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 DJFA20151106001Valve · failedDURING CLIMB, LT ENG POWER FLUCTUATED & ROLLED BACK UP TO 10 PERCENT, THEN RECOVERED. FLUCTUATIONS CEASED UPON LEVEL OFF AT CRUISING ALTITUDE. ON LANDING NOTED MULTIPLE ERROR CODES IN THE SYS. TROUBLE SHOT THE SYS & FOUND THE CVG VLV DEFECTIVE. THE UNIT WASDR DXTA2015110606117Drive Assy · failedDESCENDING THRU 9000 MSL, 245K, ATTEMPTED TO EXTEND FLAPS TO 5 DEGREES, AT WHICH TIME EICAS INDICATED FLAPS FAIL. SLATS WERE FULLY DEPLOYED & FLAPS WERE EXTENDED LESS THAN 5 DEGREES. PER CHECKLIST, ATTEMPTED TO RESET FLAPS WITH NEGATIVE RESULTS. COMPLETED CSDR AWKA20151106001Line · leakingUPON LEVELING OFF AT CRUISE, THE FLIGHT CREW NOTED THAT THE RT ENG OIL QTY WAS SHOWING 4 QUARTS LOW AFTER 35 MINUTES, TIME TO CLIMB TO ALTITUDE. CONTINUED TO MONITOR THE OIL LEVEL WHICH WAS DROPPING ½ QT EVERY 2 - 3 MINUTES. WHEN THE OIL LEVEL REACHED 7 QTS SDR AWKA20151104001Windshield · crackedCLIMBING THROUGH 20,000 FEET, THE RT FWD SIDE WINDSHIELD SHATTERED. DECLARED AN EMER, DESCENDED TO 10,000 FEET & ELECTED TO DIVERT.SDR DJFA20151029001Coalescer Bag · dirtyA STRONG ODOR OF HOT PLASTIC ON DESCENT. RAN ENGS & OPERATED BLEED SYSTEMS WITH NO ABNORMAL ODORS NOTED. CLEANED BOTH COALESCE SOCKS & RETURNED THE ACFT TO SERVICE.SDR DXTA2015102906115Apu · malfunctionedAFTER ENGINE START AND WELL AFTER APU SHUTDOWN CABIN FILLED WITH A LIGHT FOG OF SMOKE. REMOVED APU. INSPECTED FIREWALL, MOUNTS, AND SUPPORT STRUCTURE. NO DEFECTS FOUND. INSTALLED REPAIRED APU IAW CE-750 M/M 49-10-00 AND HONEYWELL GTCP36-150CX MM 49-20-00. SDR DJFA20151021001Acm · failedAIRCRAFT LANDED & TAXIED TO THE FBO NORMALLY, AFTER ENG SHUTDOWN, WITH APU RUNNING, THE CABIN BEGAN TO FILL WITH SMOKE & CREW NOTED WARMER THAN USUAL AIR COMING FROM AIR VENTS. DURING THE FLIGHT, PAXS REPORTED & SMOKE ODOR BRIEFLY BUT NOT SMOKE OR OTHER WARNISDR 2020FA0000197Data Card · abnormalPILOTS FLIGHT PLAN ON MFD AND PFD WOULD NOT DISPLAY. FOUND DURING PREFLIGHT. HAD TO CONTACT TEXTRON FOR A PREVIOUS VERSION OF CHART AND NAV DB'S TO LOAD TO ALLOW THE NEWEST VERSION OF CHART AND NAV DATABASES. FLIGHT PLAN CHECKED GOOD POST INSTALL.SDR DXTA2015101906108Brake · failedNR 1 LT MAIN OTBD BRAKE WAS SMOKING AFTER BLOCKING IN & GRABBED WHEN PARKING. R & R NR 1 BRAKE ASSEMBLY, BLED SYS & PERFORMED OPS CHECKS. ALL OPS CHECKED GOOD AT THIS TIME ON GROUND IAW MM 32-42-01.SDR 2020FA0000196Fire Bottle · emptyDATA BASE ISSUE RELATING TO FLIGHT PLAN DISPLAY ON MFD MAP AND PFD CDI ALSO "APU FIRE BOTTLE LOW" CAS. APU WOULD NOT START. FOUND APU BOTTLE EMPTY AND NEEDING REPLACEMENT. TEXTRON TECHS REPLACED BOTTLE. CONTINUED TRIP FOLLOWING DAY.SDR JZ2R2015FA0000565Buckle · failedTHE BUCKLES ON THE LAP BELTS OF THIS AIRCRAFT BECAME DIFFICULT/IMPOSSIBLE TO LATCH. CALLED MFG AND BELT SUPPLIER AND THEY KNEW OF THE PROBLEM AND FURNISHED US WITH NEW BELT ASSEMBLIES ASAP. ACFT MFG/SUPPLIER SHOULD HAVE BEEN PRO-ACTIVE INSTEAD OF REACTIVE ONSDR DXTA2015100106098Brake Sys · unknownBRAKES ARE SPONGY. TAKES ABOUT 2 INCHES OF BRAKE TRAVEL BEFORE BRAKES CAN BE ENGAGED. INSPECTED BRAKES, PERFORMED BLEEDING PROCEDURE, TAXI ACFT. OPS & LEAK CHECKED SATISFACTORY. SERVICED HYD SYS AS REQUIRED. NO FURTHER DEFECTS NOTED IAW AMM 32-42-00 & 1SDR DXTA2015092906093Coffeemaker · odorDURING GROUND OPS, PLASTIC BURNING ODOR OBSERVED IN CABIN. APPEARS TO BE CONCENTRATED IN THE AREA OF THE OVERHEAD LIGHTING VALANCE, DIRECTLY ABOVE THE GALLEY WORK TABLE. POWERED UP ACFT, INSPECTED AREA AROUND GALLEY, INCLUDING OVERHEAD LIGHTING. FOUND BURNISDR 2020FA0000195Seal · deterioratedON LEG FROM PUW TO ESN, FUEL WOULD NOT TRANSFER FROM CENTER TANK TO WING. DIVERT TO ICT. FOUND EXCESSIVE MATERIAL IN LEFT HAND WING. REMOVED SEALER AND DEBRIS IN THE LEFT HAND WING BAYS. DETERMINED EXCESSIVE DEBRIS POSSIBLY BLOCKING FUEL EJECTOR PUMP AND TRANSSDR KKVA20150927001Unknown · smokeFAINT SMOKE ODOR & BARELY VISIBLE SMOKE NOTICED AT LOWER VENT IN CLIMB. OBSERVED INCREASING COCKPIT PACK, TURNED PACK OFF.SDR 2020FA0000194Unknown · failedPILOTS REPORTED, IN FLIGHT, GDC FAIL 2 CAS MESSAGE. NO ABNORMALITIES NOTICED. DISPATCHED MX SUPPORT FROM SERVICE CENTER. REPLACED GDC. OP CHECK GOOD. NO FURTHER ACTION REQUIRED.SDR DJFA20150922001Engine · vibrationON CLIMB OUT, CREW FELT VIBRATION IN THE LT ENG & 20 SECONDS LATER RECEIVED A LT FAN DAMAGE CAS MSG. PERFORMED THEIR CHECKLIST, DECLARED AN EMER & DIVERTED BACK SAFETY. AT THE MOMENT, WE SUSPECT A BIRD, FOD, WAS INGESTED INTO THE ENG. FOUND NO DAMAGE TO THESDR 2020FA0000193Control Unit · failedGEA FAIL 2 AMBER CAS MESSAGE IN FLIGHT AT FL430. N1S FLUCTUATED, TRIM INDICATIONS XED OUT, AIRSPEED MMO DECREASED TO M.82 POSSIBLY DUE TO MOMENTARY LOSS OF MACH TRIM. ABOVE INDICATIONS OCCURRED FOR ABOUT TWO SECONDS THEN REVERTED TO NORMAL WITHOUT REOCCURRENCESDR DXTA2015091106080Hydraulic System · leakingTHE EMER LG EXTENSION BOTTLE, EMER NOSE WHEEL STEERING & EMERGENCY BRAKE BOTTLE ARE DEPLETED. A SYS HYD FLUID IS LEAKING UNDER THE ACFT. INSPECTED A HYD SYS & DISCOVERED TRANSDUCER PACKING IN THE HYD SENSOR MANIFOLD DAMAGED & LEAKING. REPLACED HYD SENSOR MSDR DXTA2015091106079Brake · unserviceableUPON SHUTDOWN AFTER A NORMAL LANDING, THE LINE GUY TOLD US THAT HE COULD SMELL OUR BRAKES. UPON FURTHER INSPECTION, FOUND SMOKE COMING OUT OF THE INSIDE OF THE LT MAIN INBD WHEEL. SMOKE WAS VERIFIED COMING OUT BEHIND THE HEAT SHIELD BETWEEN THE MAINS. BRAKESDR DXTA2015090806076Check Valve · faultedIN FLIGHT AT 41000, THE CABIN DOOR SEAL, AMBER LIGHT CAME ON. LATER THE CABIN DOOR BEGAN TO MAKE A VERY LOUD NOISE & THEN WE BEGAN TO LOSE CABIN PRESSURE. FOUND 2 CHECK VALVES WITH UPGRADED PN 9914786-1 & IN SERVICEABLE CONDITION, THE OTHER 3 ARE PN 9914171-SDR 2020FA0000192Radio Altimeter · failedIN FLIGHT TCAS FAIL. NO INFORMATION DISPLAYED, FOLLOWED BY TCAS FAIL CAS MESSAGE. DISABLED TCAS AND CONTINUED TO SERVICE CENTER.SDR DXTA2015090306074Unknown · odorUPON RESTART OF APU, THE FADEC MSGS CAME BACK, ALONG WITH A NEW MESSAGE, TAIL CONE BLEED LEAK. WHEN SELECTED THE APU AIR, THERE WAS A STRONG BURNING ODOR IN THE COCKPIT, SHUTDOWN & INSPECTED. CHECKED APU OIL LEVEL & PERFORMED A GENERAL INSPECTION OF THE APU.SDR DXTA2015082706066Indicator · out of limitsAFTER TAKEOFF & DURING CLIMB, CONTROL COLUMN, CAPTAIN'S SIDE, HAD A DEAD SPOT IN PITCH, ALLOWING PLUS OR MINUS 3 INCHES OF COLUMN MOVEMENT, WITH NO CONTROL FEEL OR ELEVATOR MOVEMENT. CONTINUED TO LANDING. FOUND GOOD, NO DEFECTS NOTED IAW IAW MM 27-32-00. PERSDR DXTA2015081106057Warning Message · false activationREMOTE CIRCUIT BREAKER TRIPPED, CYAN CAS MESSAGE APPEARED IN CRUISE FLIGHT. INSPECTED AND FOUND NO DISCREPANCIES IAW AMM 31-50-02. NO OTHER DEFECTS NOTED.SDR DXTA2015081006054Shutoff Valve · inoperativeWHILE AT CRUISE FLIGHT, AMBER FUEL IMBALANCE EICAS MSG WAS RECEIVED. FUEL WAS 2820 LT TANK 3100 CTR 3320 RT TANK. EMER & ABNORMAL CHECKLIST WAS ACCOMPLISHED & PROBLEM BECAME WORSE. IMBALANCE REACHED 700+ POUNDS & EMER WAS DECLARED & FLIGHT DIVERTED. AT NO SDR DJFA20150729001Bungee · bindingTHE CREW REPORTED THAT AT FL 230 & CLIMBING, THE ACFT YAWED HARD NOSE LT & THEN BACK TO THE RT, WHILE AUTOPILOT WAS ON, THEN SETTLED DOWN & FLEW NORMALLY. THEY DID NOT DECLARE AN EMER & CONTINUED ONTO THEIR ORIGINAL DESTINATION, BUT DID EXPERIENCE SOME YAW INSDR DXTA2015072706050Unknown · odorWHILE SETTING UP COCKPIT FOR A FLIGHT , NOTICED A SUBTLE OIL ODOR FROM THE VENTS. ON GND APU ONLY. AFTER SEVERAL MINUTES, SMOKE APPEARED. OPERATIONAL TESTED THE ENVIRONMENTAL CONTROL SYS, BOTH THE COCKPIT & CABIN SYS. SYS OPERATIONS CHECKED NORMAL. TAN THSDR DJFA20150722001Acm · faultyWHILE IN CRUISE, THE CREW SENSED A HOT BURNING SMELL FROM THE COCKPIT PACK IN THE COCKPIT. THEY DID NOT DIVERT OR DECLARE AN EMER & LANDED AT THE DESTINATION WITHOUT FURTHER INCIDENT. INSPECTED THE ACM & DECIDED TO R & R THE COCKPIT ACM IAW AMM 21-51-00 & 75SDR DJFA20150711001Connector · dirtyWHILE IN CLIMB OUT PHASE AT FL 240, AURAL WARNING TONE SOUNDED MULTIPLE TIMES, ACFT PITCHED UP UN-COMMANDED & VERTICAL SPEED INCREASED BY 2200 FPM. CREW SWITCHED TO VS MODE & REDUCED PITCH. NO EMER DECLARED, NO FURTHER INCIDENT. CLEANED & RESEATED THE NR 1 SDR DXTA2015071306043Generator · failedAFTER NR 1 ENGINE START, A RECEIVED WINDSHIELD HEAT INOP LT CAS MESSAGE. RAMP PERSONNEL SIGNALED TO SHUTDOWN. NOTICE LARGE AMOUNTS OF SMOKE FROM ENGINE. EVIDENCE OF A FIRE CAN BE SEEN INSIDE OF COWLING. FOUND BURNS ON INSIDE OF ALTERNATOR EXHAUST ON LOWESDR AWKA20150629001Acm · failedDURING DESCENT, THE FLIGHT CREW & PAX SMELT SMOKE, THE STRONGEST WAS IN THE AFT CABIN AREA. AT THE TIME, THE CREW WAS UNCERTAIN OF THE SOURCE & AN EMER WAS DECLARED. ONCE ON THE GND & PAX DEPLANED, TROUBLESHOOTING WITH MXC & FIELD SERVICE WAS ACCOMPLISHED. SDR DXTA2015062906037Unknown · odorAPU PUTS OUT LOW DUCT PRESS ON STARTS, DOWN TO 18 PSI AT HIGHER ELEVATIONS & FLUCTUATES. RUBBER BURNING ODOR IS STRONG WHEN APU BLEED AIR IS ON IN FLIGHT & GROUND. INSPECTED APU INLET, COMBUSTOR, DIFFUSER & EXTERIOR. NO DEFECTS NOTED. INSPECTED BLEED AIR DUSDR WC73201506021988Control Cable · chafedDURING ROUTINE INSPECTION THE LT AILERON CABLE WAS FOUND CHAFED WHERE THE CABLE TRAVELS THROUGH THE INBD CLOSEOUT RIB FOR THE INBD L/E SECTION INBD OF WING BS BL54.85. THE AILERON CABLE HAD BEEN CHAFING OF THE ONBOARD EDGE OF THE WING SPAR HEAT SHIELD. A SIGSDR JZ2R2015FA0000223Tire · failedTIRE TREAD SEPARATED FROM CHORD PLIES ROUGHLY .2500 TO .3333 OF THE CIRCUMFERENCE OF THE TIRE.SDR AWKA20150428001O-Ring · damagedWHILE HOLDING SHORT OF THE RUNWAY, THE FLIGHT CREW RECEIVED THE MASTER CAUTION WARNING & A HYD VOLUME LOW A CAS MSG. THEY NOTICED THE A SIDE HYD QTY INDICATING 16 PERCENT & DECREASING AT A RATE OF APPROX 1 PERCENT EVERY 2 - 5 SECONDS. THE APPROPRIATE CHECKLISDR DXTA2015041706007Acm · failedDURING TAXI, CABIN BEGAN TO FILL UP WITH SMOKE. TURNED OFF PACS & APU, SMOKE SEEMED TO SUBSIDE. RESIDUAL SMOKE NOTICED IN TAIL CONE UPON INSPECTION. REMOVED THE FWD ACM. INSTALLED A NEW ACM IAW AMM 21-51-00. OPS & LEAK CHECKED GOOD.SDR DJFA20150331001Skin · corrodedDURING A SCHEDULED MX CHECK, AFTER REMOVAL OF THE NR 1 VHF COMM, SKIN CORRODED BEYOND MAXIMUM ACCEPTABLE LIMITS. REMOVED CORROSION & ANTENNA DOUBLER & REPLACED WITH LARGER UNIT IAW ERO-716780. ACFT WAS RETURNED TO SERVICE.SDR DXTA201503316000Acm · seizedON START UP WHEN WE POWERED UP, WE GOT SMOKE IN THE COCKPIT & CABIN. VERIFIED THAT THE CABIN ACM IS STARTING TO SEIZE AT THE PROPELLER SHAFT, COCKPIT ACM FOUND TO BE IN NORMAL OPERATION. INSPECTED FWD ACM (COCKPIT PAC) FOUND TURBINE FAN FAILURE EVIDENT, RESDR DXTA2015031805998Unknown · odorDIRTY OILY ODOR FROM CABIN & COCKPIT PACKS. R & R APU POWER PLANT IAW MM 49-10-00. R & R COALESCER SOCKS. OPS & LEAK CHECKED GOOD. WORK DONE IAW MM 49-10-00.SDR DJFA20150313001Skin · corrodedWHILE COMPLYING WITH INSPECTION, FOUND AREAS OF CORROSION AT WING SKIN BEYOND ALLOWABLE LIMITS IAW THE MANUFACTURER. ACCOMPLISHED REPAIR DEFINITION S-750-0073 09RD REPAIR OF LOWER WING SKIN CORROSION. LEAK & OPERATION CHECKS WERE GOOD & THE ACFT RETURNED TO SDR DJFA20150228001Flap · lack of lubeTHE CREW EXPERIENCED A FLAP FAIL CAS MSG AFTER TAKEOFF. THE ACFT WAS DIVERTED & THE CREW DECLARED AN EMER UPON LANDING. MAINTENANCE PERFORMED PDU CURRENT PROBE CHECK PER AMM 27-50-00 AND FLAP SYSTEM LUBRICATION PER CITATION 750 AMM 27-40-50. ALL LIMITS FOUNDSDR DXTA2015022505986Acm · unserviceableACRID SMELL NOTED DURING DESCENT. AT AUTOPILOT DISCONNECT, NO TONE AND BOTH PFDS SWITCHED UNCOMMANDED AFTER TOUCHDOWN TO SHORT RANGE CROSS SIDE INDICATION FROM FMS MODE. STARTED TROUBLE SHOOTING SYSTEM BY GAINING ACCESS TO MAINTENANCE PAGE AND CHECKING SYSTEMSDR DXTA2015022305985Generator · failedON LANDING BELOW A SPEED PF 65 KNOTS THE RT ENG FAILED, DU4, DU5, FMS2 & RM2 WENT BLANK. R&R ENGINE GENERATOR & ACCOMPLISH SB750-24-24 IAW CE-750 AMM 24-30-00 & SB 750-24-24. REMOVED 2 EA PCB CARDS (PN 6918471-6 SN 0163 & 0164 AND REPLACED W/ 2 NEW PCB CARDSSDR DXTA2015021805982Engine · leakingON BREAKING GROUND, PRIOR TO GEAR RETRACTION, FIRST OFFICER CALLED SMOKE IN COCKPIT, SMELLED ELECTRICAL. TURNED PAC'S OFF CHANGED NOTHING. APPEARED TO BE COMING FROM FIRST OFFICER`S SIDE OF COCKPIT. INSPECTED APU NO OIL NOTED. ISOLATED OIL ODOR SOURCE COMSDR AWKA20150217001O-Ring · leakingWHILE IN CRUISE FLIGHT, THE FLIGHT CREW RECEIVED AN AMBER HYD VOLUME A LOW CAS MSG. THE FLIGHT CREW ELECTED TO RETURN & AN EMER WAS DECLARED FOR PRECAUTIONARY MEASURES. MX CREWS FOUND THE LT A SYS HYD PRESS TRANSDUCER O RING TO BE LEAKING. THE O RING WAS RESDR AWKA20150205001Indicator · defectiveAFTER SELECTING LG HANDLE TO THE DOWN POSITION WHILE ON APPROACH, FLIGHT CREW DID NOT GET A GEAR DOWN, GREEN LIGHT, INDICATION ON THE RT MAIN GEAR. THE GEAR HANDLE, RED, UNLOCK LIGHT WAS NOT ILLUMINATED & THERE WAS NO GEAR HORN WITH THE THROTTLES RETARDED. FSDR AWKA20150203001A/C Pack · failedON DESCENT, THE FLIGHT CREW REPORTED THEY HAD SMOKE ACCUMULATING IN THE CABIN. THE FLIGHT CREW TURNED THE PACK OFF & THE SMOKE EVENTUALLY CLEARED. THE ACFT LANDED WITHOUT INCIDENT. THE CABIN PACK WAS DEFERRED & THE ACFT RETURNED TO SERVICE. THE PACK IS SCHSDR DXTA2015012105965Acm · failedAFTER ENGINE START WITH APU OFF, FUMES & SMOKE COULD BE SEEN & SMELLED IN THE CABIN. PERFORMED TROUBLESHOOTING IAW MM 21-52-00 & FOUND ODOR TO BE COMING FROM COCKPIT ACM. R & R THE AFT ACM TURBINE WITH A NEW AIR BEARING ACM TURBINE. PERFORMED OPERATIONAL SDR DXTA2015012005963Coalescer Bag · odorIMMEDIATELY AFTER TAKEOFF, THE COCKPIT BEGAN TO FILL WITH SMOKE. AFTER TURNING COCKPIT PACK OFF, SMOKE SEEMED TO DISSIPATE. COMPLIED WITH A LIMITED BORESCOPE INSPECTION OF THE APU IMPELLER. NO DEFECTS NOTED. COMPLIED WITH APU OPERATIONAL CHECK IAW MM 49-10-
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