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 4USA20200608001Wire · arcedFLAP/SLAT FAIL CAUTION LEADING TO SMOKE COMING FROM FLAP HANDLE. FURTHER TROUBLESHOOTING FOUND FLAP HANDLE LIGHT BEZEL WIRES ARCING AND CAUSING SMOKE TO EMANATE FROM FLAP HANDLE ASSEMBLY. LIGHT BEZEL WIRES WERE CAPPED AND STOWED AND LIGHT ASSEMBLY DEFERRED AS SDR 4USA202006080311Wire · arcedFLAP/SLAT FAIL CAUTION LEADING TO SMOKE COMING FROM FLAP SELECT HANDLE DURING TAXI UNTO RAMP. FURTHER TROUBLESHOOTING BY MAINTENANCE PERSONNEL DISCOVERED THE FLAP HANDLE LIGHT BEZEL WIRES WERE ARCING CAUSING THE SMOKE EMANATING FROM THE FLAP HANDLE.SDR 2020FA0000262Yaw Damper · odorMAY 8TH, 2020 FLIGHT FROM (APF) TO (FAR), DURING CRUSE AT FLIGHT FL400 CREW HAD A SMOKE ODOR IN THE COCKPIT. SMOKE WAS NOT ROARING BUT A LIGHT HAZE AND IRRITATING TO THE EYES. CAPTAIN DECLARED AN INFLIGHT EMERGENCY AND DIVERTED TO (STL). AFTER INSPECTING AISDR VQMA2020040800000Fuel Sys · low pressureLOW FUEL PRESS L-R AFTER ENCOUNTERING MODERATE TURBULENCE. -- MET THE CREW UPON LANDING-SAID WHEN THEY WERE IN A 40DEGREE BANK AT AN ALT 41K OVER THE ROCKY MOUNTAINS THEY ENCOUNTERED MODERATE TURBULENCE AND WHEN THEY COMPLIED WITH THE IN FLIGHT CHECKLIST PROCESDR 2020F00162Web · cracked(FIELD REPAIR) CRACK, NOSE WHEEL WELL, LH SIDEWALL WEB, NEAR F.S. 79.40 FIELD REPAIR FR-750-0195-7828 REV-SDR 2020F00104Rib · crackedBULLET FAIRING RIB CRACK. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ25104M1 DATED MARCH 12, 2020; 750-0158 (N958QS) BULLET FAIRING RIB REPAIR.SDR VQMA2020031700001Actuator · not reportedLOSS OF ALL QUANTITY AND PRESSURE A SIDE HYDRAULICS, EMERGENCY BRAKING REQUIRED, A PUMP UNLOADED, PTU BREAKER PULLED.SDR EBVR20200306001Stinger · corrodedTAIL STINGER HAD SOME CORROSION BEYOND LIMITS, COMPLIED WITH MINOR REPAIR TO TAIL STINGER IAW AQRD ERO-966015,REV.IR DATED 03-02-2020SDR DXTA2020030603550Warning System · false activationRUDDER LIMIT FAIL AMBER CAS ILLUMINATED - RUDDER LIMIT FAIL B AMBER CAS MESSAGE ILLUMINATED DURING DESCENT. CONTROL PAGE INDICATED RUDDER LIMIT 20%. SEE ATTACHED PHOTO.***CORRECTIVE ACTION*** ACCOMPLISHED RUDDER CONTROL SYSTEM LIMITER TEST IAW CE750 M/M CH
27SDR 2020F00091Door Frame · damagedOVERSIZED HOLES IN CABIN DOOR FRAME AND HANDRAIL PIVOT BLOCK. ACCOMPLISHED REPAIR DEFINITION NO. S-750-ATA52/02RD, REPAIR OF OVERSIZED HOLES IN CABIN DOOR FRAME AND HANDRAIL PIVOT BLOCK - REPAIR DATED AUG. 1, 2008- AND FAA FORM 8110-3 DATED AUG. 1, 2008.SDR 2020FA0000189Printed Ckt Board · defectiveCREW REPORTED DURING COCKPIT SETUP PRIOR TO DEPARTURE, A "SECONDARY TRIM FAIL" AMBER CAS MESSAGE ILLUMINATED. THIS
SYSTEM IS REQUIRED FOR DISPATCH, AND THE AIRCRAFT CANNOT BE RELIEVED USING THE MEL OR MMEL. SUBSEQUENT TESTING OF
THIS SYSTEM WAS PERFORMED ANDSDR 2020FA0000161Skin · corrodedCORROSION DAMAGE WAS FOUND AT 5 SITES ON THE RH WING UPPER SKIN FROM CWS 363.9 TO 378.71. REFERENCE FAA FORM 8100-9 FIELD REPAIR FR-750-0201-7656 REV -, DATED 2/6/2020.SDR DXTA2020021753467Float Valve · defectiveWING TANK O'FULL R AMBER CAS ILLUMINATED - WING O' FILL AMBER CAS MSG ILLUMINATED EN ROUTE. ACCOMPLISHED CHECK LIST AND VERIFIED WE WERE LOSING FUEL. TRIED VARIOUS ATTITUDE AND PITCH CHANGES AS WELL AS A 360 DEG TURN BUT NO CHANGE. THERE WAS VERY LITTLE FSDR DXTA2020011323331Actuator · failedDURING GEAR EXTENSION ON FINAL APPROACH, THE NLG GREEN LIGHT DID NOT ILLUMINATE AND RED UNLOCK LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE SELECTED DOWN. BOTH MAIN GEAR LIGHTS ILLUMINATED GREEN. AFTER ROTARY TEST CONFIRMED ALL LIGHTS WORKING, BLEW DOWN THE SDR DXTA2020011303323Squat Switch · defectiveALL LANDING GEAR RETRACTION DID NOT RETRACT - ON GEAR UP COMMAND, THE GEAR DID NOT RETRACT AND 3 GREEN AND 1 RED LIGHTS REMAINED ON. // SIGNOFF // FOUND RH MLG SQUAT SWITCH TO HAVE INTERMITTENT HIGH RESISTANCE. INSTALLED NEW RH SQUAT SWITCH P/N S3176-1 AND RIGSDR AJXA2020012190005Strut · low pressureDURING DEPARTURE, THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR AFTER TAKEOFF. THE AIRCRAFT RETURNED SAFELY TO TETERBORO AIRPORT TO INVESTIGATE THE PROBLEM. THE AIRCRAFT WAS PUT INTO MAINTENANCE AND IT WAS FOUND THAT THE PRESSURE OF THE NOSE GEAR STRUT WASSDR AWKA2019122401Coalescer Bag · wornON APPROACH, THE CAPTAIN'S FOOT WELL FILLED WITH A MIXTURE OF WHAT APPEARED TO BE THICK SMOKE AND VAPOR. THE EMISSION HAD AN ODOR OF BURNED DUST AND MILDEW. AS THE PILOT ADVANCED THE THRUST LEVERS TO APPROACH POWER, THE EMISSION DISCONTINUED. ON LANDING, THE CSDR AWKA2019121001Valve · failedDURING CRUISE AT FL410, THE FLIGHT CREW NOTED THAT THE COCKPIT PAC HAD BECOME UNCONTROLLABLE IN BOTH AUTO AND MANUAL MODES. THE CREW RAN THE APPROPRIATE CHECK LIST AND WITHIN 5 MINUTES, A CABIN PAC O'TEMP MESSAGE WAS RECEIVED. THE FIGHT CREW DONNED THEIR OXYGESDR 2020F00138Actuator · bindingAMBER FLAPS FAIL ANNUNCIATION UPON RETRACTION.SDR 16AA20191125001Hose · leakingDURING TAKEOFF CREW DISCOVERED HYDRAULIC PRESSURE LOSS ON SYSTEM A. CREW DECLARED A EMERGENCY LANDING AND LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT. MANUFACTURER HAS BEEN DISPATCHED AND WILL BE LOOKING INTO THE CAUSE OF FAILURE OF THE HYDRAULIC SYSTEM.SDR 2019FA0000361Skin · corrodedLH AND RH WING PANELS EDDY CURRENT INDICATIONS OF CORROSION ON THE UPPER SURFACE. ACCOMPLISHED FLAP PEEN REPAIR IAW TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ19509M1, DATED MAY 10, 2019.SDR AWKA 2019102101Actuator · failedWHILE DESCENDING, THE FLIGHT CREW RECEIVED AN AMBER PITCH FEEL FAIL CAS MESSAGE. THE MESSAGE WAS INTERMITTENT AT FIRST, BUT THEN STAYED ON UNTIL LANDING. THE FLIGHT CREW FOLLOWED THE CHECK LIST PROCEDURE AN DECLARED AN EMERGENCY FOR A PRIORITY LANDING. THE AIRSDR CVGA20191018001Hose · rupturedUPON TAKEOFF AND AFTER RAISING THE LANDING GEAR, RECEIVED A DOWN AND UNLOCK NOSE GEAR WARNING. BROUGHT THE GEAR HANDLE DOWN AND GOT AN ALL WHEELS DOWN AND LOCK ANNUNCIATION. ALMOST IMMEDIATELY, A HYD VOLUME LOW A (CAS MESSAGE) APPEARED. HYDRAULIC GAUGE FOR THESDR DXTA2019100402915Unknown · odorODOR OF OIL IN THE COCKPIT DURING DESCENT FROM LOW 20,000'S TO GROUND. APU NOT RUNNING. CONFIGURED AIRCRAFT FOR HIGH POWER ENGINE RUNS AND TAXIED AIRCRAFT TO RUN UP AREA. RAN THE NR 1 ENGINE AT CRUISE POWER WITH CABIN AND COCKPIT AIRCONDITIONING ON IN COLDESTSDR AWKA2019100401Ground Stud · dirtyDURING RETURN TO LNK AND WHILE CONDUCTING A MX CONFIDENCE FLIGHT FOR FLAP ISSUE, FLIGHT CREW RECEIVED AN AMBER FLAP FAIL CAS MESSAGE. CREW RAN THE APPROPRIATE CHECKLIST AND THEN DECLARED AN EMERGENCY. SEVERAL MINUTES FOLLOWING, CREW WAS ABLE TO LOWER THE FLAPSSDR EBV220191002001Attach Fitting · crackedFOUND CRACK IN RH AUXILIARY WING SPAR INBOARD ATTACH FITTING. LOCATED ON AFT CLOSEOUT OF RH MLG WHEEL WELL AT FS446.38. CRACK EXTENDS FROM BOLT HOLE TO BOLT HOLE THROUGH WEB IN FITTING. FOUND BY VISUAL INSPECTION DURING SCHEDULED MAINTENANCE.SDR DXTA201909192861Strut · out of toleranceIN FLIGHT, ONCE IN CRUISE AND SECOND TIME DURING DESCENT. UNLOCK RED GEAR LIGHT ILLUMINATED FOR ABOUT ONE SECOND. LOUD NOISE APPEARED TO BE COMING FROM THE NOSE GEAR AREA, GEAR DOOR OPENED AT OVER OVER 300 KTS. IT WAS FOLLOWED BY A LOUD BANG FROM THE NOSE GEARSDR AWKA2019082701Diode · shortedDURING CLIMB OUT THROUGH FL350 FOR FL450, THE FLIGHT CREW RECEIVED A FMS SINGLE OPERATION MODE MESSAGE ON THE RIGHT FMS AND THE LEFT FMS DISPLAY WENT BLANK FOLLOWED BY THE DU 1 DISPLAY GOING BLANK, FOLLOWED BY BATT 1 OVER CURRENT MESSAGE AND THE AUTOPILOT DISESDR O2GA2019081490401Circuit Board · failedLEFT STAB BLEED LEAK WARNING ANNUNCIATOR ILLUMINATED DURING FLIGHT. ANNUNCIATOR WENT AWAY WITH POWER REDUCED BUT CAME BACK AFTER POWER APPLIED. FOLLOWED CHECKLIST, DECLARED AND EMERGENCY. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE BLEAD THE LEFT BLEAD AISDR CA190814006Line · chafed(CAN) THE LH ELEVATOR HYDRAULIC LINE WAS CHAFFED AS A RESULT OF CONTACT WITH THE HORIZONTAL STAB INTERNAL STRUCTURE RESULTING IN FAILURE. DUE TO THIS FAILURE THE AC EXPERIENCED A LOSS OF SYSTEM A HYDRAULIC PRESSURE. (TC# 20190814006)SDR AJXA201908220002Computer · malfunctionedWHILE IN FLIGHT THE CREW NOTICED A FLIGHT GUIDANCE COMPUTER FAILURE ON THE EICAS. THE CREW DIVERTED TO KCLE SAFELY AND THE AIRCRAFT WAS SENT TO MAINTENANCE AT CONSTANT WHILE IN FLIGHT THE CREW NOTICE A FLIGHT GUIDANCE COMPUTER FAILURE ON THE EICAS. THE CREW DISDR AJXA201908150245Computer · failedWHILE IN FLIGHT THE CREW NOTICED A FLIGHT GUIDANCE COMPUTER FAILURE ON THE EICAS. THE CREW DIVERTED TO KCLE SAFELY AND THE AIRCRAFT WAS SENT TO MAINTENANCE AT CONSTANT WHILE IN FLIGHT THE CREW NOTICE A FLIGHT GUIDANCE COMPUTER FAILURE ON THE EICAS. THE CREW DISDR 2020FA0000148Probe · false indicationPILOTS REPORTED LT PYLON OVERHEAT. ACFT RETURNED TO KAZO. TROUBLESHOT TO FAULTY PYLON TEMPERATURE PROBE. REPLACED BOTH PYLON PROBES WITH NEW PROBES. OPERATION CHECKED GOOD.SDR 2020FA0000147Probe · malfunctionedPILOTS REPORTED LT PYLON OVERHEAT. ACFT RETURNED TO KAZO. TROUBLESHOT TO FAULTY PYLON TEMPERATURE PROBE. REPLACED BOTH PYLON PROBES WITH NEW PROBES. OPERATION CHECKED GOOD.SDR 2020FA0000103Probe · malfunctionedPILOTS REPORTED LT PYLON OVERHEAT. AIRCRAFT RETURNED TO DEPARTURE. TROUBLE SHOT FAULTY PYLON TEMPERATURE PROBE. REPLACED BOTH PYLON PROBES WITH NEW PROBES. OPS CHK`D GOOD.SDR JGVR20190415002Spar · corrodedNUMEROUS AREAS OF CORROSION AROUND FASTENERS ON RT WING, AFT SPAR ON BOTH SIDES ON OUTBOARD AILERON HINGE. MECHANICALLY BLENDED LEVEL 1 CORROSION RT WING AFT SPAR BETWEEN THE MIDDLE AND OUTBOARD AILERON HINGES, IAW SRM 51-10-01. EVALUATED BLENDED AREAS AND FOSDR JGVR20190715001Hinge · corrodedNUMEROUS AREAS OF SUSPECTED LEVEL 1 CORROSION ON LT WING, AFT SPAR BETWEEN THE MIDDLE AND OUTBOARD AILERON HINGE. MECHANICALLY BLENDED LEVEL 1 CORROSION LT WING AFT SPAR BETWEEN THE MIDDLE AND OUTBOARD AILERON HINGES, IAW SRM 51-10-01. EVALUATED BLENDED AREAS SDR O2GA2019062790001Latch · out of adjustIN FLIGHT CREW HEAR A POPPING SOUND IN COCKPIT FOLLOWED BY "NOSE DOOR OPEN L" CAS MESSAGE. FOLLOWED EMERGENCY CHECKLIST AND DIVERTED. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND NOSE FORWARD LATCH OPEN. LATCH WAS ADJUSTED AND LUBRICATED. OPERATION CHECKED OKAY. SDR 2019F00227Fairing · crackedAFT SECTION BULLET DAMAGE IAW ENGINEERING MEMO DQ21974M1SDR AWKA2019061701Pump · leakingSHORTLY AFTER TAKEOFF, THE FLIGHT CREW NOTICED THE A SIDE HYDRAULIC PRESSURE WAS FLUCTUATING BETWEEN 3200 AND 3300 PSI. AS THE FLIGHT CONTINUED, THE "A" SIDE VOLUME WAS STEADILY DECREASING. AS THE QUANTITY FELL BELOW 45% PERCENT, THE DIVERTED THE FLIGHT. EVENTSDR CWQA20190613001Brake Assy · bindingDURING TAKEOFF ROLL AROUND 35 KNOTS, CREW NOTICED AIRCRAFT PULLING LEFT AND FELT AIRCRAFT STRUGGLING TO ACCELERATE. CREW ABORTED TAKEOFF, EXITED RUNWAY, AND FELT LEFT BRAKE DRAGGING AND FELT MAIN TIRES BLOW. MAINTENANCE EVALUATION FOUND BOTH LEFT MAIN TIRES SDR CA190612012Door · malfunctioned(CAN) IN DECEMBER 2018 AIRCRAFT C750 C-XXXX HAD ADS-B MODIFICATION SB750-34-58R1 INSTALLED AT CESSNA/TEXTRON SERVICE CENTER. WE JUST BEGINNING A SCHEDULED INSPECTION ON THE AIRCRAFT AND UPON ATTEMPTED TO REMOVE THE EMERGENCY EXIT, TO FIND THE WIRE HARNESS INSTSDR 2019F00220Fairing · wornREPAIR OF RUDDER FAIRING DAMAGE (ONE FASTENER PULLED THROUGH).SDR 2019F00217Skin · corrodedREPAIR OF LOWER WING SKIN CORROSION ACCOMPLISHED IAW TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ19509M1, DATED 10 MAY 2019.SDR O2GA2019061390101Hose · rupturedAFTER TAKEOFF GEAR SELECTED TO UP POSITION, CAS MESSAGE 'HYD VLUME LOW A'. THE HYDRAULIC QUANTITY DROPPED TO ZERO, FOLLOWED BY 'HYD PTU FAIL' CAS MESSAGE. EMERGENCY WAS DECLARED. DIVERTED TO KMSY. LANDING AND BRAKING WERE UNEVENTFUL. MAINTENANCE REMOVED AND RESDR 2019F00219Cap · out of toleranceAPU MUFFLER EXHAUST CAP ASSEMBLY OVERSIZED HOLES.SDR 2019F00218Cap · out of toleranceAPU MUFFLER EXHAUST CAP ASSEMBLY OVERSIZED HOLES.SDR 2019FA0000169Firewall · crackedLEFT ENGINE INLET AFT BULKHEAD/FIREWALL CRACK. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER. DQ21738M1REVA (CORRECTED DQ NUMBER, TT AND TL); 750-0203 (N999QS) LEFT ENGINE INLET AFT BULKHEAD/FIREWALL CRACK.SDR 2019F00199Fairing · damagedOVER-WING FAIRING (LEFT SIDE) DAMAGE (FASTENER HOLES OVERSIZED). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ21615M1 DATED MAY 21, 2019; 750-0203 (N999QS) OVER-WING FAIRING (LEFT SIDE) DAMAGE (FASTENER HOLES OVERSIZED).SDR 2019F00198Skin · gougedGOUGE DAMAGE, FUSELAGE, MAIN CABIN DOOR SKIN, FS 190.2 AND WL 143.5. ACCOMPLISHED REPAIR DEFINITION NO. FR-750-0203-6643 REV-, FIELD REPAIR - GOUGE DAMAGE, FUSELAGE, MAIN CABIN DOOR SKIN, FS 190.2 AND WL 143.5 - REPAIR DATED MAY 21, 2019- AND FAA FORM 8100-9
Back to Textron 750