIL" LIGHT AFTER HITTING THE START SWITCH. VISUAL INSP SHOWS SIGN OF A FIRE NEAR THE INTAKE OF THE APU. GAINED ACCESS TO APU EXTERIOR AND ACCOMPLISHED VISUAL INSP OF EXTERIOR COMPONENTS AND ACCESSORIES IASDR DJFA2009032Access Panel · corrodedDURING SCHEDULED MAINTENANCE INSPECTION, TECHNICIANS FOUND SIGNIFICANT CORROSION ON THE INTERNAL SURFACE OF CERTAIN EXTERNAL FUEL ACCESS PANEL COVERS. IN MOST CASES, THE CORROSION WAS CORRECTABLE PER THE STRUCTURAL REPAIR MANUAL BUT FOUR PANELS HAD TO BE REPLSDR DXTA2009073003748Pump · leakingLOST HYD B SYS QUANITY IN FLIGHT RAN CHECKLIST AND UNLOADED THE B PUMP. FOUND THAT RT ENG HYD PUMP FAILED. REMOVED HYD PUMP AND INSTALLED REPAIRED UNIT (REF WO 29760 1.15) PRIMED PUMP, BLED HYD SYS B, RAN ENGINES, AND FOUND NO LEAKS AT THIS TIME AND HYD SYS BSDR DXTA2009073003747Pedal · out of rigLT TOE BRAKE ON BOTH SIDES HAS TO BE PRESSED ABOUT 2 INCHES MORE THAN THE RT BEFORE THE BRAKES ACTIVATE AND THEY ARE GRABBY. FOUND BRAKE PEDALS OUT OF RIG. RERIGGED PEDALS IAW MM 32-42-02. OPERATIONAL CHECKS GOODSDR DXTA200907303746Acm · failedCABIN PAC IS SMOKING / OVERHEATING. REPLACED CABIN ACM DUE TO INTERNAL FAILURE WITH REPAIRED UNIT. WORK PERFORMED IAW MM 21-51-00. LEAK & OPS CHECKS GOOD.SDR DXTA2009072903744Uplock Switch · out of rigDESCENDING THRU 20,000 FT AND 340KTS INDICATED THE NOSE GEAR STARTED TO EXTEND FOLLOWED BY GEAR UNLOCK LIGHT THEN RETRACTED BACK UP. FOUND ALL 3 UPLOCK SWITCHES OUT OF RIG. COMPLIED WITH ADJUSTMENTS OF ALL 3 UPLOCK SWITCHES TO SPEC'S OPS CHECKS GOOD IAW MM 32SDR DXTA2009072703740Alternator · failedPILOT'S WINDOW OUTER PANE SHATTERED AT FL430. REMOVED LT ALTERNATOR AND INSTALLED OVERHAULED UNIT. GROUND RAN AIRCRAFT- ALL ELECTRICAL CHECKS AND ALTERNATOR OPS CHECK GOOD.SDR DXTA2009072703742Generator · odorUPON INITIAL START UP OF APU AND OPENING BLEED AIR ON, RECEIVED ELECTRICAL ODOR IN COCKPIT AND CABIN. ALSO GET FADEC REV ADC L AMBER CAS MESSAGE IN CONJUNCTION WITH ODOR. REMOVED APU GENERATOR S/N 242 AND INSTALLED OVERHAULED GENERATOR S/N 083C IAW AMM 24-32SDR CWQA072309N84EASensor · faultyON ARRIVAL INTO KSAT, BAT NR 1 OVERTEMP LIGHT ON, EMERGENCY DECLARED, UNEVENTFUL LANDING ACCOMPLISHED. MAINTENANCE FOUND BAD TEMP SENSOR AND REPLACED WITH NEW SENSOR.SDR DXTA2009072303737Lead · failedFIRE COMING FROM APU EXHAUST. AT THE SAME TIME, BANGING NOISE IS COMING FROM LEFT WING. T/S AND FOUND APU IGNITOR LEAD BAD REMOVED AND REPLACED WITH NEW. OPS CHECK WAS GOOD IAW MM 49-40-3.SDR DXTA2009072203735O-Ring · leakingCLIMBING THRU FL 410 AMBER "HYD VOLUME LOW B" EICAS MSG DISPLAYED. B-SIDE VOLUME SHOWED 18 PERCENT, DECREASED TO 16 PERCENT. RAN CHECKLIST. UNLOADED B PUMP. FLUID VISIBLE ON BELLY BETWEEN MAIN GEAR WELLS. GAIN ACCESS. REMOVED AFT FUSELAGE BELLY PANELS CLESDR DXTA2009072203734Strut · dischargedAFTER TAKEOFF, GEAR WAS SELECTED UP AND RED IN-TRANSIT LIGHT STAYED ON. GEAR WAS PUT BACK DOWN WITH 3 GREEN INDICATIONS. GEAR SELECTED BACK UP AND IT FUNCTIONED NORMALLY. SERVICED NOSE STRUT PER MM 12-10-38. PERFORMED SEVERAL GEAR SWINGS. OPS CHECKS GOOD.SDR DXTA2009072103733Power Supply · fumesSTRONG ACRID FUMES IN CABIN AREA AROUND SEAT NR 8, NO SMOKE NOTED. FOUND INOP INDIRECT POWER SUPPLY ABOVE SEAT NR 8. REPLACED POWER SUPPLY. OPS CHECK GOOD. WORK DONE IAW ALC INSTALLATION MANUAL AL-11043M.SDR DXTA2009071303726Pump · malfunctionedDURING DESCENT, "HYD VOL LOW B" CAS ILLUMINATED IN FLIGHT. ACCOMPLISHED CHECKLIST AND LANDED WITHOUT INCIDENT. VOLUME QTY INDICATED 10 PERCENT AT FIRST THEN DROPPED TO 0 PERCENT ON LANDING. REPLACED NR 2 HYDRAULIC PUMP OPS CK GOOD IAW MM 29-10-02.SDR DXTA2009070803723Coalescer Bag · odorCOALESCER CLOTHS SMELL FOUL, MORE NOTICEABLE FROM COCKPIT PAC, AND SLIGHT BURNED ODOR AS WELL. REMOVED AND CLEANED COALESCER CLOTHS IAW THE MM TASK 12-10-01-160. OPS CHECK GOOD.SDR DXTA2009070603717Brake Assy · weakPILOT SIDE BRAKES FEEL SOFT AND SEEM TO REQUIRE EXTRA PRESSURE TO GET ADEQUATE BRAKING, ESPECIALLY AT HIGH SPEEDS AND HIGH WEIGHTS, ALSO WHEN SETTING PARKING BRAKE. FOUND LEFT INBOARD & OUTBOARD BRAKE ASSEMBLIES WORN. REPLACED BOTH BRAKES WITH OVERHAULED ASSESDR DXTA2009070603719Brake Assy · weakPILOT SIDE BRAKES FEEL SOFT AND SEEM TO REQUIRE EXTRA PRESSURE TO GET ADEQUATE BRAKING ON LANDING AND WHEN SETTING THE PARKING BRAKE. VERIFIED SQUAWK. PERFORMED BLEED OF POWER BRAKE AND ANTISKID SYSTEM IAW MM 32-402. OP CHECK IS GOOD. PILOT AND COPILOT BRAKESDR DXTA2009070203715Bolt · looseAFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT. NOSE LIGHT REMAINED ILLUMINATED. INSPECTED NOSE GEAR ASSY AND FOUND LOWER TORQUE LINK MOUNTING BOLT LOOSE. RETORQUED TORQUE LINK BOLT. LANDING GEAR OPS CHECKED GOOD. ALL WORK DONE IAW MM 32-20-00 & 32-00-01SDR DJFA2009030Hinge Bracket · crackedDURING A SCHEDULED MX INSP, TECHS FOUND A CRACK IN THE RT INBD HORIZONTAL STABILIZER HINGE BRACKET. REQUIRED NDT INSP WAS PERFORMED AND THE CRACK WAS FOUND TO BE LESS THAN 0.49", THEREFORE A 50 HOUR RECURRING INSP HAS BEEN SCHEDULED FOR THIS ACFT.SDR DXTA2009063003709Compressor · odorDURING CRUISE, DETECTED "ENVIRONMENTAL" BURNING/SMOKE. IT CAME ON AND WENT AWAY 3 SEPARATE TIMES. THE FIRST 2 TIMES IT WAS FAINT. DID SOME PRELIM CHECKS AND DID NOT NOTICE ANY UNUSUAL TEMPS FROM THE PACK SUPPLIES. 3 RD TIME THE ODOR OF BURNING WAS VERY STRSDR AWKA787614Actuator · failedDURING CLIMB OUT WITH THE AUTO PILOT ON, MODE SELECTED TO LNAV AND VERTICAL SPEED, THE ACFT BEGAN AN UN-COMMANDED ROLL TO THE RT WHICH EXCEEDED 40 DEGREES BEFORE THE SIC DISCONNECTED THE AUTOPILOT. THERE WAS A MOMENTARY AMBER CAUTION MESSAGE WHICH WAS TOO FASTSDR DXTA2009061503687Acm · seizedSWEET SMOKE ODOR IN COCKPIT IN CRUISE AT FL430. NO VISIBLE SMOKE. NO PAX SMOKING. EMERGENCY DESCENT TO LANDING PERFORMED. PAX DIDN'T DETECT ANYTHING. FOUND COCKPIT PAC TO HAVE NO COOLING OUTPUT. VISUALLY INSPECTED INLET IMPELLER, VERIFIED NO ROTATION WITH PACSDR DXTA2009060803681Uplock Switch · malfunctionedON DEPARTURE, WHEN RETRACTING THE MLG RECEIVED A RED GEAR UNLOCK LIGHT WITH ALL 3 GREEN MLG LIGHTS EXTINGUISHED. AFTER EXTENDING THE MLG ALL INDICATIONS WERE NORMAL. JACKED ACFT CYCLED GEAR, COULD NOT DUPLICATE, INSPECTED GEAR WELLS, CONNECTORS IN WELLS, AND SDR DJFA2009029Hinge Bracket · crackedDURING A SCHEDULED MX INSP, TECHS FOUND A CRACK IN THE RT INBD HORIZONTAL STABILIZER HINGE BRACKET. REQUIRED NDT INSP WAS PERFORMED AND THE CRACK WAS FOUND TO BE LESS THAN 0.49", THEREFORE A 50 HOUR RECURRING INSP HAS BEEN SCHEDULED FOR THIS ACFT.SDR DXTA2009052803672Cable · misriggedNOSE GEAR THUMP TWICE DURING CLIMB AND TWICE DURING DESCENT. PERFORMED MLG CONTROL MANIFOLD INTERNAL BLEED RATE CHECK IAW MM 32-30-00. CHECKS GOOD. FOUND NOSE GEAR UPLOCK SWITCH AND MLG UPLOCK SWITCH RIGGING AND OPS CHECKS GOO. FOUND BOTH MLG RELEASE CABLES RSDR DXTA2009052803665Unknown · odorAFTER TURNING ON THE ANTI-ICE, A STRONG SULFUR ODOR WAS PRESENT FOR ABOUT 1 MINUTE, THEN DISSIPATED. RAN ACFT & TRIED TO DUPLICATE PROBLEM. NO ODOR NOTED IN COCKPIT OR CABIN. ALL OPERATION OF A/I & ACM'S NORMAL AT HOT & COLD TEMP SETTINGS. CHECKED COCKPIT FORSDR DXTA2009051803655Pcu · leakingLOST B HYD SYS ENROUTE. "HYD B VOL LOW" CAS MSG AROUND FL 210. DURING DESCENT IN TO PHX "RUDDER STBY FAIL" CAS ILLUMINATED. VERIFIED DISCREPANCY, CLEANED RESIDUAL HYD FLUID FROM RUDDER TO JUST FWD OF TAILCONE ACCESS DOOR. FOUND HYD FLUID COLLECTING AT THE BOSDR DJFA2009018Manifold · leakingDURING TAXI CREW NOTED LARGE AMOUNT OF SMOKE FROM THE VENTIALLTION SYS. ACFT WAS STOPPED AND SHUTDOWN. UPON INSP, CREW NOTICED HYD FLUID COATING THE EXTERIOR SURFACE OF THE TAIL SECTION ON THE ACFT. MAINT DISCOVERED THE STANDBY RUDDER HYD MANIFOLD LEAKING HSDR DXTA2009051503654Uplock Switch · malfunctionedDURING CLIMB AND DESCENT WE FELT AND HEARD THE NOSE GEAR THUMP SEVERAL TIMES. REMOVED THE NOSE GEAR UPLOCK SWITCH AND INSTALLED NEW SWITCH AND RIGGED SWITCH IAW CHAPTER 32-30-05 OF THE MM.SDR DXTA2009051503652Actuator · malfunctionedDURING HIGH SPEED DECENT FROM FL 410 TO FL 240 WITH FGC B IN CONTROL ON AUTOPILOT, TAIL SLIDE OUT, THEN RECOVERED. THIS WENT ON AT LEAST 20 TIMES. COMPLETED IMT LOWER RUDDER ACTUATOR TEST, FOUND CURRENT OF BOTH ACTUATORS HIGH, OVER 1100 MIL/AMP- HAVE 2 ACTUSDR DXTA2009051403651Brake · faultyON LANDING ROLL OUT, LT BRAKE IS HYPER SENSITIVE TO INPUTS AND IS ALMOST UNUSABLE BECAUSE IT GRABS VIOLENTLY. INSPECTED THE LTH MLG BRAKES, NO DEFECTS NOTED. MEASURED BRAKE WEAR. O/B BRAKE MEASURED AT 0.4" & I/B BRAKE MEASURED 0.6". TAXI CHECKED AIRCRAFT &SDR DXTA2009051103644Actuator · malfunctionedRUDDER LIMIT FAIL B AMBER CAS MESSAGE ILLUMINATED ON CLIMBOUT. RUDDER LIMITED TO 32 PERCENT. TROUBLESHOT SYSTEM. REMOVED AND REPLACED RUDDER LIMIT ACTUATOR "B" IAW MM 27-23-00. OPERATIONAL AND RIG CHECK GOOD.SDR DXTA2009051103646Acm · failedSMOKE IN CABIN AFTER START, TROUBLESHOT TO RT PAC. SMOKE DISAPATES AFTER PAC HAS BEEN TURNED OFF. TROUBLESHOT SYSTEM, FOUND CABIN PAC FAILED. REMOVED AND REPLACED CABIN ACM IAW MM 21-51-00. SERVICED ACM IAW MM 12-10-01. ALL OPS AND LEAK CHECKS GOOD.SDR DXTA2009050603634Switch · failedWITH POWER AT TAKE-OFF AND DOING A STATIC TAKE OFF, AFTER RELEASING BRAKES WE GET A RED NO TAKE-OFF EICAS MESSAGE. WHITE "A/C MAINTENANCE" CYCLING ON EICAS. TROUBLESHOT TO FAILED FUEL LOW LEVEL SWITCHES. REMOVED SWITCHES AND INSTALLED NEW SWITCHES. RAN ENGINESDR DXTA2009050503632Landing Gear · malfunctionedAFTER TAKEOFF, GEAR WOULD NOT RETRACT. AFTER 4 ATTEMPTS GEAR HANDLE CAME UP AND GEAR RETRACTED, BUT RED "UNLOCK" LIGHT STAYED ON FOR 20-30 SECONDS, THEN WENT OUT. (NOISE AND VIBRATION WAS NOTICED COMING FROM NOSE GEAR). RE-PACKED NLG STRUT AND LUBRICATED NLGSDR DXTA2009050403631A/C Pack · odorSMOKE IN COCKPIT. WHEN PAC'S TURNED ON A BURNED MILDEW ODOR AND HAZE STARTED TO BUILD UP IN COCKPIT. PAC'S SWITCHED OFF AND ODOR / HAZE DISSIPATED. FOUND COCKPIT ACM SIEZED. REMOVED AND REPLACED COCKPIT ACM WITH SERVICEABLE UNIT.SDR DXTA2009043003626Motor · malfunctionedAUTOPILOT ENGAGED THE TRIM CLACKER BEGAN TO RUN AND DID NOT STOP. WITH AUTOPILOT OFF, PRIMARY TRIM FAILED WITH NO CAS MESSAGE. CLACKER RUNS CONTINOUS IN FGC A OR B. REMOVED PRIMARY TRIM MOTOR ASSEMBLY AND INSTALLED A NEW MOTOR ASSEMBLY. OPERATIONAL CHECKED GOSDR DJFA2009028Hinge Bracket · crackedDURING A SCHEDULED MX INSP, TECHS FOUND A CRACK IN THE RT INBD HORIZONTAL STABILIZER HINGE BRACKET. THE REQUIRED NDT INSP WAS PERFORMED AND CRACK WAS FOUND TO BE LESS THAN 0.49", THEREFORE A 50 HOUR RECURRING INSP HAS BEEN SCHEDULED FOR THIS ACFT.SDR DXTA2009042103616Connector · damagedWITH AUTOPILOT ENGAGED TRIM CLACKER SOUNDED AND DID NOT STOP. UPON DISCONNECTING AUTOPILOT ANBER PRI STAB TRIM FAIL AND MACH TRIM OFF CAS MESSAGES ILLUMINATED AS WELL AS CYAN YD FAIL LOWER A CAS MESSAGE. REMOVED AND REPLACED CONNECTOR PV003 IAW MM 20-20-01.SDR DXTA2009042703616Connector · damagedWITH AUTOPILOT ENGAGED, TRIM CLACKER SOUNDED AND DID NOT STOP. UPON DISCONNECTING AUTOPILOT AMBER "PRI STAB TRIM FAIL" AND "MACH TRIM OFF" CAS MESSAGES ILLUMINATED AS WELL AS CYAN "YD FAIL LOWER A" CAS MESSAGE. ILLUMINATED AS WELL AS CYAN YD FAIL LOWER A CASSDR DXTA2009042703618Steering Unit · malfunctionedNOSE GEAR DID NOT RETRACT AFTER T/O. WE HAD GREEN NOSE LIGHT AND RED UNLOCK LIGHT ILLUMINATED WHEN GEAR HANDLE WAS BROUGHT UP. ALL GEAR DOWN INDICATIONS WERE NORM WHEN GEAR HANDLE WAS PLACED DOWN FOR LANDING AFTER ALL APPROPRIATE CHECKLIST WERE COMPLETED. REMSDR DXTA2009042703619Switch · malfunctionedIN FLIGHT AT FL430 AMBER "RUD STBY SYS FAIL" ILLUMINATED. RESET WAS UNSUCCESSFUL. REMOVED AND REPLACED RUDDER STANDBY SWITCH IAW MM 29-20-05. SYSTEM OPS CHECK GOOD.SDR DXTA2009042203613Computer · malfunctionedDURING TAKEFF ROLL #1 MFD & #1 PFD WENT BLANK MOMENTARILY AND AMBER "IAC TEST INOP 1" ILLUMINATED. REMOVED NR 1 IC-800 INSTALLED SUPPLIED UNIT IAW CE750 M/M CH 34-25-01. NR 1 IC-800 OPS CHECK GOOD. RELOADED NAV DATABASE, ACFT DATA BASE, CUSTOM DATABASESDR DXTA2009042103613Computer · malfunctionedDURING TAKEOFF ROLL NR 1 MFD & NR 1 PFD WENT BLANK MOMENTARILY AND AMBER "IAC TEST INOP 1" ILLUMINATED. REMOVED NR 1 INTEGRATED COMPUTER & INSTALLED SUPPLIED UNIT IAW MM 34-25-01. NR 1 INTEGRATED COMPUTER OPS CHECK GOOD. RELOADED NAV DATABASE, ACFT DATA BASSDR DXTA2009042103609Warning Message · false activationRED " NO TAKE-OFF " CAME ON DURING BEGINNING OF T/O ROLL-SPEED LESS THAN 30KTS. (MESSAGE DOES NOT COME WHEN THROTTLES ARE INITIALLY PUT IN T/O POSITION, ACFT HAS TO BE MOVING FOR MESSAGE TO COME ON). CONTACTED PILOTS TO GET FUEL LOAD 3200 LBS POWER TO TAKE SDR DXTA2009042003605Coalescer Bag · dirtyCHEMICAL ODOR COMING FROM COCKPIT AND CABIN PACS. REPLACED RT COALESCER SOCK. LEAK & OPS CHECK GOOD. DONE IAW MM 12-10-01-160.SDR DXTA2009042003606Warning Message · false indication"PITCH FEEL FAIL" CAS MESSAGE ILLUMINATED. STAYED ON FOR 10 MINS., THEN INTERMITTENT OFF AND ON UNTIL LANDING. CONNECTED AIR DATA TEST UNIT AND PERFORMED PITCH FEEL SYSTEM FUNCTIONAL CHECK WHILE AT 4/20/09 OPERATING ELEVATORS AND PITCH TRIM. COULD NOT DUPLICASDR DJFA2009014Acm · odorON DESCENT, PAX REPORTED "BAD" ODOR IN THE CABIN. SUBSEQUENTLY, THE CREW REPORTED A SMOKE HAZE IN THE CABIN. ACFT LANDED SAFELY AT ITS DESTINATION. MX ISOLATED THE PROBLEM TO THE PAX CABIN PACK. MX FOUND METALLIC PARTICLES IN THE COALESCER SOCK INDICATING ANSDR DXTA2009041703603Steering Unit · faultyNOSE WHEEL SHIMMY AT 30 KTS WAS EXCESSIVE. ABORTED T/O NO FASTER THAN 60 KTS. TRIED TO HAVE BACK PRESSURE ON YOKE TO EASE NOSE WHEEL SHIMMY, HAD NO EFFECT. REMOVED FAULTY NOSE STEERING UNIT INSTALLED A MODIFIED UNIT BLED HYDARULIC SYSTEM REGG NOSE STEEPINSDR DJFA2009027Hinge Bracket · crackedDURING A SCHEDULED MX INSP, TECHS FOUND A CRACK IN THE RT INBD ELEVATOR HINGE BRACKET. THE REQUIRED NDT INSP WAS PERFORMED AND THE CRACK WAS FOUND TO BE GREATER THAN 0.30". ELEVATOR HINGE BRACKET WAS REMOVED AND REPLACED.
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