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 5JHA2025030700160Overheat Sensor · false indicationTHE LH AND RH HYDRAULIC TEMP SENSORS GIVE FALSE INDICATIONS. WE HAVE REPLACED 5 SENSORS IN THE LAST FEW YEARS AND THE LATEST ONE THAT IS BRAND NEW FAILED AFTER TWO WEEKS IN SERVICE.SDR 3EJA 20250314001Regulator · failedCABIN DOOR SEAL AND CABIN DOOR CAS MESSAGE ILLUMINATED AT 2000 FT. LEVELED OFF AT 4000 AND NOTICED CABIN WAS NOT PRESSURIZING. CAS MESSAGES DID NOT ILLUMINATE UNTIL AFTER TAKEOFF. R/R CABIN DOOR SEAL PRESSURE REGULATOR.SDR 3EJA202503060001Warning Message · illuminatedCABIN DOOR SEAL AND CABIN DOOR CAS MESSAGE ILLUMINATED AT 2000 FT. LEVELED OFF AT 4000 AND NOTICED CABIN WAS NOT PRESSURIZING. CAS MESSAGES DID NOT ILLUMINATE UNTIL AFTER TAKEOFF.SDR AJXA2025030600152Landing Gear · malfunctionedAFTER TAKEOFF PILOT SELECTED THE LANDING GEAR TO THE UP POSITION AND HEARD A NOISE FROM THE NOSE WHEEL WELL. THEY LOWERED THE LANDING GEAR A THE DOWN AND LOK INDICATION LIGHT DID NOT INITIALLY COME ON. THE PILOT RETURNED TO THE AIRPORT AND JUST BEFORE LANDING SDR AJXA2025040300030Tire · wornPILOT NOTED VIBRATION IN NLG DURING TAKEOFF ROLL / BOTH NOSE WHEEL TIRE ASSEMBLIES WERE REPLACED WITH NEW TIRES. PILOTS PERFORMED HIGH SPEED TAXI WITH NO FURTHER ISSUES NOTED AT THIS TIME.SDR 3EJA20250220001Warning Message · illuminatedCABIN DOOR SEAL CAUTION ILLUMINATED CLIMBING THRU 5000 FEET.SDR 3EJA2025020613025Switch · failedEICAS POPULATED AN AMBER CODE OF “HP DUCT O’PRESS R”. T/S SYSTEM. R/R OVERPRESSURE SWITCH RH SIDE DUCT. OPS CK GOODSDR CVGA20250123006Flap System · faultedFLAPS FAIL AT 5 DEGREES. TOWER DECLARED EMERGENCY ON BEHALF OF THE CREW. VERIFIED FLAP FAIL LT WITH CODES 2+7 ON FLAP CONTROLLER. RESET BITE CODES AND CYCLED FLAPS NUMEROUS TIMES WITH NO FAULTS NOTED. PERFORMED FLAP SYSTEM ELECTRICAL RIGGING WITH NO DEFECTS NOSDR CVGA20250122005Flap System · faultedFLAPS FAIL CAS MESSAGE; FLAPS WOULD NOT RESET FLAPS DID NOT EXTEND AT ALL. TOWER DECLARED EMERGENCY ON CREWS BEHALF. RESET FLAPS REF CE750 AMM 27-50-00 PROCEDURE AND VERIFIED NO FAULT CODES ON CONTROL UNIT. OPERATED FLAPS WITH NO FAULTS FOUND. VERIFIED FLAP PDSDR 9JLA202501170001Pump · leakingLEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING.SDR CVGA20250110003Drive Unit · intermittentFLAPS FAIL MESSAGE OCCURED AFTER TAKEOFF/ENROUTE, POSTION INDICATED FALPS 0 AND SLATS NOT EXTENED. EMERGENCY DECLARED. T/S FLAPS SYSTEM. POWERED AIRCRAFT AND REVIEWED BIT CHECK ON FLAP CONTROLLER, FLAP CONTROLLER SHOWED BIT FAULT 2 (MOTOR FAULT) ANO BIT FAULT SDR CVGA20250102002Flap System · warning messageFLAPS FAILURE CAS MESSAGE, NO RESET. - DECLARED EMERGENCYSDR 6JPA202412020935Warning Message · false activationFLAPS FAIL CAS MESSAGE ENROUTE TO KDEN. FLAPS READ 0. CREW DECLARED AN EMERGENCY, AND COMPLETED FLAPS UP LANDING IN KDEN NO INCIDENT. CAS MESSAGE CLEARED, AND FLAPS CYCLED THROUGH RANGE WITH NO FURTHER DEFECT NOTED. NO ISSUE ON SUBSEQUENT FLIGHT.SDR CVGA20241126003Landing Gear · faultedNOSE LANDING GEAR FAILED TO EXTEND ON APPROACH. EMERGENCY DECLARED.SDR CVGA20241122002Relay · faultedFLAP FAIL CAS MESSAGE. OCCURRED AT FL 470, UNABLE TO RESET. WAS ABLE TO RESET ONCE AT A LOWER ALTITUDE. USED NORMAL PROCEDURE AND SELECTED FLAPS 5* SLATS EXTENDED AND FLAPS REMAINED AT ZERO. NO CAS MESSAGE AFTER A MIN FLAPS FAIL CAS MESSAGE APPEARED WITH FLAPSSDR AWKA20241118001Squat Switch · faultedAFTER TAKEOFF, THE LANDING GEAR LEVER REMAINED LOCKED IN THE DOWN POSITION. GEAR WOULD NOT RETRACT. TROUBLESHOT ISSUE TO NGL SQUAT SWITCH NOT BEING CLOSED DUE TO PARTIAL SHOCK STRUT EXTENSION. REMOVED LH AND RH NLG WHEELS, CLEANED AND SERVICED STRUT, RE-INSTSDR AWKA2024111301Handle · dirtyAPPROXIMATELY 30 MINUTES PRIOR TO LANDING RGK, THE FLIGHT CREW RECEIVED A FLAP FAIL AMBER CAS MESSAGE. THE CREW ACCOMPLISHED QRH FOR THE ISSUE AND WERE ONLY ABLE TO GET LEADING EDGE SLATS AND NO FLAPS. REQUIRED RUNWAY LENGTH PROHIBITED LANDING IN RGK SO THE CSDR CVGA20241023006Pump · failedHYD PUMP FAIL 'A' AMBER CAS MESSAGE IN FLIGHT. EMERGENCY DECLARED. RAN #1 ENGINE TO CONFIRM SQUAWK. AFTER START SEQUENCE HYD PUMP, A FAIL CAS MESSAGE APPEARED. RAN #2 ENGINE AND I GOT HYD PRESSURE ON A SIDE. SUSPECTED PUMP FAILURE. REMOVED #1 ENGINE HYD PUMP PSDR CVGA20241021004Hose · damagedUPON LANDING GEAR EXTENSION, THE "A" HYDRAULIC QUANTITY DROPPED TO ZERO. AT LANDING, WE HAD TO USE THE NITROGEN EMERGENCY BRAKES IN ORDER TO BRING THE AIRCRAFT TO A STOP. EMERGENCY DECLARED. REMOVED DAMAGED NOSE LANDING GEAR ACTUATOR EXTEND AND RETRACT HOSES ASDR 2024F00251Squat Switch · inoperativeLANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. CORRECTIVE ACTION: TROUBLESHOT LANDING GEAR SYSTEM. FOUND THE NOSE GEAR SQAUT SWITCH NOT MAKING CONTACT WITH TARGET. SERVICED NOSE LANDING GEAR STRUT AS PER MAINTENANCE MANUAL. LANDING GEAR RETRACTION CHECKS CARRISDR CVGA20241008001Tire · failedAIRCRAFT INSPECTION NEEDED FOR POSSIBLE BLOWN TIRE. POPPING NOISE SIMILAR TO BLOWN TIRE AT ROTATION. DECLARED AN EMERGENCY AT DESTINATION AIRPORT OF KSAN. INSPECTED THE TIRES, GEAR, FUSELAGE, ENGINE INLETS, A/C SYSTEM IN AFT ACCESSORY COMPARTMENT. NO DISCREPANSDR CVGA20240909001Pump · failedWHITE AT CRUISE ALTITUDE OF 43000 LOST B SIDE HYDRULIC ENGINE PUMP, DIVERTED TO ICT. EMERGENCY DECLARED. REMOVED #2 HYDRAULIC PUMP P/N: 66166 S/N: A0517P AND INSTALLED OVERHAULED HYDRAULIC PUMP P/N: 66166 S/N: LG43P IAW CE750 AMM 29-10-02. THRUST TECH ACCESSORSDR CVGA20240820003Spacer · missingAFTER TAKE OFF THE LANDING GEAR HANDLE WOULD NOT RAISE FLEW TO DENVER AND LANDED, LANDED UNDER MAX LANDING WEIGHT. REFERENCE AML 051414. INSPECTED NOSE WHEEL UPLOCK SWITCH AND TARGET. RANG OUT NOSE SQUAT SWITCH AND GROUNDS IAW CESSNA 750 WIRE DIAGRAM MANUAL CHSDR VQMA907TX081724R0Battery · failedON SATURDAY AUGUST 11TH, 2024, CESSNA CITATION 750 (X) N907TX, SN: 750-0201 RECEIVED A #2 MAIN BATTERY OVERTEMP CAS MESSAGE. THE FLIGHT CREW DIVERTED TO KATL AND DECLARED AN EMERGENCY. UPON INSPECTION, NO EVIDENCE OF OVERHEATING WAS FOUND. TECHNICIANS CHANGSDR 3EJA2024080900001Warning Message · illuminatedON TAKEOFF ROLL AMBER CAUTION MESSAGE ENG O’SPD SHUTDN L ILLUMINATED ON EICAS.SDR AWKA2024072302Control Handle · dirtyENROUTE TO KTEB DURING CONFIGURATION FOR LANDING, WHEN GOING FROM FLAPS 5 TO FLAPS 15, FLT CREW RECEIVED A FLAPS FAIL AMBER CAS MESSAGE. RAN QRH PROCEDURE & TRIED TO RESET MULTIPLE TIMES TO NO EFFECT. CREW COMPUTED APPROACH SPEEDS & LANDING DISTANCES THAT CONFSDR AWKA2024071701O-Ring · leakingAFTER ENGINE START, CREW HAD A NORMAL HYD FLUID QUANTITY OF 56%. ON CLIMB OUT AT AROUND 33,000 FT NOTICED QUANTITY AROUND 28%. AFTER A FEW MINUTES, QTY HAD SLOWLY DROPPED TO 25%. CREW DIVERTED TO CVG, RAN ALL NORMAL CHECKLISTS. ON BASE TO FINAL, CREW RECEIVESDR 3EJA9202406250001Battery · over voltageWHILE IN FLIGHT THE WE HAD BATT OVERCURRENT 1&2 EICAS.SDR AWKA202405290002Skin Panel · corrodedRESUBMIT FROM 27-MAY-24: CORROSION DAMAGE ON THE LH WING LOWER SKIN (P/N 6722172-1) AT ACCESS PANEL LAND 551EB. ***ACCOMPLISHED AEROSPACE QUALITY RESEARCH & DEVELOPMENT (AQRD) ENGINEERING REPAIR ORDER ERO-979707 REV. IR DATED 16-APR-24 "N716XJ LH WING ACCESS PSDR AWKA202405290001Skin Panel · corrodedRESUBMIT FROM 27-MAY-24: CORROSION WAS FOUND ON THE LH WING LOWER FORWARD SKIN (P/N 6722166-1) AT ACCESS PANEL 531AB AND RH WING LOWER FORWARD SKIN (P/N 6722166-2) AT ACCESS PANEL 621BB. ***ACCOMPLISHED FIELD REPAIR FR-750-0016-13486 REV. - DATED 02-APR-24 "FISDR AWKA202405277161Skin · corrodedACCOMPLISHED FR-750-0016-13486 BY REMOVAL OF THE CORRODED FUEL LANDS AT PANEL LOCATIONS 531 AB AND 621 BB. ACCOMPLISHED EDDY CURRENT PER NDTM 6-20-00-02 AND ULTRA SONIC INSPECTION PER NDTM 4-20-10-01, NO REMAINING DEFECTS. LOCATED EXTERNAL DOUBLERS: 531AB LOCASDR AWKA202405290003Control System · multiple fail(DECLARED EMER.) (DIVERTED) CREW REPORTED DURING CLIMB AS GEAR MADE THE UPLOCKS MULTIPLE CAS MESSAGES POSTED, PITCH TRIM, YAW DAMP, MACH TRIM. MESSAGES BEGAN TO EXTINGUISH, STAB. TRIM REMAINED INOP. PERFORMED AFCS FAULTS PER TECH SUPPORT, OPS CHECKS GOOD ON GSDR AWKA202405270171Warning Message · false activation(DIVERTED) (DECLARED EMER.) CREW REPORTED DURING CLIMB AS GEAR MADE THE UPLOCKS MULTIPLE CAS MESSAGES POSTED, PITCH TRIM, YAW DAMP, MACH TRIM. MESSAGES BEGAN TO EXTINGUISH, STAB. TRIM REMAINED INOP. PERFORMING AFCS FAULTS PER TECH SUPPORT. OPS CHECKS GOOD ON SDR VQMA202406070001Flex Hose · rupturedA-SIDE HYDRAULIC SYSTEM QUANTITY LOSS. FLIGHT CREW USED EMERGENCY GEAR EXTENSION TO LAND. UPON INSPECTION, TECHNICIANS FOUND RH MLG ACTUATOR HOSE RUPTURED: FOUND RH MLG ACTUATOR EXTENSION FLEX HOSE BRAIDING TO BE COMPROMISED. REMOVED BOTH LH AND RH MLG EXTENSDR VQMA920TX050724R0Safety Switch · shortedAML # M241432: REMOTE CB TRIPPED CAS MESAAGE HK005 CIRCUIT BREAKER TRIPPED. FLIGHT CREW REPORTED CB TRIPPED CAS MESSAGE FOLLOWED BY A BURNING SMELL. REMOVED AND REPLACED PASS SAFETY SWITCH PN: M8805/93-015, NSN AND TWO DIODES PN: 1N5061, NSN IAW THE CE-750 WSDR AWKA202405027351Packing · wornCREW REPORTS HYDRAULIC SYSTEM B LOSS OF HYDRAULIC FLUID IN FLIGHT. - VISUAL INSPECTED FOR LEAK AND FOUND RUDDER STANDBY MANIFOLD PLUG O-RING LEAKING. REPLACED PLUG O-RING WITH NEW P/N NAS1612-6A, CLEANED MANIFOLD PRESSURE TRANSDUCER CONNECTOR AND SERVICED WITSDR VQMA202405130002Window · crackedON THURSDAY, APRIL 11TH 2024, CESSNA CITATION 750 (X), REGISTRATION NUMBER N992TX, SERIAL NUMBER 750-0208 DIVERTED TO TPA DUE TO A LH WINDSHIELD CRACK. THE FLIGHT CREW MADE THE FOLLOWING ENTRY ON AIRCRAFT MAINTENANCE LOG (AML) FORM SERIAL NUMBER M241543: LEFSDR 674A202403200082Electrical Sys · power lossLOSS OF THE RH ELECTRICAL BUSS INFLIGHT; ON SATURDAY, MARCH 16, 2024, WE DEPARTED KDAL AT 2155Z FOR A POSITIONING FLIGHT TO KSBA. THE FLIGHT WAS NORMAL UNTIL OVER NORTHERN ARIZONA AT APPROXIMATELY 2330Z. AT THIS TIME, WE OBSERVED SEVERAL PRESSURIZATION BUMPS ASDR VQMA202405130001Window · crackedON MONDAY, MARCH 18TH 2024, CESSNA CITATION 750 (X), REGISTRATION NUMBER N478PJ, SERIAL NUMBER 750-0014 DIVERTED TO FLL DUE TO A LH SIDE WINDSHIELD SHATTERING. THE FLIGHT CREW MADE THE FOLLOWING ENTRY ON AIRCRAFT MAINTENANCE LOG (AML) FORM SERIAL NUMBER M23849SDR AWKA202405290004Door Frame · gougedRESUBMIT FROM 27-MAY-24: DURING INTERNAL ZONAL INSPECTION FOUND THE PSU SCREWS CONTACTED STRUCTURE AROUND THE E-EXIT DOOR FRAME (P/N 6711256-31). ***ACCOMPLISHED FIELD REPAIR FR-750-0250-13015 REV. A DATED 22-JAN-24 "FIELD REPAIR - GOUGE, FUSELAGE, EMERGENCYSDR AWKA2024052707501Door Frame · gougedDURING INTERNAL ZONAL INSPECTION FOUND THE PSU SCREWS CONTACTED STRUCTURE AROUND THE E-EXIT DOOR FRAME. ACCOMPLISHED FIELD REPAIR - GOUGE, FUSELAGE, EMERGENCY ESCAPE HATCH SURROUND, FS336 THROUGH FS356 (FR-750-0250-13015 REV. A).SDR AWKA202404187191Skin · corrodedREPAIRED THE RH UPPER IB WING SKIN BY R&R OF THE RH AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING) BLENDING CORRODED AREAS, PERFORMING NDT, REPLACING BLENDED FASTENERS, ROTO-PEENING BLENDED AREAS, TREATING AND PRIMING, AND REPLACING AN EXISTING SKIN PANEL WITH NEW SDR AJXA2024030100028Motor · failedPILOT REPORTED THAT THE FLAP SYSTEM HAD A FAILURE/ FLAPS WOULD NOT DEPLOY ON APPROACH. THE FLAP MOTOR FAILED.SDR AWKA202405290005Floor Skin · corrodedRESUBMIT FROM 27-MAY-24: FOUND CORRODED AREAS OF THE DROPPED AISLE FLOOR AT FS189, FS193, AND BETWEEN FS 223.35 AND FS 240.35. ***ACCOMPLISHED AEROSPACE QUALITY RESEARCH & DEVELOPMENT (AQRD) ENGINEERING REPAIR ORDER ERO-978143 REV. IR "N735XJ · DROP AISLE FUSESDR AWKA2024052707351Skin · corrodedFOUND CORRODED AREAS OF THE DROPPED AISLE FLOOR AT FS189, FS193, AND BETWEEN FS 223.35 AND FS 240.35. ACCOMPLISHED DROP AISLE FUSELAGE SKIN CORROSION, AEROSPACE QUALITY RESEARCH & DEVELOPMENT (AQRD) ENGINEERING REPAIR ORDER ERO-978143 REV. IR.SDR AWKA202404297361Gcu · faultyFOLLOW UP FROM SDR DATED 27-FEB-24: CREW REPORTED #1, 2 & 3 DISPLAY SCREENS WENT BLANK IN FLIGHT, FGC A FAIL WITH SMOKE IN THE CABIN. THE FOLLOWING CB'S POPPED DURING THE EVENT, GPWS, FADEC 1 & 2 A CHANNELS & FLAP CONTROL. REPLACED NO. 1 GENERATOR CONTROL UNITSDR 2024F00042Display · failedINITIAL REPORTING, AIRCRAFT STILL IN MAINTENANCE, CREW REPORTED #1, 2 & 3 DISPLAY SCREENS WENT BLANK IN FLIGHT, FGC A FAIL WITH SMOKE IN THE CABIN. THE FOLLOWING CB'S POPPED DURING THE EVENT, GPWS, FADEC 1 & 2 A CHANNELS.SDR 2024F00035Flap System · warning messageCREW REPORTS FLAP FAIL CAS MESSAGE POSTED. POWERED UP AIRCRAFT AND DID NOT HAVE ACTIVE FLAP FAIL CAS MESSAGE BUT FOUND MOTOR FAULT, COMMAND ERROR, GROUND FAULT, NO COMMAND, AND INTERNAL FAULT AT FLAP CONTROLLER BOX. RESET FLAP FAULTS, CYCLED FLAPS / SLATS SEVESDR 2024F00025Lockwasher · wornCREW REPORTS FLAP FAIL CAS MESSAGE WHEN FLAPS USED. WIRES TO PDU FOUND LOOSE. TERMINALS AND LUGS ON PDU CLEANED, WIRES RE-SECURED WITH NEW LOCK WASHERS. BITE 2 FAULT CLEARED FROM CONTROLLER. FLAPS CYCLES 10 TIMES FROM 0-FULL-0 WITH NO DISCREPANCIES NOTED.SDR AJXA2024011200027Proximity Sensor · out of toleranceAFTER TAKEOFF PILOT REPORTED THAT THEY RECEIVED 3 WARNINGS. 1. CABIN DOOR OPEN, 2. CABIN VENT DOOR OPEN AND A CABIN ALTITUDE WARNING. AFTER TROUBLESHOOTING FOUND THAT THE DOOR PROXIMITY SWITCH FAILED. THE SWITCH CONTROLS THE VENT DOOR WARNING AND THE CABIN DO
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