N694QS
Service difficulty reports · 16
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N694QS' AND registry_match = 'registration' 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 n_number = 'N694QS' AND registry_match = 'registration' 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 2025FA0000834Hp Turbine · crackedRH ENGINE HAS EVIDENCE OF AXIAL CRACKING ON HPT STAGE 1 BLADES (4 TOTAL BLADES).SDR DXTA2025060603788Door · bindingMAIN CABIN DOOR DIFFICULT TO CLOSE FROM INSIDE. FEELS LIKE PIN ALLIGNMENT, TOP AFT PIN. FUNCTIONAL FROM EXTERIOR. DOOR IS ALSO INTERMITTENTLY SLOW TO OPEN. UPON INSPECTING OF THE MED. FOUND UPPER AFT CABIN DOOR STOP LOOSE. ADJUSTED THE CLEARANCE BETWEEN SDR DXTA2025031702678Battery Pack · inoperativeEMERGENCY LIGHTING: EMERGENCY LIGHTS DO NOT ILLUMINATE IN THE ARM POSITION. CORRECTIVE ACTION; REPLACED THE EMERGENCY LIGHT BATTERY PACK ASSEMBLY BATTERY !AW SIL·CBS28+2024-001. OPS CHECK GOOD.SDR 2025FA0000131Deck Plate · corrodedFOUND LAVATORY DECK CORRODED ON UNDER SIDE. COMPLIED WITH RFTS-113043 N694QS (680A-0226) TOILET SEAL PANEL CORROSION REV.0 DATED 21FEB25.SDR 2025FA0000125Tail Cone · corrodedAFT FUSELAGE FAIRING SUPPORT CORROSIONSDR DXTA2025021002265Battery · dischargedCABIN EMERG LIGHT: DURING THE POWER ON CHECKLIST, WITH THE BATTERIES OFF, WHEN THE EMER LTS SWITCH IS PLACED IN THE ARM POSITION NONE OF THE INTERIOR EMERGENCY LIGHTS ILLUMINATE. RAN THE QRH FOR EMERGENCY LIGHTS FAIL PERFLIGHT TEST AND TRIED CHARGING THE EMERGSDR DXTA2025012902141Battery Pack · no testDURING THE EMER LIGHT TEST WHILE SELECTING TO ARM THE EMERGENCY EXIT AND OVERHEAD LIGHTS DID NOT ILLUMINATE. WHEN SELECTING EMER LIGHT TO ON THE LIGHTS WOULD ELIMINATE CORRECTLY. WE THEN CHARGED THE BATTERIES FOR 30 MINUTES WITH THE APU. ON THE SECOND TEST THSDR DXTA2024110701046Rudder · no discrepancyRUDDER: DURING APPROACH WITH 15 KTS LEFT CROSSWIND THE RUDDER PEDAL SEEM TO BE BINDING AND HARD TO PUSH FOR CROSSWIND ALIGNMENT. THE YAW DAMPER WAS VERIFIED OFF. AND THERE WERE NO CAS MESSAGE. BUT FELT LIKE RUDDER WAS BEING LIMITED. SEEMS TO FUNCTION FINE ON GSDR DXTA2024021510901Generator · failedHALF WAY DURING FLIGHT AT 40,000 THE RIGHT WINDSHEILD HEAT INOP CAS MESSAGE CAME ON. PROCEDURE ON CHECKLIST WAS COMPLETED. THIS IS A REPEAT WRITE UP. REMOVED FAILED AC GEN PN: 9914443-1 SN: 537. INSTALLED NEW CUSTOMER SUPPLIED AC GEN PN: 991443-1 SN: 1203 AS SDR DXTA2023111310032Unknown · unknownLAV EMERG LIGHT: WITH THE EMER LIGHT TO ARM AND THE MAIN BATTERIES OFF, THE EXIT SIGN ON THE BULKHEAD BEHIND SEAT 7 IS INOP, THE SPOT LIGHT AT SEAT 7 IS INOP, THE KICK PLATE LIGHT UNDER THE LAV IS INOP, AND THE SPOTLIGHT AT THE LAV IS INOP. ///SIGN-OFF/// COMPSDR DXTA2023071991230Unknown · unknownCABIN DOOR OPEN AMBER CAS: CHECK DOORS AMBER CAS AND AMBER DOOR OPEN LIGHT ON THE HANDLE ALL ILLUMINATED WITH THE DOOR CLOSED. QRH COMPLIED WITH. RESULTS WERE UNSUCCESSFUL. VERIFIED THAT THE EXTERNAL CABIN DOOR OPEN LIGHT AND THAT THE CABIN DOOR OPEN CAS MESSSDR 2023FA0000103None · noneIMPACT DAMAGE - L/H WING, UPPER AND LOWER SKINS, TRAILING EDGE, CWS 320 - WS 369. REFERENCE FR-680A-0226-10757 AND FAA FORM 8100-9 DATED 06JUL2022. REFERENCE TEXTRON AVIATION LETTER DQ34743M1, 680A-0226 (N694QS)LEFT WING LOWER SKIN DIS-BOND (FR-680A-0226-10757SDR DXTA2021091548840Landing Gear · defectiveGSD FAIL 2 AMBER CAS: SHORTLY AFTER BEGINNING OUR DISSENT FROM FLIGHT LEVEL 410 THE GSD FAIL 2 AMBER ICAS MESSAGE ELIMINATED. THE AMBER MESSAGE CHECKLIST DROVE US TO BLOW THE GEAR DOWN. STOWED LANDING GEAR HANDLE AND SAFETED. SERVICED LANDING GEAR BOTTLE WSDR 2021F00219Skin · chafedCHAFE IN LOWER FUSELAGE SKIN CAUSED BY ANTI-ICE CROSSFLOW VALVE. ACCOMPLISHED TEXTRON STANDARD REPAIR SR-680A-ATA53-22175 DATED 7/19/2019, STEPS 1-5, STEPS 6-8 N/A DUE TO COMPLETION OF SB680A-30-01. INCLUDED FAA FORM 8100-9 DATED 7/19/2019.SDR DXTA2021032239780Support Rod · bentWHILE CLOSING THE MED THE DOOR SUPPORT ROD WAS BENT. THIS ALSO PUT ABOUT A 1/2" CRACK IN THE INNER LINER OF THE MED. "CORRECTIVE ACTION" INSTALLED NEW LIFT LINK ASSEMBLY P/N 7411323-2 NSN AS REQUIRED. RIGGED THE DOOR AS REQUIRED.SDR DXTA2021020404673Indicator · warning messageGEAR POSITION & WARNING: LANDING GEAR EXCEEDED GEAR EXTENSION SPEED AT APPROX 230KTS CORRECTIVE ACTION JACKED AIRCRAFT, PERFORMED SLOW CYCLE OF LANDING GEAR. INSPECTED LANDING GEAR, ATTACH STRUCTURE, HEAR DOORS AND LANDING GEAR CLEARANCE CHECKS. DOWN JACKED
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