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 = '200' 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 = '200' 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 BKEA201608110001Landing Gear · malfunctionedDURING A ROUTINE FLIGHT SHORTLY AFTER DEPARTING AND CLIMBING THROUGH 3000 FT, NOTICED SPEED TAPE HAD TURNED RED. IMMEDIATELY LOOKED TO THE EICAS SCREEN AND SAW THAT THE
LEFT MAIN GEAR WAS INDICATING A GEAR POSITION STUCK IN TRANSIT. A RED BOX INDICATED THISSDR 9JLA2016093012098Bolt · shearedDURING A POST-FLIGHT WALK-AROUND CHECK BY MAINTENANCE MANAGER, IT WAS NOTED THAT THE LEFT LOWER SHOCK ABSORBER ATTACHMENT CROSS BOLT WAS BROKEN. THIS BOLT HAS AN 800 CYCLE LIFE LIMIT AND WAS DUE FOR REPLACEMENT IN 74 CYCLES. THE RT STRUT ATTACHMENT WAS CHECKSDR BKEA2016021600001Door · out of positionAFTER TAKEOFF, FAILED TO RECEIVE A GEAR UP INDICATION ON THE RT MAIN. WE CYCLED THE GEAR 3 TIMES WITH NO CHANGE. DUMPED FUEL AND RETURNED TO DEPARTURE, LANDING UNDER MAX WEIGHT. DISCOVERED SOME ICE IN THE AFT FLANGE OF THE GEAR DOOR THAT MAKES CONTACT WITSDR 2016FA0000217Bearing · failedA SAFRAN 23291-006, STARTER GENERATOR, SN 98021 HAD AN IN FLIGHT FAILURE OF THE ANTI-DRIVE END BEARING NECESSITATING AN ENGINE SHUTDOWN. INSPECTION REVEALED THE FAILED BEARING WAS MARKED PMA EH03-6010-19 ON THE INNER RING. THE DRIVE END WAS THE SAME PMA BEARINSDR IMJA20160215001Starter Gen · failedENROUTE, THE LT GEN FAILED, WITH PERCEPTIBLE VIBRATION. SECURED THE GEN & CONTINUED THE FLIGHT. WHILE ON APPROACH, AS POWER WAS REDUCED, THE LT ENG FAILED. DECLARED AN EMER. THE LANDING & TAXI TO THE RAMP WAS UNEVENTFUL & REQUIRED NO EMER ASSISTANCE. A CRSDR 9JLA2016092814673Actuator · defectiveAFTER TAKEOFF THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR INDICATES DOWN AND LOCKED AFTER GEAR RETRACTION. TROUBLESHOOTING DETERMINED THAT THE RT MAIN LANDING GEAR ACTUATOR WAS DEFECTIVE. THE ACTUATOR WAS REPLACED, AIRCRAFT WAS RETURNED TO SERVICE.SDR 9JLA2015120912076Clamp · brokenTHE CREW REPORTED THAT DURING THE POST FLIGHT CHECK THAT THEY FOUND THE LT MAIN BATTERY AFT HOLD DOWN CLAMP WAS BROKEN. THE BROKEN CLAMP WAS REMOVED & A NEW CLAMP WAS INSTALLED PN AN3156-3. THE ACFT WAS RETURNED TO SERVICE.SDR DXTA2015111306121Unknown · smokeUPON TAKEOFF, THE CABIN & COCKPIT FILLED WITH SMOKE. AFTER COMPLETING SEVERAL VISUAL INSP & CLEANING OF RESIDUAL OIL, RAN APU BLEED AT HIGH FLOW ON MAX HEAT FOR 15 MINS TO START DUCT BURN OUT PROCEDURE. STARTED ACFT ENGS, RAN LT ENG AT HIGH POWER WITH ECS SESDR 9JLA2015120812055Controller · failedDURING THE FINAL CLIMB TO FL360, AFTER DEPARTURE, THE ACFT AUTO PRESSURIZATION SYS DEVELOPED A FAULT & BEGAN TO SLOWLY LOSE PRESSURIZATION. CABIN ALTITUDE WAS CLIMBING AT 1000 FPM 7 REACHED 9000 FT. AT THAT POINT, THE CREW WAS ABLE MANUALLY CONTROL. SHORTLYSDR DXTA2015100506099Unknown · odorAFTER STARTING BOTH ENGS & SELECTING ECS TO BOTH, A STRONG ODOR OF JET FUEL WAS PRESENT. OPERATED BOTH ENGINES FOUR SEPARATE TIMES, NO FUEL ODOR DURING ANY EVENT. OPERATED APU BLEED AIR DURING START & NO FUEL ODOR. OPERATED BLEED AIR FROM LT & RT ENGINES & SDR DXTA2015092906095Unknown · odorFUEL ODOR IN BAGGAGE COMPARTMENT. ACCESSED BAGGAGE COMPARTMENT AND WAS NOT ABLE TO DETECT THE ODOR OF FUEL. INSPECTED AREA FOR ANY LEAKS OR EVIDENCE OF PREVIOUS LEAKS, DID NOT FIND ANY EVIDENCE IN BAGGAGE AREA. WORK PERFORMED IAW AMM 25-50-00, NO DEFECTS NSDR DXTA2015092106087Brake Sys · malfunctionedABORTED TAKEOFF. THE ABORT WAS NOT HIGH SPEED & WAS NOT AGGRESSIVE. AT A VERY SLOW SPEED WE LOST BRAKES & HAD TO USE EMER BRAKE.SDR DXTA2015091506085Circuit Board · failedELECTRICAL BURNING ODOR OBSERVED BY BOTH CREW DURING FLIGHT. COFFEE HEATERS WERE TURNED OFF & ODOR REMAINED. LT & RT GEN SHOWED 170 & 130 AMP, SPLIT RESPECTIVELY & WERE FLUCTUATING +/- 20 AMPS RAPIDLY. WHEN GALLEY & CABIN POWER WAS REMOVED AMP LOAD SEEMED SDR DXTA2015091406084Spring · wornUNCOMMANDED AUTOPILOT DISCONNECT AT FL410. AILERONS WERE STIFF UNTIL REACHING FL270. REMOVED AND REPLACED A WORN AILERON FEEL SPRING. PERFORMED SATISFACTORY OPS CHECKS WITH NO DEFECTS NOTED. WORK DONE IAW AMM 27-10-35.SDR DXTA2015090106073Apu · fireWITH BATTERY IN OVERRIDE, APU DOOR OPEN, APU NOT RUNNING, NOTICED WHITE SMOKE FOLLOWED BY FLAMES COMING OUT OF THE TAILPIPE. APU FIRE BOTTLE WAS DISCHARGED, DID NOT EXTINGUISH FLAMES. FIRE DEPARTMENT EXTINGUISH FLAMES. NO FIRE WARNING IN COCKPIT AT ANY TIMSDR BKEA20150826001O-Ring · leakingEN-ROUTE A CAS MSG APPEARED THAT READ, R HYD LEVEL LOW. FOLLOWING THE QRH, WE BEGAN TO MONITOR THE RT HYD FLUID LEVEL, WHICH AT THE TIME WAS 28. IT WAS DECIDED THAT IF THE LEVEL CONTINUED TO DROP, OR IF THE PRESS STARTED TO FLUCTUATE, TO LAND AS SOON AS POSSSDR BKEA20150819Transponder · malfunctionedJUST AFTER TAKEOFF WE RECEIVED "RT T/R INOPERATIVE" CASS MESSAGE AND ATC REPORTED THAT THEY DIDN'T HAVE OUR TRANSPONDER. WE CYCLED THROUGH OUR TRANSPONDER OPTIONS AS ATC CONTINUOUSLY ASKED WHERE AND AT WHAT ALTITUDE WE WERE. DURING THE 31 MINUTE FLIGHT WE INSDR W6JA20150723004Warning System · false activationDURING CRUISE AT FL 350, EICAS DISPLAYED RT BLEED AIR LEA. FOLLOWED QRH STEP BY STEP BUT EICAS MSG REMAINED ILLUMINATED. QRH DIRECTED CREW TO SHUTDOWN RT NR 2 ENG & LAND AS SOON AS POSSIBLE. CREW & PAX OBSERVED AN UNUSUAL BURNING OIL SMELL. CREW THEN DECLASDR 9JLA2015081414658Limiter · failedDURING DESCENT & APPROACH TO LANDING THE CREW SELECTED SLAT & FLAPS WITH NO CHANGE OR MOVEMENT. THE CREW WAS REQUIRED TO SELECT BYPASS TO ACHIEVE FLAP MOVEMENT. AFTER LANDING THEY WERE UNABLE TO DUPLICATE THE FAULT. TROUBLE SHOT & FOUND INTERMITTENT RT SLATSDR W6JA20150512002Reservoir · lowAFTER TAKEOFF, RT HYD PRESS LOW LIGHT CAME ON DURING GEAR RETRACTION ACCOMPANIED WITH LOW HYD QTY. HYD PRESS FLUCTUATED BETWEEN 0 - 2950. RT HYD RESERVOIR WAS SERVICED, NO LEAKS NOTED.SDR W6JA20150428001Warning System · false activationUPON TAKEOFF, IMMEDIATELY AFTER THE GEAR WAS RETRACTED, AN EICAS MSG CAUTION LIGHT FOR, MAIN CABIN DOOR, CAME ON. PILOT COMMUNICATED TO TOWER TO RETURN WITHOUT DECLARING EMER. WHEN TRANSFERRED TO APPROACH, PILOT DECLARED EMER & WAS GIVEN PRIORITY TO 25R & LASDR 9JLA201504038653Pressure Switch · defectiveDURING LANDING THE RT THRUST REVERSER ARM LIGHT TESTS, BUT DOES NOT ILLUMINATE WHEN THE THRUST REVERSER SYS WAS ARMED. THRUST REVERSER OPERATION WAS REPORTED TO BE NORMAL. TROUBLESHOOTING FOUND THE RT THRUST REVERSER PRESS SWITCH TO BE DEFECTIVE, PN 6607-7-7SDR DXTA2015031005991Limiter · malfunctionedSLAT FLAP MX, WHITE EICAS MESSAGE ILLUMINATED WHEN FLAP HANDLE MOVED. SLAT JAMBED BITE LIGHT MESSAGE ON LAV PANEL. TROUBLESHOT SLAT SYS & FOUND LT TORQUE LIMITER BRAKE FAILED. REPLACED TORQUE LIMITER PN 1258AOOOO-02 SN 0056, WITH REPAIRED TORQUE LIMITER PN SDR 9JLA201504038128Control Unit · failedDURING FLIGHT AT FLT LEVEL 360 THEY RECEIVED AN APU BLEED AIR LEAK WARNING. NOTE, APU WAS NOT OPERATING. TROUBLESHOOTING DISCOVERED THAT THE APU BLEED AIR LEAK DETECTION CONTROL UNIT PN 35009-20 WAS DEFECTIVE. A NEW UNIT WAS INSTALLED. OPERATIONS CHECKED OSDR O2GA2015021621201Wire · chafedAT CRUISE FL370 45 MINUTES AFTER DEPARTURE, EICAS INDICATIONS SLAT MOVED INTERMITTENTLY BETWEEN 0* & 2*. CAS MSG, SLAT & FLAP MAINTENANCE. ON ARRIVAL FOR LANDING, SLATS & KRUEGERS DID NOT EXTEND. LANDING WAS PERFORMED WITH 20 DEGREES FLAPS IAW CHECKLIST. LSDR DXTA2015021705981Spring · failedAILERONS COMPLETELY FROZEN IN FLIGHT. DISCONNECTED AUTOPILOT, NO ROLL CONTROL. DESCENDED TO FL310 TO REGAIN CONTROL & ROLL BEGAN TO IMPROVE. REGAINED FULL CONTROL AT FL250. REMOVED AFU & INSTALLED A NEW UNIT. OPS CHECKED GOOD WITH NO DEFECTS NOTED IAW AMMSDR DXTA2015012605970Unknown · odorDURING FLIGHT, STRONG ELECTRICAL BURNING ODOR WAS PRESENT IN COCKPIT. NO OTHER INDICATIONS WERE SEEN. TURNED OFF GALLEY & CABIN, THE ODOR SEEMED TO REDUCE. ODOR SEEMED STRONGEST BEHIND COPILOT. R & R CIRCUIT CARD 82P. PERFORMED OPS CHECKS OF ANNUNCIATOSDR DXTA2014120805941Battery · overheatedDURING FLIGHT THE EMERGENCY BATTERY OVERHEAT EICAS ILLUMINATED. REPLACED THE EMERGENCY BATTERY. PERFORMED OPS CHECKS WITH NO DEFECTS NOTED. ACCOMPLISHED IAW AMM 24-30-20.SDR CWQA20141112001Unknown · leakingDURING CLIMB, CREW WAS INFORMED OF SMOKE IN CABIN. CHECK LIST FOLLOWED & UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. ON DESCENT & APPROACH SMOKE SUBSIDED. MX EVALUATION FOUND ENG OIL CONTAMINATION IN BLEED AIR SYS & IDENTIFIED COMING FROM LT ENG LP BLEESDR 9JLA2015012807410Actuator · failedCREW REPORTED THAT THE EMER AILERON TRIM FAILED DURING PREFLIGHT CHECKS. TROUBLE SHOT & FOUND THE EMER AILERON TRIM ACTUATOR FAULTY. THE DEFECTIVE ACTUATOR PN 021127-01, SN 534 WAS REMOVED & AN OVERHAULED UNIT WAS INSTALLED. OPERATIONS CHECKED SATISFACTORY.SDR DXTA2014100605906Engine · leakingDURING LANDING & FLIGHT IDLE HAD AN ODOR IN THE COCKPIT. TOWER ADVISED THE RT ENGINE WAS SMOKING. THE SMOKE DISSIPATED INSIDE & WAS NO LONGER VISIBLE TO THE TOWER. REPLACED THE RT ENGINE DUE TO INTERNAL OIL LEAK & SMOKE IN THE CABIN. PERFORMED SATISFACTOSDR DXTA2014092505895Engine · odorRETURNED TO FIELD DUE TO SMOKE SMELL IN THE CABIN ON TAKEOFF. REMOVED LT ENGINE& REPLACED WITH SERVICEABLE ENG SN PCE-CC0246. PERFORMED LEAK & OPERATIONAL CHECKS OF ALL WORK PERFORMED WITH NO DEFECTS NOTED. COMPLETED 5 POINT CALIBRATION RUNS WITH SATISFACTOSDR DXTA2014092205889Fitting · looseAFTER LANDING HEAVY SMOKE FROM BOTH MLG BRAKES. LANDING ROLL OUT WAS APPROX 6000FT FROM 100KTS TO TAXI SPEED BRAKES SEEMED TO FADE REQUIRING MORE PEDAL PRESSURE TO MAINTAIN CONSISTENT BRAKING. DURING BRAKE BLEEDS AND OP CHECKS, FOUND FLUID LEAKING FROM LOWERSDR DXTA2014090805875Brake Sys · contaminatedDURING ACFT MOVEMENT WITH BRAKES INITIALLY APPLIED A GROANING SOUND CAN BE HEARD UNDER COCKPIT FLOOR. WITH PARK BRAKE SET A THUMPING SOUND CAN BE HEARD BELOW PEDESTAL. EXCESSIVE BRAKE PRESS SEEMS TO BE REQUIRED TO RECEIVE NORMAL BRAKING ACTION AT TAXI SPEED.SDR 9JLA201409108120Adc · faultyA DUAL FADC ALT AS MACH FAILURE IN FLIGHT. THEY WERE ABLE TO WORK WITH GULFSTREAM SUPPORT & GET THE SYS RESET. TROUBLESHOOTING INDICATED THE THE CODES WERE POINTING TO A FAILURE OF THE NR 2 AIR DATA COMPUTER. THE DEFECTIVE COMPUTER WAS REMOVED PN 822-0374-45SDR DXTA2014090405872Apu · unserviceableAFTER APU ON SPEED FOR OVER 2 MINUTES, TURNED ON ECS TO APU. BLUISH-GRAY SMOKE BOILED OUT OF THE COCKPIT AIR VENTS, HEAVIER OUT OF THE COPILOTS SIDE. NO SMOKE NOTED IN CABIN. REMOVED APU PN 3800710-1 SN P-187 IAW CMP 490001. INSTALLED ON NEW APU IAW MM 49-SDR 9JLA201409108117Boot · leakingFOR SEVERAL MONTHS THE CREW DESCRIBED AN INTERMITTENT IN FLIGHT VIBRATION, STARTING TYPICALLY WHILE CLIMBING THROUGH 12K'-13K'. THE VIBRATION WOULD CONTINUE WHILE AT ALTITUDE & STOP ONCE BELOW 10K'. ENG SPEED THRUST LEVER POSITION DID NOT INFLUENCE THE VIBRASDR DXTA2014081805858Unknown · malfunctionedON TAXI BRAKES WHERE STIFF WITH REDUCED EFFECTIVENESS. RT SIDE PEDALS SEEMED BETTER THAN PILOTS SIDE. PERFORMED THE NORMAL BRAKE FUNCTIONAL TEST IAW MM 32-40-00, TEST PASSED. BLED BRAKES & VERIFIED HYD FLUID LEVEL GOOD. WORK PERFORMED IAW MM 32-40-20, TAXISDR CWQA20140813001Relay · stickingDURING CRUISE CREW EXPERIENCED SMOKE COMING FROM BETWEEN GLARE SHIELD & CAPTAINS WINDOW. CHECK LIST FOLLOWED, EMER DECLARED & UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. CREW REPORTED SMOKE STOPPED AFTER TURNING OFF LT WINDSHIELD HEAT. EVALUATION FOUND SDR DXTA2014080605843Unknown · odorDURING FLIGHT AT FL400 ALL COCKPIT WINDOWS FOGGED UP VERY QUICKLY WITHIN A 10 - 15 SECONDS THIS WAS ACCOMPANIED BY A STRONG ACRID BURNING SMELL. WE PUSHED THE DEFOG BUTTON FOR A FEW SECONDS & SWITCHED FROM LOW TO HIGH ON THE WINDSHIELD HEAT. WITHIN A FEW MINSDR DXTA2014072405830Brake Sys · unknownLOSS OF BRAKING DURING LANDING ROLLOUT. PERFORMED NORMAL BRAKE SYSTEM OPS FROM EACH POSITION AND BOTH TOGETHER, BRAKE SYSTEM FUNCTIONED NORMALLY IAW AMM 32-40-20.SDR 9JLA201407298102Pump · defectiveCREW REPORTED THAT THE LT STAND-BY PUMP WAS MAKING A GRINDING NOISE AFTER PARKING WITH & WITHOUT ENG RUNNING. THE LT STAND-BY PUMP WAS REPLACED WITH AN OVERHAULED UNIT 34.7 HRS TT PREVIOUSLY. THE DEFECTIVE PUMP SN 1BA3 WAS REMOVED FROM SERVICE & A INSPECTED SDR CA140619015Oil System · low pressure(CAN) DURING FLIGHT AT FL350, THE OIL PRESSURE PEAKED TO 188 PSI. REDUCTION OF POWER TO IDLE MADE THE OIL PRESSURE DROP TO 166 PSI THEN INTO NORMAL RANGE AFTER 10 MIN. THE FLIGHT WAS DIVERTED AND THE AIRCRAFT LANDED SAFELY. TROUBLESHOOTING IS ON-GOING.SDR 9JLA2014061006438Shutoff Valve · failedTHE CREW REPORTED THAT DURING PREFLIGHT CHECKS IT WAS DISCOVERED THAT THE LT ENG FIRE SHUTOFF VLV NOT INDICATING CLOSED. THE DEFECTIVE VLV SN 001273 WAS REMOVED FROM SERVICE & AN OVERHAULED UNIT WAS INSTALLED. LEAK & FUNCTIONAL CHECKS WERE SATISFACTORY.SDR 9JLA201405218101Pump · defectiveTHE CREW REPORTED THAT THE LT STANDBY FUEL PUMP WAS MAKING A GRINDING NOISE WHILE SWITCH WAS IN THE AUTO POSITION. EXAMINATION FOUND THAT THE LT STANDBY BOOST PUMP PN 2C40-5, SN 1AV2 WAS DEFECTIVE & WAS REPLACED WITH AN OVERHAULED UNIT. FUNCTIONAL & LEAK CHESDR DXTA2014042505744Control Column · chafedLEFT PILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. RIGHT COPILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. REMOVED CHAFFED PILOT CONTROL COLUMN P/N 4AS5320110-501, NSN AND PERFORMED MINOR REPAIR BY SDR DXTA2014042505743Control Column · chafedLEFT AND RIGHT CONTROL COLUMNS CHAFED FROM THE AILERON CABLES INSIDE COLUMNS. REMOVED CONTROL COLUMNS, REWORKED IAW EO4AS5320110-502A02. REINSTALLED CONTROL COLUMNS IAW AMM 27-10-06 AND EO4AS5320110-502A02.SDR DXTA2014042505742Control Column · chafedLEFT PILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. REMOVED PILOT'S CONTROL COLUMN. MACHINED AND BLENDED DAMAGED AREA. ALODINED AND PRIMED AS REQUIRED. RE-INSTALLED PILOT'S CONTROL COLUMN. PERFORMED ALL FLIGHT CONTROL TRAVEL TSDR DXTA2014041705735Proximity Switch · frozenRT MLG FAILED TO RETRACT. GEAR SELECTED DOWN, GEAR LEFT IN DOWN POSITION AN ADDITIONAL 5 MINUTES. GEAR SELECTED UP SECOND TIME WITH BOTH LT & RT MLG FAILING TO RETRACT. SUSPECT FALSE INDICATION DUE TO ICE BUILD UP ON LANDING GEAR PROX SWITCHES. JACKED ACFT SDR DXTA2014041405728Uplock Switch · inoperativeRIGHT MAIN GEAR WOULD NOT INDICATE UP. COMPLIED WITH QRH PROCEDURES. R & R RT MLG NR 2 UPLOCK SWITCH IN THE AFT POSITION IAW AMM 32-10-11. PERFORMED EXTENSION & RETRACTION FUNCTIONAL TESTS IAW AMM 32-30-00. OPS CHECKED GOOD.
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