N698QS, cancelled Jul 7, 2025
Service difficulty reports · 44
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 = 'N698QS' AND deregistration_id = 'N698QS-2025-07-07' 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 = 'N698QS' AND deregistration_id = 'N698QS-2025-07-07' 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 DXTA2025030302554Door · damagedMAIN DOOR: WHEN OPENING MAIN CABIN DOOR , ONCE THE DOOR PINS RELEASE THE DOOR WILL FALL OPEN RAPIDLY TO ABOUT 1 FOOT FROM FULLY OPEN POSITION. WHEN CLOSING CABIN DOOR ALL IS NORMAL UNTIL IT REACHES ABOUT 2 TO 3 FEET OFF THE GROUND AND THE IT TAKES ALOT OF DOWSDR DXTA2025022402449Rub Strip · wornMAIN CABIN DOOR DOES NOT OPEN WHEN MOVING THE HANDLE TO THE OPEN POSITION UNLESS YOU PULL THE PRE-CATCH THEN THE DOOR WILL OPEN. THIS HAPPENS FROM THE OUTSIDE AS WELL AS THE INSIDE. PERFORMED ADJUSTMENT TO THE MED FWD RUB BLOCK AND FOLLOW ON IAW RFTS-113085 RESDR DXTA2025022002400Latch · out of adjustMAIN DOOR: REPEAT WRITE UP. MAIN ENTRY DOOR HANDLE IS DIFFICULT TO LOCK AND UNLOCK AND VERY DIFFICULT TO UNLOCK OR LOCK AFTER COLD SOAK FLIGHT. VIDEO ATTACHED. CORRECTIVE ACTION: ADJUSTED LATCH PLATES. OPS CHECK GOOD. IAW CE-560XL AMM CH 52-10-00.SDR DXTA2024122001555Door · out of adjustMAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN WITHOUT USING PRECATCH BOTH FROM OUTSIDE AND INSIDE. ADJUSTED DOOR IAW AMM 52-10-00SDR DXTA2024120201301Precatch · out of adjustMAIN DOOR HANDLE: THE AMOUNT OF FORCE REQUIRED TO LOCK OR OPEN THE MAIN CABIN DOOR IS EXCESSIVE. CORRECTIVE ACTION; ADJUSTED MAIN DOOR PRE-CATCH MECHANISM IAW CE 560XL MM 52-10-01. NO FURTHER DEFECTS NOTED.SDR DXTA2024112601235Handle · bindingMAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE FROM INSIDE OF CABIN. MAIN DOOR: MAIN CABIN DOOR HANDLE REQUIRED TRIED ADJUSTING AFT LOWER SOCKET BUT NEEDS MORE ADJUSTMENT, CALLED NETJETS AND THEIR TECH'S ADJUSTED THE AFT LOWER SOCKET AND THESDR DXTA2024111401124Door · bindingMAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE FROM INSIDE OF CABIN. OPS CHECK DOOR AND VERIFIED DOOR STRUGGLES TO CLOSE AND OPEN. SEEMS TO BE TOUGHER WHILE OPERATING FROM INSIDE CABIN. LUBRICATED DOOR PINS, LATCHES ECT. NO FIX. PLACED ALUMSDR DXTA2024090300393Switch · defectiveSTAB MISCOMPARE LIGHT: ON 5 MILE FINAL PRIOR TO LANDING, WE GOT THE STAB MISCOMPARE ANNUNCIATOR LIGHT AND ALSO THE HYD PRESS LIGHT ( FLASHING ). TOOK A LOT OF CONTROL FORCE TO HOLD ALTITUDE. RAN QRH CHECK LIST AND LANDED UNEVENTFULLY. PHOTO ATTACHED. PRIOR TO SDR DXTA2024062412149Warning Message · false activationDURING TAXI TO ACTIVE RUNWAY THE LO BRK PRESS AND ANTI SKID INOP WARING LIGHTS CAME ON. TRIED STOPPING AIRCRAFT WITH TOE BRAKES BUT THEY WHERE INOP. STOPPED AIRCRAFT USING EMERGENCY BRAKE. AIRCRAFT TOWED BACK TO RAMP. TROUBLESHOT BRAKE SYSTEM, NO FAULTS WERE SDR DXTA2024030111052Pump · leakingLEFT MLG LANDING GEAR EXTENSION: PERFORMED EMERGENCY LANDING GEAR EXTENSION DUE TO NO HYDRAULIC FLUID. HYD LOW LVL AND BOTH HYD LOW FLO ANNUCIATORS ILLUMINATED AT FL400. AFTER LANDING, AIRPORT PERSONNEL DISCOVERED HYDRAULIC POOLING AREAS INSIDE THE HYDRAUSDR DXTA202403011105Hydraulic System · leakingLEFT MLG LANDING GEAR EXTENSION: PERFORMED EMERGENCY LANDING GEAR EXTENSION DUE TO NO HYDRAULIC FLUID. HYD LOW LVL AND BOTH HYD LOW FLO ANNUCIATORS ILLUMINATED AT FL400. AFTER LANDING, AIRPORT PERSONNEL DISCOVERED HYDRAULIC POOLING AREAS INSIDE THE HYDRAUSDR DXTA2024030111051Pump · failedHYDRAULIC RESERVOIR: DURING FLIGHT AT FLIGHT LEVEL 400 WE RECEIVED A HYD LOW LVL ANNUCIATOR. WE RAN THE QRH AND ANNUCIATOR REMAINED ON. REMOVED UH EDP PN 9912062-4 SN 6008 DUE TO AIRCRAFT LOSS OF HYDRAULIC FLUID AND INSTALLED THE NEW UNIT LISTED ABOVE IAW ASDR DXTA2024022010939Windshield · failedCAPTAIN COCKPIT WINDOW SHATTERED IN FLIGHT. WE HAD A L W/S FAULT ANNUNCIATOR COME ON WITH ASSOCIATED MASTER CAUTION. WE RAN THE ASSOCIATED QRH AND THE ANNUNCIATOR WENT OUT. FIVE MINUTES LATER THE WINDOW SHATTERED. WE WERE AT FL200. COCKPIT FORWARD OR SIDE WINSDR DXTA2023122810455Unknown · unknownMAIN ENTRANCE DOOR IS HARD TO LATCH AND UNLATCH. ESPECIALLY FROM THE INSIDE. PERFORMED SEVERAL OPS CHECK OF THE MAIN ENTRANCE DOOR WITH NO DISCREPANCIES TO NOTE AT THIS TIME, IAW AMM 52-10-00.SDR DXTA2023090594650Unknown · unknownMAIN DOOR: MAIN DOOR EXTREMELY DIFFICULT TO CLOSE FROM THE INSIDE. THE HANDLE CLOSES FINE THE FIRST 45 DEGREES THEN MEETS VERY STIFF RESISTANCE. THE MAIN DOOR CLOSES FINE FROM THE OUTSIDE. //SIGNOFF// FOUND THE MED LATCH PLATES OUT OF ADJUSTMENT PERFORMED THE SDR DXTA2023080492260Unknown · unknownEMERG EXIT SIGN/LIGHT: EXIT SIGN TO LEFT OF MAIN ENTRY DOOR WILL NOT ILLUMINATE IN ANY SWITCH CONFIGURATION. GAINED ACCESS TO EXIT SIGN TO LEFT OF MAIN ENTRY DOOR AFTER FURTHER T/S FOUND ON CONNECTOR FRAYED. REMOVED DEFECTIVE EXIT SIGN TO LEFT OF MAIN ENTRY DSDR DXTA2023072191430Unknown · unknownMAIN CABIN DOOR ACOUSTIC SEAL WILL NOT RELEASE AFTER SHORT FLIGHT WITH SERVICE AIR ON. DOOR CANNOT BE OPENED WHILE APU WAS RUNNING. HAD TO SHUT DOWN APU TO REMOVE SERVICE AIR BEFORE WE COULD EXIT. REMOVED CABIN ENTRY DOOR STEPS AND INSPECTED PRIMARY DOOR SEALSDR EBVR202305160001Unknown · unknownFOUND CORROSION ON LH/RH WING UPPER SURFACE ALONG FS 335.38 OVER MAIN WING SPAR. DAMAGE SUBMITTED TO TEXTRON AND REPAIRED IAW TEXTRON FIELD REPAIR FR-560-5653-11886 DATED 5/15/23. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 3J7R2023021700001Battery Pack · depletedREAR CABIN AND EXTERIOR EMERGENCY LIGHTS INOP WHEN MAIN BATTERY IS OFF. LIGHTS WORK NORMALLY WHEN MAIN BATTERY IS ON.SDR DXTA2022060263150Fan · shortedCOCKPIT ODOR: JUST PRIOR TO TAKEOFF THE APU WAS SHUTDOWN AND THE COCKPIT RECIRC FAN TURNED TO THE HIGH POSITION. NOTICED AT THE END OF TAKEOFF ROLL A ELECTRICAL ODOR THERE WAS NO SMOKE. I TURNED THE COCKPIT RECIRC FAN OFF, BUT THE ODOR DID NOT DISSIPATE. ON THSDR DXTA2021081647000Lock Bolt · looseMAIN CABIN DOOR EXTREMELY HARD TO CLOSE FROM OUTSIDE AS WELL AS INSIDE. INSPECTED DOOR BOLT SYSTEM PINS, FOUND DIRTY AND DRAGGING. CLEANED AS NEEDED, GAINED ACCESS TO DOOR INNER MECHANISM, OPERATED AND NOTED SMOOTH WHEN DOOR WAS OPEN. LUBRICATED AS NEEDED. CLSDR DXTA2021061443550Cable · defectiveLEFT ENGINE FIRE DETECTION LIGHT: IN FLIGHT CLIMBING TO 10000' THE LEFT FIRE RED LIGHT CAME ON. ACCOMPLISHED ENTIRE INFLIGHT ENGINE FIRE QRC & ENGINE INOP APPROACH QRC & ENGINE INOP LANDING QRC. ENGINE FIRE LIGHT NEVER EXTINGUISHED. FIRE DEPARTMENT AT KAZO FOUSDR JGVR2020012017004Axle · corrodedFOUND CORROSION ON THE LT MAIN LANDING GEAR AXLE. REPLACED CORRODED AXLE WITH NEW P/N 6641646-1.SDR JGVR2020012017003Hinge · corrodedFOUND CORROSION ON THE MAIN ENTRY DOOR FORWARD HINGE ON THE FUSELAGE SIDE HINGE-HALF. BLENDED CORRODED AREA, PERFORMED NDT AND REPORTED RESULTS FOR DISPOSITION. REPLACED FUSELAGE SIDE OF THE FWD HINGE WITH NEW P/N 6611037-1.SDR JGVR202001197002Stiffener · crackedFOUND CRACKED STIFFENER NEAR THE AFT COUNTERBALANCE SPRING OF THE MAIN ENTY DOOR. REPAIRED STIFFENER BY CUTTING OUT THE CRACKED AREA AND INSTALLING REPAIR DOUBLER AND FILLER IAW ENGINEERING ORDER.SDR JGVR202001197001Trunnion · corrodedFOUND CORRODED AREAS ON THE RT MAIN LANDING GEAR TRUNNION AT THE UPPER BRAKE LINE BAND CLAMP, REMOVED CLAMP BLENDED AREA AND TREATED IAW REPAIR MEMO.SDR DXTA2019062412525Throttle · obstructedRIGHT ENGINE POWER LEVER STUCK - ON LANDING ROLLOUT, ATC GAVE CLEARANCE TO MAKE NEXT LEFT TURN. THE RIGHT SEAT PILOT ADVANCED THE RIGHT THROTTLE TO ASSIST THE TURN. WHEN HE ATTEMPED TO RETARD THE THROTTLE IT STUCK ABOUT HALF WAY. PIC GRABBED THE RIGHT THROTSDR DXTA2019FA0000061Floorboard · crackedREPAIR OF LEFT FORWARD COCKPIT FLOORBOARD DAMAGE (CRACK). ENGINEERING LETTER DQ18712M1 DATED MAR 6, 2019.SDR DXTA2015102606114Brake Sys · malfunctionedUPON INITIAL TAKEOFF ROLL THE ACFT PULLED TO THE RT. AT 30 KNOTS THE TAKEOFF WAS ABORTED. DURING THE ABORT THE ACFT PULLED HARD LT. UPON EXITING THE RUNWAY IT SEEMED TO TAKE EXCESSIVE POWER TO CLEAR TO THE TAXIWAY. ON TAXI IN, CHECKED THE BRAKES AT A HIGHESDR DXTA2014050205757Door Frame · chafedCHAFE ON DOOR FRAME STRUCTURE ABOVE & FWD OF DOOR. REPAIRED IAW RD 5653 04RD.SDR CWQR20131016044Hinge · crackedDURING A SCHEDULED MAINTENANCE, FOUND THE AFT MAIN CABIN DOOR HINGE HALF VERTICAL ATTACH FLANGE CRACKED FROM THE EDGE OF THE PART 0.60" INWARD. NDT INSPECTION VERIFIED CRACK. R & R HINGE HALF ASSY. SUBMITTED SERVICE CONDITON REPORT TO MFG REF NR 672273.SDR DXTA2011031704512Uplock Switch · out of adjustNORMAL TAKEOFF ROLL, UPON POSITIVE RATE, GEAR LEVER WAS SELECTED UP, IT APPEARED GEAR CYCLED UP HOWEVER RED "UNLOCK" LIGHT REMAINED ILLUMINATED. FOUND HYD FLUID LEVEL FULL AND NO LEAKS NOTED. PERFORMED GEAR SWINGS MULTIPLE TIMES IAW MM 32-01-00 AND COULD NOTSDR DXTA2011020104438Control Handle · malfunctionedAFTER T/O, PLACED GEAR LEVER UP, RED LIGHT CAME ON, SOUNDED LIKE DOORS OPENED, BUT 3 GREEN STAYED ON WITH THE RED. WIGGLED THE HANDLE IN THE UP POSITION AND THEN THE GEAR DID RETRACT NORMALLY. R & R LANDING GEAR CONTROL HANDLE IAW MM 32-30-01. OPS CHECKED GSDR DXTA2009110203838Structure · dentedBIRD STRIKE ON THE RIGHT SIDE JUST ABOVE THE ROSEMOUNT, IT CONTINUE TO THE RIGHT WING AT THE STALL STRIP DENTING THE WING AND IT HIT THE RT ENGINE JUST BELOW THE BOTTOM. REMOVED DENTED RT WING INBD HEATED L/E, INSTALLED NEW L/E IAW SRM 51-40-03, OPS CHECKED GSDR DXTA200811143356Check Valve · unknownABORT, THE LIGHT EXTINGUISHED ( POWER REDUCTION). COMPLIED WITH APPENDIX 29-2, "O" PROCEDURE. DEFERRED IAW MEL 29-2. CAT C. DUE 11-24-08. RAN AC AT T/O POWER IN VARIOUS CONFIGURATIONS COULD NOT DUPLICATE, ALL OPS NORMAL. FOUND HYDR RESERVOIR NOT FULLY SERVICEDSDR DXTA20081114Switch · malfunctionedDURING TAKEOFF AT APPX 60KTS, THE RT HYD LOW FLOW ANNUNCIATOR ILLUMINATED. AFTER ABORT, THE LIGHT EXTINGUISHED( POWER REDUCTION). COMPLIED WITH APPENDIX 29-2, "O" PROCEDURE. DEFERRED IAW MEL 29-2. CAT C. DUE 11-24-08. RAN A/C AT TO POWER IN VARIOUS CONFIGURASDR DXTA2008111703356Warning System · activatedDURING TAKEOFF AT APPROX 60KTS, THE RIGHT HYD LOW FLOW ANNUNCIATOR ILLUMINATED.SDR DXTA200811093346Reservoir · underservicedLOW HYD FLOW RT ANNUNCIATOR ILLUMINATED WHEN POWER APPLIED FOR T/O TROUBLESHOT HYD SYS. FOUND HYD RESERVOIR UNDERSERVICED. INSPECTED HYD PANEL ASSY. HOOKED UP HYD SERVICE CART TO ACFT, CYCLED HYD COMPONETS AND SERVICED HYD RESERVOIR RAN ACFT TO T/OSDR DXTA2008111003346Warning System · activatedLOW HYD FLOW RT ANNUNCIATOR ILLUMINATED WHEN POWER APPLIED FOR T/O. T/O ABORTED.SDR DXTA200810093300Actuator · faultyWHEN LANDING GEAR WAS SELECTED DOWN. RT GREEN LIGHT ILLUMINATED. THE NO GREEN LIGHT APPEARED TO TAKE LONGER THAN NORMAL TO ILLUMINATE THE LT GREEN LIGHT DID NOT ILLUMINATE AND THE RED UNLOCK LIGHT REMAINED ILLUMINATED. COMPLETED THE EMERGENCY CHECK LIST INCLUDSDR DXTA200803300Warning System · activatedWHEN LANDING GEAR WAS SELECTED DOWN, THE "RT" GREEN LIGHT ILLUMINATED. THE "LT" GREEN LIGHT DID NOT ILLUMINATE AND THE RED "UNLOCK" LIGHT REMAINED ILLUMINATED.SDR 2008FA0000360Stiffener · misinstalledFOUND RT STIFFENER (PN 662121126) INADVERTENTLY INSTALLED IN LT POSITION. WITH LANDING GEAR IN THE STOWED POSITION, THE ACTUATOR CONTACTED THE STIFFENER AND CAUSED MINOR CHAFFING. NEITHER THE ACTUATOR NOR THE STIFFENER WERE DEFORMED/ DAMAGED. (K)SDR CWQR200804Stiffener · chafedAC WAS IN SCHEDULED MAINTENANCE, AN INSP NOTICED THAT THE LT MAIN GEAR ACTUATOR WAS CHAFING ON THE WING SPAR WHEEL WELL STIFFENER, PN 6621211-26. UPON FURTHER INVESTIGATION WE FOUND THAT THE -26 STIFFENER WAS INSTALLED ON THE WRONG SIDE FROM THE FACTORY. SINCSDR CWQR200707Balance Weight · misinstalledDURING A PHASE 1-4 INSPECTION, FOUND THE RUDDER BALANCE WEIGHT WAS TRIMMED DOWN AND ATTACHED WITH ONLY (2) BOLTS.THE IPC SHOWS (4) BOLTS TO ATTACH THIS WEIGHT. CONTACTED MFG ENGINEERING, THEY STATED THE WEIGHT REQUIRES (4) BOLTS TO MEET THE 100 (G) STANDARD. A
Back to N698QS, cancelled Jul 7, 2025