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 E0YA201608090001Hose · leakingAFTER INITIAL CLIMB OUT, THE CREW NOTED A STEADY DEPLETION OF THE "A" HYDRAULIC SYSTEM. AFTER ASCERTAINING THE FLIGHT COULD CONTINUE SAFELY, THE CONTINUED ON AND LANDED. THE AIRCRAFT WAS SHUT DOWN ON THE RUNWAY AND TOWED TO THE HANGAR DUE TO NO BRAKES AVAILABSDR AWKA201607060001Controller · failedWHILE ON DEPARTURE AND DURING CLIMB, CREW RECEIVED A FLAPS FAIL CAS MESSAGE. CREW CONTINUED THE CLIMB, AND ONCE AT A SAFE ALTITUDE, PERFORMED THE CORRESPONDING CHECKLIST, BUT WAS UNABLE TO CLEAR THE MESSAGE. FLIGHT CONTINUED TO DESTINATION WHERE THE CREW ELESDR CVGA2016062200144Seal · contaminatedENROUTE, JUST PRIOR TO NUCAR INTERSECTION, BAGGAGE DOOR SEAL, CAS MESSAGE ILLUMINATED, FOLLOWED BY CABIN ALTITUDE, CAS MESSAGE SHORTLY THEREAFTER. RAN BOTH ABNORMAL PROCEDURES AND INITIATED AN EMERGENCY DECENT. DECLARED AN EMERGENCY WITH ATC. WE MADE THE DESDR DXTA2016061406258Downlock Switch · unserviceableWHEN LANDING GEAR WAS EXTENDED WE GOT 3 GREEN AND 1 RED UNLOCKED LIGHT. AURAL WARNINGS CAME ON WHEN FLAPS FULLY EXTENDED AND WHEN TLA WAS BROUGHT TO IDLE. REMOVED RT MAIN LANDING GEAR DOWN LOCK SWITCH P/N 6-0407-1. INSTALLED AND RIGGED NEW DOWN LOCK SWITCH SDR AWKA2016061500610Controller · failedWHILE LEVELING OFF AT FL410, THE FLIGHT CREW RECEIVED AN AMBER, CABIN ALTITUDE, CAS MESSAGE. THE CREW DONNED THEIR O2 MASKS AND REQUESTED FL380; AT THIS ALTITUDE IT WAS NOTED THAT THE CABIN PRESSURE WAS NOT STABILIZING, SO AN EMERGENCY DESCENT WAS INITIATED. SDR DXTA2016060506250Float Valve · defectiveWING TANK O'FULL R CAS MSG CLIMBING THROUGH 37000' 270 KIAS WITH 30LBS FUEL IN CENTER TANK & APPROX 3100 LBS IN EACH WING TANK. VISUALLY OBSERVED FUEL VENTING. LOST 200 LBS IN 2 MINUTES. DE-FUELED ACFT, DOWN TO BE ABLE TO REMOVE OTBD WING ACCESS PANEL. REMSDR DXTA2016060306252Bracket · damagedDAMAGE FOUND IN TAILSTAND AREA WHILE INSTALLING TAIL STAND PRIOR TO MAINTENANCE. NO RECORD OF DAMAGE FOUND. REMOVED TAIL STAND BRACKET, PN 6712405-10 IAW SRM 51-40-03. IAW ENGINEERING REQUEST, RECONTOURED CREASED AREA AND BLENDED SHARP EDGES. STARTED FITTINGSDR DXTA2016052006244Coalescer Bag · odorON TAXI IN WE COULD SMELL SMOKE, TURNED PACS OFF. ON LATER TESTING IT SEEMS TO HAPPEN WHEN WE TURN THE COCKPIT PAC ON. RAN BOTH PACS WITH THE APU FOR ABOUT 3 HOURS IN ALL MODES AND CONFIGURATIONS WITH NO SMOKE OR ABNORMAL SMELLS. OPERATED BOTH PACS. WITH EACSDR DXTA2016052006243Apu · defectiveON GND, APU ONLY, ACFT FILLED WITH SMOKE. REMOVED DEFECTIVE APU & INSTALLED A REPAIRED CUSTOMER SUPPLIED APU. COMPLIED WITH APU OPERATIONAL CHECKS & LEAK CHECKS WITH GOOD RESULTS. ALL WORK DONE IAW MM 49-10-00 & MM 49-20-00. NO OTHER DEFECTS NOTED & PROGRASDR EBV220160525001Bearing · crackedDURING REMOVAL OF THE RT MLG TRUNNION, THE AFT SPHERICAL BEARING FELL OUT OF THE BORE IN THE AFT WING SPAR. THE BEARING INNER RACE IS CRACKED IN TWO PLACES ALONG THE BORE AXIS & A PIECE OF THE INNER RACE FELL OUT.SDR AWKA20160513001Outflow Valve · failedAMBER, CABIN ALTITUDE, CAS MESSAGE WAS REPORTED ON A SUBSEQUENT FLIGHT. MAINTENANCE TECHS TROUBLESHOT THE SYSTEM AND FOUND A FAULTY PRIMARY OUTFLOW VALVE. THE VALVE, PN 103678-3, WAS REPLACED WITH AN O/H UNIT. LEAK AND OPS CHECKS WERE NORMAL AND THE ACFT WASSDR DXTA2016050406233Elevator · damagedIN DESCENT AT 15000 FT, ACFT SUFFERED A LT SIDE LIGHTNING STRIKE. BURN MARKS AT VARIOUS RIVETS ALONG FUSELAGE. LT SIDE HORIZONTAL STAB IS MISSING OTBD STATIC WICK. BURN & EXIT MARKS AT PORT SIDE OF HORIZONTAL STAB. COMPLIED WITH LIGHTNING STRIKE INSPECTIONSDR CWQR20160502014Tube · leakingDURING A SCHEDULED MX, WHEN PERFORMING POST INSPECTION ENG RUNS, FOUND LT ENG BLEED AIR TUBE ASSEMBLY LEAKING AT THE BELLOWS & SMALL AREA OF DISCOLORATION, BUT NO DAMAGE TO COWLING & ADJACENT AREAS.SDR DXTA2016042206229Apu · leakingSTRONG OIL SMELL FROM OVERHEAD WEMACS, SEEMED STRONGER IN COCKPIT. NOTICED PRIOR TO DESCENT FROM ALTITUDE. EVIDENCE OF OIL IN CABIN APU COMPRESSOR. REPLACED APU ASSEMBLY IAW MM CH 45-10-00. OPERATIONAL & LEAK CHECKED GOOD. INSTALLED 11, 647 HAS, 11, 595 CSDR DXTA2016042606229Unknown · odorSTRONG OIL SMELL FROM OVERHEAD WEMACS. SEEMED STRONGER IN COCKPIT. NOTICED PRIOR TO DESCENT FROM ALTITUDE.SDR DXTA2016042206228Skin · corrodedCORROSION WAS FOUND ON THE EDGE OF THE PANEL LAND AT PANEL 642AB ON THE PN 6722146-2, RT WING LOWER SKIN. CWS 268.05-288.4. ACCOMPLISHED CORROSION REMOVAL ON RT PANEL 40 642AB IAW SRM 57-20-01. ACCOMPLISHED ET NDI OF AREA IAW NDTM PART 6-57-20-01, AFTER CORRSDR AWKA7190415Control Handle · failedTHE FLIGHT CREW REPORTED THEY FOLLOWED THE BEFORE LANDING CHECKLIST & CONFIRMED ALL INDICATIONS OF LG DOWN & LOCKED. THE MAIN GEAR TOUCHED DOWN, SPEED BRAKES WERE DEPLOYED & THE NOSE GEAR CONTACTED THE RUNWAY. THE NOSE CONTINUED LOWERING TO THE RUNWAY SURFACSDR DXTA2016040806229Firewall · crackedAPU FIREWALL CRACKED UNDER LT UPPER TRUSS MOUNT ATA 51. REPAIRED IAW REPAIR DEFINITION S-750-0156 23PRD & SRM 51-40-03. DOUBLER & 6712625-15-2 FILLER WAS FABRICATED. MATCH DRILL 1 DOUBLER & 2 FILLER IAW DWG 6712625 & PRELIMINARY REPORT S-750-0156 23PRD. INSDR AWKA20160525001Bearing · out of positionDURING CRUISE AT FL340, THE FLIGHT CREW EXPERIENCED A LOUD BANG WHICH WAS FOLLOWED UP WITH THE RED GEAR UNLOCK LIGHT ILLUMINATING. FLIGHT CREW CONSULTING WITH MX CONTROL, ELECTED TO DIVERT WHERE THEY LANDED UNEVENTFULLY. WHILE TROUBLESHOOTING, FOUND THE NLG SDR DXTA2016032306214Skin · corrodedCORROSION WAS FOUND UP TO 0.003 INCHES DEEP ON THE SKIN, PN 6711032-9, OF THE LOWER SKIN BOND ASSEMBLY, PN 6711030-4, ALONG THE FWD PRESS BULKHEAD PLANE AT LBL 17.5. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WAS MAPPED USING ULTRASDR DXTA2016032306213Skin · corrodedCORROSION WAS FOUND ON THE 6711070-2 RT AFT CABIN SKIN UNDER THE TCAS ANTENNA AT FS 205.00, RBL 4.17. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WERE MAPPED USING ULTRASOUND. THE MINIMUM REMAINING THICKNESS WAS 0.025 INCHES. THE SDR DXTA2016032306212Skin · corrodedCORROSION WAS FOUND UP TO 0.012 INCH DEEP ON THE LT SKIN, PN 6711032-21, OF THE LT SKIN BOND ASSEMBLY, PN 6711033-3, AT FS 187 ABOVE STRINGER 12L. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WAS MAPPED USING ULTRASOUND.SDR DXTA2016032306211Tail Cone · corrodedCORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE TAIL CONE. ALL CORROSION WAS REMOVED BY BLENDING. THE REMAINING THICKNESSES WERE MAPPED AT EACH SITE USING ULTRASOUND. ACCOMPLISHED REPAIR DEFINITION S-750-0055 25RD, MAJOR REPAIR, REPAIR OF BAGGAGE DOOR & TAISDR DXTA2016032306210Skin · corrodedCORROSION WAS FOUND AT FOUR LOCATIONS ON THE TAIL CONE UPPER SKIN, AROUND THE PERIPHERY OF THE DORSAL FAIRING. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESSES WERE MAPPED AT EACH SITE USING ULTRASOUND. ACCOMPLISHED REPAIR DEFINITION SDR DXTA2016032306209Skin · corrodedSEVERAL CORROSION SITES WERE FOUND ON THE FUSELAGE SKINS. PRESS VESSEL SKIN IS CORRODED AT THE FOLLOWING ATA 53 LOCATIONS ALONG THE UPPER SURFACE, FS 527 3 SPOTS, FS 413 1 SPOT, FS 388 3 SPOTS, FS 362 1 SPOT, FS 370 1 SPOT, FS 327, FS 316, FS313, FS 298, FS 2SDR DXTA2016032306207Unknown · smokeVISIBLE SMOKE & SMELL OF BURNING RUBBER IN CABIN ON GND. VISUALLY CHECKED OIL LEVEL OF APU WITH NO DEFECTS NOTED. CHECKED COALESCER SOCKS OIL. OPERATED APU, BOTH COCKPIT & CABIN PACS, NO SMOKE SMELL NOTED. HEAVY CONDENSATION SMOKE FROM ALL EYELETS. OPERATESDR DXTA2016030706204Coalescer Bag · odorSTRONG ODOR WAS SMELLED AFTER TAKEOFF. TURNED OFF CABIN PACK & ODOR WENT AWAY. VERIFIED ODOR WAS COMING FROM CABIN PACK WHEN WE TURNED IT BACK ON PRIOR TO LANDING. RAN THE APU AND VERIFIED A DISTINCT ODOR COMING FROM THE CABIN PAC. RAN THE RT ENG WITH THE SDR AWKA20160310001Warning System · false activationWHILE ON DEPARTURE, & CLIMBING THROUGH 5000’, THE FLIGHT CREW RECEIVED A RED, RT PYLON BLEED LEAK, CAS MSG. THE CREW RAN THE CHECKLIST & DECLARED AN EMER. THE DECISION WAS MADE TO DIVERT, WHERE THEY LANDED WITHOUT INCIDENT. NO BLEED AIR LEAKS WERE FOUND DURSDR CWQR20160226008Bulkhead · crackedDURING THE DISASSEMBLY OF THE ENG INLET ASSEMBLY WE FOUND THIS BULKHEAD CRACKED IN NUMEROUS PLACES AT THE INLET LIP TO THROAT ATTACH FASTENERS. SUBMITTED DEFECT TO MFG UNDER SCR REPORT 746597.SDR CWQR20160226009Channel · crackedDURING THE DISASSEMBLY OF THE ENG INLET ASSEMBLY, WE FOUND THIS CHANNEL CRACKED IN NUMEROUS PLACES AT THE INLET LIP TO BULKHEAD ATTACH FASTENERS. SUBMITTED DEFECT TO MFG UNDER SCR REPORT 746605.SDR AWKA20160219001Reservoir · failedWHILE ON CLIMB OUT, THE FLIGHT CREW NOTICED A LOSS OF THE A SYS HYD QTY, THE CREW DECLARED AN EMER & THEY RETURNED BACK. FLIGHT CREW EXECUTED THE APPROPRIATE CHECKLISTS & BURNED OFF ENOUGH FUEL TO MEET THE LANDING WEIGHT. WHEN THEY LANDED THE A SYS HYD QTY WSDR DJFA20160211001Light · inoperativeDURING AN APPROACH, EXTENDED GEAR & DID NOT GET THE LOCKED SAGE LIGHT. CREW FOLLOWED THE EMER CHECKLIST & USED THE EMER EXTEND TO ENSURE THE GEAR WAS DOWN & LOCKED FOR LANDING. ACFT SAFELY LANDED WITH NO FURTHER ISSUE. FOUND FAILED LAMPS ON THE RT GEAR DOWNSDR DXTA2016020306180Blade · damagedNUMBER 2 ENG HAS 5 BLADES DAMAGED & BENT. ACCOMPLISHED FAN BLADE INSPECTION IAW MM 72-21-15-200-801. R & R 5 FAN BLADES IAW MM 72-21-15-000-801 & 82-21-15-400-801. INSTALLED BLADE ASSEMBLY, PN 23060567, SN VWB1323. INSTALLED BLADE ASSEMBLY, PN 23089650, SN SDR DXTA2016020306177Warning System · activated40 MINS AFTER TAKEOFF GEAR UNLOCK LIGHT APPEARED, ACCOMPANIED BY AN AUDIBLE THUMP. JACKED ACFT, CYCLED GEAR & VERIFIED DISCREPANCY. CHECKED OPERATION OF ALL UPLOCK ASSEMBLIES & FOUND THE NOSE OUT OF TOLERANCE. ADJUSTED NOSE UPLOCK SWITCH & CYCLED GEAR SEVERSDR DXTA2016020206176Blade · bentON PREFLIGHT FOUND 4 BLADES ON PRIMARY FAN ARE BENT ON NR 1 ENG. ACCOMPLISHED FAN BLADE INSPECTION IAW MM 72-21-15-200-801. R & R 6 FAN BLADES IAW MM 72-21-15-000-801 & 72-21-15-400-801. REMOVED PN 23060567, SN VWB1309, INSTALLED BLADE ASSEMBLY PN 23089650,SDR DXTA2016012406173Unknown · odorAT 40000 FT STRONG BURNING ODOR COMING FROM COCKPIT & CABIN. ODOR DISSIPATED ON ITS OWN AFTER APPROX 5 MINUTES. NO EICAS MESSAGES, PACK SUPPLY TEMPS BOTH AROUND 120. CHECKED APU OIL & SYS IS FULL. STARTED APU & TURNED ON BLEED AIR. OPENED ALL VENTS IN COCSDR AWKA7500127Bearing · corrodedDURING CLIMB OUT, THE FLIGHT CREW NOTED AT SEVERAL ALTITUDE CHANGES. WHILE PULLING THE CONTROL YOKE BACK TO CLIMB & ALSO MOVING THE YOKE FWD TO CAPTURE THE ASSIGNED ALTITUDE THAT THERE WAS CONSIDERABLE ROUGHNESS FELT IN THE CONTROL YOKE. ALSO, THEY OBSERVED SDR DXTA2016012306167Circuit Breaker · failedPRIMARY STAB FAILED AT 23000 FEET WITH ASSOCIATED CAS MESSAGES. PRIMARY TRIM POWER CIRCUIT BREAKER TRIPPED WITH A FAINT BURNING ODOR. R & R THE PRIMARY STAB TRIM CIRCUIT BREAKER . OPS CHECKED GOOD. WORK DONE IAW MM 24-52-00 & 750 WIRE DIAGRAM MANUAL 27-40SDR DXTA2016011806165Cdu · failedIN FLIGHT THE NR 1 FMS SCREEN FAILED, FOLLOWED BY THE AMBER LATERAL MODE OFF CAS MESSAGE. FOR THE NEXT FEW MINUTES THERE WAS A MUSTY ODOR IN THE COCKPIT THAT DISSIPATED. REMOVED AND REPLACED THE CDU . PERFORMED A SATISFACTORY OPERATIONS CHECK. WORK DONE LASDR DXTA2015123006147Unknown · smokeON THE GND WITH APU RUNNING FOR ABOUT 5 MINUTES, TAIL CONE BLD LEAK AMBER CAS MSG CAME ON. WITHIN 30 SECONDS COCKPIT & CABIN FILLED WITH SMOKE. INSPECTED TAIL CONE COMPARTMENT, NO SMOKE DETECTED. POWERED UP APU & RAN ENVIRONMENTAL SYS FOR 30 MINUTES, ALL INSDR DXTA2015122906146Coalescer Bag · odorA NASTY FOUL SOUR ODOR IS COMING FROM THE AIR CONDITIONING SYS. REMOVED LT & RT COALESCER SOCKS, THE SOCKS HAD A STRONG OIL ODOR. INSPECTED APU INLET & FOUND OIL IN APU INLET. REMOVED APU. INSTALLED A REPAIRED APU. APU WAS INSTALLED WITH SIX EACH NEW MOUSDR DXTA2015120306136Acm · seizedCABIN PAC CREATED SMOKE IN CABIN DUE TO CABIN TEMP RISING & NO AUTOMATIC OR MANUAL CONTROL FROM CABIN TEMP CONTROL. TROUBLE SHOT & FOUND COCKPIT ACM TURBINE DID NOT SPIN WHEN BLEED WAS SELECTED. REMOVED COCKPIT ACM, PN 9914497-1, SN 2014060019. INSTALLED A SDR DXTA2015120306134Pump · malfunctionedWHILE DESCENDING THRU 30000 FT & CROSS FEEDING RT TANK TO LT ENG, THE FUEL BOOST ON LT AMBER CAS CAME ON, TURNED THE CROSS FEED OFF. THEN THE FUEL PRESS LOW RT AMBER CAS CAME ON, TURNED ON THE BOOST PUMPS. AT THAT TIME THE RT ENG QUIT RUNNING. RAN THE ENG SSDR DJFA20151207001Bottle · failedON TAKEOFF, AS THE CREW INITIATED THE LG RETRACTION, THEY RECEIVED A HYD A LOW QTY WARNING & SUBSEQUENTLY NOTED THE HYD QTY DROPPED TO 11%. THE ACFT DIVERTED, DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. DISCOVERED THE LANDING EMER PNEUMATIC STORAGE BSDR DJFA20151126001Engine · surgesDURING CLIMB OUT, CREW REPORTED THE LT ENG SURGED & ROLLED BACK MULTIPLE TIMES. ACFT RETURNED TO THE DEPARTURE AIRPORT & LANDED SAFELY. REPLACED THE NR 2 ENG.SDR DXTA2015111306129Pump · failedDURING TAKEOFF THROUGH 3000 FEET WITH THROTTLE IN TAKE OFF, THE RT ENGINE N2 WENT TO 102 & INDICATED RED. THE FLYING PILOT FELT A POWER BUMP & THEN SLOWLY RETARDED THE RT ENG TO IDLE. THE ITT ON THE RT ENG SLOWLY SURGED BETWEEN AROUND 500 & 700 DEGREES A COUSDR DJFA20151120002Wire Harness · damagedCREW REPORTED ENG POWER ROLL BACK INTERMITTENTLY. ACFT LANDED SAFELY. REPLACED THE ENG CONTROL B WIRE HARNESS.SDR DJFA20151120001Flap System · failedENCOUNTERED A FLAP FAILURE WHEN SELECTING FLAP 10 FROM 0 ON DESCENT. PERFORMED ONE RESET WITH NO CHANGE. DECLARED AN EMER FOR PRIORITY HANDLING & LANDED WITHOUT FURTHER INCIDENT. PERFORMED TROUBLESHOOTING & FOUND FLAP CONTROL HANDLE NEEDED CLEANED. PERFORMSDR DJFA20151114001Fadec · malfunctionedDURING CLIMB, LT ENG POWER FLUCTUATED & ROLLED BACK 10 PERCENT 3 TIMES. AFTER THE THIRD ROLL BACK, FAN DAMAGE CAS MSG ILLUMINATED. ACFT LANDED SAFELY & NO ENG DAMAGE WAS NOTED. REPLACED THE LT ENGINE B SYS FADEC. SYS OPERATIONAL CHECKS WERE FOUND SATISFACTSDR DXTA2015111306123Actuator · failedNOSE GEAR DID NOT CATCH ON UNLOCK AFTER TAKEOFF. PERFORMED GEAR BUMP TROUBLESHOOTING. NLG & LT MLG ARE FUNCTIONING NORMALLY. FOUND THE RT MLG UPLOCK ACTUATOR TO BE CYCLING UNCOMMANDED, FOLLOWING THE RETRACT CYCLE CAUSING RT GEAR TO HAMMER UP & DOWN IN THE
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