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 O2GA2018091390001Generator · failedAPU GENERATOR KICKED OFF LINE AND SMOKE NOTED FROM TAIL CONE. INSPECTION IDENTIFIED APU GENERATOR HAD EXPERIENCED A HIGH HEAT INCIDENT AND INTERNAL FAILURE. AIRCRAFT WAS FERRIED TO MANUFACTURER FOR FURTHER INVESTIGATION. SDR SUPPLEMENT TO FOLLOW.SDR DXTA2018090901408Pump · failedHYDRAULIC FLUID LEAK - HYDRAULIC B FAIL. HYDRAULIC OIL ALL OVER RIGHT REAR OF AIRCRAFT. 0 QUANTITY AND 0 PSI. STRONG BURNING ODORS IN CABIN.//SIGNOFF// REMOVED AND REPLACED THE FOLLOWING PARTS REMOVED AND REPLACED RH B SIDE HYRQ ENG. DRIVEN PUMP REF CE-750 AMSDR DXTA2018073100318Cowling · damagedCOWLING DAMAGED. REPAIRED.SDR 9JLA2018080919551Position Sensor · defectiveDURING FLIGHT CONTROL CHECKS, PRIOR TO FLIGHT, IT WAS DISCOVERED THAT THE UPPER RUDDER CHANNEL B FAILED THE PRE-FLIGHT CHECKS. THE UPPER RUDDER POSITION WOULD STAY FULLY DEFLECTED UNTIL RESET. THE MAINTENANCE FOUND THE CHANNEL B RUDDER POSITION SENSOR DEFECTISDR VQMA2018080103001Hydraulic Line · leakingDEPARTED KMAE FOR KCLT AT 2027Z. DURING THE CLIMB TO FL410 AN AMBER CAS MESSAGES APPEARED STATING THAT THE HYDRAULIC QUANTITY IN B SYSTEM WAS LOW. WHILE THE PNF GRABBED AND READ THROUGH THE CHECKLIST, THE PF TURNED TO THE HYDRAULIC SYSTEM PAGE TO VIEW SYSTEM BSDR EBVR20180702002Skin · corrodedBLEND AND EVALUATE CORROSION ON UPPER OUTBOARD SURFACE OF LT WING SKIN AT AFT SPAR LOCATION.BLENDED AND REMOVED ALL VISIBLE CORROSION FROM UPPER OUTBOARD SURFACE OF LT WING SKIN AT AFT SPAR LOCATION UNTIL VISUALLY ELIMINATED.PERFORMED REPAIR TO LT UPPER WING SSDR EBVR20180702001Skin · corrodedBLEND AND REMOVE CORROSION AND EVALUATE 1 EACH PIN HOLE ON THE R/H SIDE OF THE FUSELAGE, JUST AFT OF THE NOSE ACCESS DOOR. PERFORMED REPAIR TO RT NOSE SKIN AFT OF AVIONICS DOOR.SDR DXTA2018062200083Spar Cap · corrodedREPAIR OF LT HORIZONTAL AFT UPPER SPAR CAP CORROSION. AIRCRAFT REPAIR DEFINITION REPORT NR S-750-0187/13RD DATED JUNE 20, 2018 WITH FAA FORM 8100-9 DATED 6/21/2018.SDR 2018FA0000188Skin · dentedRT WING SKIN DENTED. REPAIRED.SDR 2018FA0000187Link · corrodedRIGHT MLG TRAILING LINK WAS CORRODED. REPAIRED.SDR 2018FA0000183Seal · blew outHP BLEED AIR SEALS FAILED AT ENGINE OUTLET 12 O'CLOCK POSITION ON BOTH R AND L ENGINES. INSPECTION REVEALED BOTH UPPER COWLINGS SCORCHED AND DELAMINATED. CONTACTED ENGINEERING FOR DISPOSITION AND GAINED APPROVAL FROM FSDO.SDR 2018FA0000173Signal Cond Unit · faultyCENTER FUEL TANK FUEL QUANTITY INDICATION DASHED OUT. FUEL QUANTITY SIGNAL CONDITIONER PN 9914422-12.SDR DXTA2018060761049Landing Gear · malfunctionedAFTER TAKEOFF, RETRACTED THE GEAR. ALL GEAR CAME UP, BUT THE NOSE GEAR STARTED CYCLING UP AND DOWN. THE NOSE GEAR INDICATIONS CYCLED FROM RED TO GREEN. PUT THE GEAR HANDLE BACK DOWN. ALL GEAR INDICATIONS STAYED GREEN, THE LANDING GEAR LOCK WAS CYCLING ON ANDSDR DBCA2018060640002Coupler · failedCREW CALLED SAYING THEY HAVE A COMPUTER ISSUE WITH RUDDER DEFLECTION NOTIFICATION ON GROUND DURING PREFLIGHT INSPECTION. DETERMINED THE POSITION TRANSMITTER FLEXIBLE COUPLER WAS UNSERVICEABLE. REPLACED THE FLEXIBLE COUPLER WITH NEW. OPS CHECKED GOOD.SDR DXTA2018053001013O-Ring · leakingDURING DESCENT THROUGH 20,000', -A- HYDRAULIC QUANTITY DROPPED BELOW 16%. DROPPED TO 13% BEFORE UNLOADED. PNEUMATIC GEAR BLOWDOWN AND EMERGENCY BRAKE WERE USED. AFTER SHUTDOWN, HYDRAULIC FLUID COULD BE SEEN FROM THE CENTER OF THE FUSELAGE NEAR THE MAIN GEAR USDR 2018FA0000162Spar Cap · damagedRIGHT WING FORWARD SPAR HAD OVERSIZED FASTENER HOLES, WS 34.SDR AWKA2018060101Gcu · failedAT FL450, FLIGHT CREW NOTED THE LT BATTERY VOLTAGE WAS AMBER AND INDICATING BETWEEN 30V AND 31V AND FLUCTUATING, ALSO NOTED BATTERY TEMPERATURE ON THE LEFT WAS SLIGHTLY HIGHER THAN THE RIGHT AND WAS SLOWLY INCREASING, ALL OTHER INDICATIONS WERE NORMAL. CREW RSDR 2018FA0000152Valve · faultyPARKING BRAKE VALVE FAILS TO HOLD PRESSURE.SDR 2018FA0000151Valve · leakingINSTALLED PARKING BRAKE VALVE AS A A REPLACEMENT FOR FAILED VALVE. PARKING BRAKE VALVE FAILS TO HOLD PRESSURE ON LT INBD BRAKE. FAILS FUNCTIONAL CHECK.SDR 9JLA2018042711498Hydraulic Line · chafedDURING POST FLIGHT INSPECTIONS, THE RT THRUST REVERSER PRESSURE HYDRAULIC LINE WAS FOUND TO BE CHAFED BY NEARBY B-NUT CAUSING A HYDRAULIC LEAK. . THE LOCATION OF THE CHAFED HYDRAULIC LINE WAS WITHIN THE AFT MAINTENANCE BAY ON THE RT SIDE OF THE COMPARTMENT JUSSDR DXTA2018041900161Skin · damagedRT WING TIP SKIN DAMAGED. REPAIRED IAW MEMO DQ11936M1.SDR 2018FA0000143Valve · faultyPARKING BRAKE VALVE FAILED . REPLACED THE PARKING BRAKE VALVE.SDR 2018FA0000142Valve · faultyPARKING BRAKE FAILS TO HOLD PRESSURE IAW MM REQUIREMENTSSDR 2018FA0000135Brake Assy · noisyWHEN TOWING AIRCRAFT ON GROUND BRAKE ASSEMBLY EXHIBITED EXCESSIVE NOISE.SDR 2018FA0000134Door Seal · damagedACOUSTIC UPPER SEAL ON MAIN CABIN DOOR WAS FOUND WITH A PIN HOLE AIR LEAK AFTER BEING REPORTED BY THE FLIGHT CREW DUE TO AUDIBLE INDICATION. SEAL WAS DEFERRED PER THE MEL. SEAL WAS CHANGED BY MAINTENANCE ON 4/6/18.SDR 2018F00149Skin · damagedDAMAGE TO SLAT SKIN AND GOUGE TO INBOARD HLE SKIN P/N 6722402-41. ACCOMPLISHED ENGINEERING LETTER DQ11736M1.SDR 2018FA0000127Skin · damagedDAMAGE TO SLAT SKIN AND GOUGE TO INBOARD HLE SKIN P/N 6722402-41. ACCOMPLISHED ENGINEERING LETTER DQ11736M1.SDR DXTA2018032900143Skin · corrodedFUSELAGE BELLY SKIN CORRODED. REPAIRED IAW S-750-0198/14RD, MAJOR REPAIR.SDR 2018FA0000104Cable · chafedCABLE INSIDE THE LT WING CHAFED THROUGH. CABLE SUPPORT CAUSING DAMAGE TO WING RIB.SDR 2018FA0000082Skin · corrodedREPAIR OF LEFT FUSELAGE SKIN CORROSION PER ENGINEERING REPAIR DEFINITION REPORT NR S-750-0005/19RD.SDR CVGA20180312001Not Reported · unknownWHEN AIRCRAFT DEPARTED CVG (FOR A MAINTENANCE TEST FLIGHT) AND AFTER GEAR WAS PUT IN THE RETRACT POSITION, THE "A" SIDE VOLUME READ 17%. DECLARED EMERGENCY AND RETURNED TO CVG. LANDING AND ROLLOUT WERE UNEVENTFUL.SDR 9JLA2018021911496Seal · leakingWHILE WAITING FOR PASSENGERS WITH THE APU RUNNING AND THE AIR CONDITIONING OPERATING, THE CREW REPORTED THAT VISIBLE SMOKE WAS SEEN IN THE COCKPIT WITH THE ODORS OF SOMETHING GETTING HOT, WERE UNABLE TO CONTROL THE COCKPIT TEMP. THE CREW SHUTOFF THE COCKPIT AISDR CWQA2018021600015Window · crackedDURING THE CLIMB AT 31,000 FEET THE RIGHT FORWARD COCKPIT SIDE WINDOW OUTER PLY SHATTERED. THE CREW LANDED THE AIRCRAFT WITHOUT INCIDENT AND A NEW WINDOW WAS INSTALLED.SDR DXTA2018010100517Shutoff Valve · failedWHILE STARTING THE APU WHILE AIRBORNE THERE WAS A LOUD BOOM AND SIMULTANEOUSLY THE APU FIRE ANNUNCIATOR ILLUMINATED MOMENTARILY. THE APU WAS SHUT DOWN AND THE APU FAUL ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED THE FUEL SHUTOFF VALVE SOLENOID AND FUEL FLOWSDR 2018F00030O-Ring · failedAFTER TAKEOFF, DURING FLIGHT A FAILURE OF THE NR 1 HYDRAULIC SYS OCCURRED. THE PRESSURE WAS LOST AND THE QTY INDICATION DROPPED TO ZERO. AFTER COMPLETING THE CHECKLIST, ACFT LANDED. EMERGENCY GEAR EXTENSION USED, AND EMERGENCY BRAKING, FOUND AN O-RINSDR 2018F00082Doubler · gougedDOUBLER GOUGED.SDR 2018FA0000006Support · corrodedREPAIR OF LT AUX. SPAR MLG BEARING SUPPORT BORE CORROSION.SDR AWKA201801040001Landing Gear · malfunctionedWHILE CONDUCTING A MAINTENANCE CONFIDENCE FLIGHT FOR AN UNRELATED ISSUE, AND REACHING AN ALTITUDE OF APPROXIMATELY FL200, FLIGHT CREW EXPERIENCED SEVERAL THUMPS FROM THE NOSE GEAR AND NOTED THE RED UNLOCK ANNUNCIATOR WAS ILLUMINATED. THE THUMPING STOPPED AND TSDR DXTA2017122800001Converter · dirtyPASSENGERS AND CREW SMELLED A STRONG SMOKY ODOR COMING INTO CABIN. CLEANED FWD & AFT WATER SEPARATOR AND DRAIN LINE. CLEANED OZONE CONVERTER. RAN SYSTEM, NO DEFECTS NOTED. WORK PERFORMED IAW MM 21-11-00, 21-21-00, 21-22-00, 21-51-00, AND 21-71-00.SDR CVGA20171226001Motor · failedFLAPS FAILED. FLAPS WERE SELECTED AS USUAL. SLATS EXTENDED. FLAPS DID NOT. RAN CHECKLIST, BUT FLAPS REMAINED FAILED. TROUBLESHOOTING LED TO FAULTY FLAP DRIVE MOTOR.SDR DXTA2017121806434Display · unserviceableDU CAS MESSAGE AND PFD 2 CIRCUIT BREAKER POPPED. STRONG ELECTRICAL ODOR ALSO. CORRECTIVE ACTION: CONFIRMED PFD 2 BREAKER TRIP IMMEDIATELY WITH AVIONICS SWITCH ON. REMOVED #5 DU SCREEN. APPLIED POWER AND CB IS NO LONGER TRIPPING. INSPECTED WIRING BEHIND RH CB PSDR DXTA201712120001Light · inoperativeLEFT GEAR GREEN INDICATOR IS NOT ILLUMINATED. DECLARED EMERGENCY FOR UNSAFE LANDING GEAR INDICATION. DETERMINED LIGHT BULBS INOPERABLE. REMOVED AND REPLACED LEFT LANDING GEAR INDICATION LIGHT BULBS IAW AMM 32-60-00. OPS CHECK GOOD.SDR JGVR20171201004Drag Angle · corrodedREPAIRED CORROSION FOUND UNDER THE LH WING FORWARD AND AFT DRAG ANGLES PER CESSNA REPAIR DEFINITION S-750-0190/17RD. REPAIRED CORROSION FOUND UNDER THE RH WING AFT DRAG ANGLE PER CESSNA REPAIR DEFINITION S-750-0190/17RD.
MECHANICALLY BLENDED APPROXIMATELY 40SDR JGVR20171201003Skin · corrodedREPLACED CORRODED LH INBOARD UPPER WING SKIN WITH NEW P/N 6722311-17.SDR JGVR20171201001Skin · corrodedFOUND LOWER STINGER SKIN NEAR THE APU CORRODED. REPLACED WITH NEW SKIN P/N 6712615-56.SDR JGVR20171201002Skin · corrodedREPLACED CORRODED RT INBOARD UPPER WING SKIN WITH NEW P/N 6722311-18.SDR JGVR194F1201001Skin · corrodedFOUND LOWER AFT TAILCONE SKIN AND STRINGER, NEAR THE APU, CORRODED. REPLACED PARTS WITH NEW STRINGER P/N 6712615-56 AND LOWER SKIN P/N 6712615-56.SDR DXTA2017112900001Transfer Sys · malfunctionedDURING TAXI, RECEIVED AN AMBER CAS WING TANK OVER FULL RT. WASN'T ABLE TO STOP THE FUEL FROM DUMPING FROM OVERFLOW UNTIL PULLING THE EXTERNAL CENTER TANK TEE HANDLE. AIRCRAFT WAS FUELED TO 7000LBS. PERFORMED INSPECTIONS AND OPS CHECKS OF RT SURGE TANK FLOAT SDR 9JLA2017120413650Switch · defectiveWHILE EN-ROUTE AT FL430 THE CREW RECEIVED A BAGGAGE DOOR OPEN INDICATION FOLLOWED BY A BAGGAGE DOOR SEAL AMBER CAS MESSAGE. SHORTLY THEREAFTER THE CABIN BEGAN TO DEPRESSURIZE RAPIDLY. THE CABIN OXYGEN MASKED DEPLOYED. THE CREW RAN THROUGH THEIR EMERGENCY CHECKSDR JGVR20171121003Skin · corrodedTHREE CORRODED AREAS ON THE CENTER UPPER SKIN OF THE LT PYLON. BLENDED, TREATED, FABRICATED AND INSTALLED DOUBLERS IAW EO ERO-910739, REVISION IR.
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