N380QS, cancelled Feb 10, 2026

Service difficulty reports · 53

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 = 'N380QS' AND deregistration_id = 'N380QS-2026-02-10'
  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.

SDR 2025F00128Spar Cap · corrodedEXFOLIATION CORROSION ON LH AFT SPAR LOWER CAP BEHIND PANEL 720DL. MECHANICALLY REMOVED AREA OF CORROSION FROM LH WING AFT SPAR IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMMay 20, 2025 · N380QS · Cessna 680A · Wing SparSDR 2025F00129Fitting · corrodedRH MLG WS 37.00 SUPPORT BEAM IN GEARWELL, FWD AREAS, HAVE HYD LINE CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHANICALLY BLENDED CORROSION IN ACCORDANCE WITH C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 EXCEEDING .May 20, 2025 · N380QS · Cessna 680A · Wing Main, Frame StructureSDR DXTA2025040202907Warning Message · illuminatedBLEED AIR O'TEMP R AMBER CAS: ON THE PRIOR FLIGHT BLEED AIR OVER TEMP RIGHT AMBER CAST ILLUMINATED. COMPLIED WITH CHECKLIST AND TURNED OFF RIGHT SIDE PRESSURE FOR 30 SECONDS. LIGHT WENT OUT AND DID NOT COME BACK ON. ON THE FLIGHT IN QUESTION, BLEED AIR OVER TEApr 1, 2025 · N380QS · Cessna 680SOV · Pneumatic Distribution SystemSDR DXTA2025013002121Actuator · faultedFLAP: AFTER TAKEOFF WHEN BRINGING FLAPS FROM 7 TO 0, WE GOT A FLAPS FAIL, WE RAN ALL THE CHECKLIST AND DID AN EMERGENCY RETURN. CORRECTIVE ACTION: REPLACED FLAP ACTUATOR. OPS CHECK GOOD. IAW CE-680 AMM 27-50-00. OSD: 1/30/2025Jan 26, 2025 · N380QS · Cessna 680SOV · Trailing Edge Flap ActuatorSDR DXTA2024112501227G Switch · damagedEMERGENCY LIGHTING: REPEAT WRITE UP. EMERGENCY LIGHTING: WITH EMER LTS SWITCH IN THE OFF POSITION, THE FOLLOWING LIGHTS REMAINED ILLUMINATED AND COULD NOT BE EXTINGUISHED: RIGHT WING FORWARD OVER WING LIGHT, EXIT LIGHT AND OVERHEAD LIGHT ABOVE EMERGENCY EXITNov 21, 2024 · N380QS · Cessna 680SOV · Emergency LightingSDR 2024F00172Torque Tube · corrodedDURING RUDDER UPPER TORQUE TUBE DETAILED INSPECTION FOUND CORROSION TO EXTEND BETWEEN 0.1 AND 0.2 INCH FROM THE TORQUE TUBE. REMOVED CORRODED RUDDER TORQUE TUBE (RUDDER P/N 6933000-19 S/N 573185) AND REPLACED WITH NEW RUDDER TORQUE TUBE DUE TO LEVEL 2 CORROSIOJul 23, 2024 · N380QS · Cessna 680A · Rudder StructureSDR 2024FA0000511Spar · corrodedMECHANICALLY REMOVED 2 EA AREAS OF CORROSION ON LH WING AFT SPAR, LOWER CLIP INBD SIDE OF WS 37.00 IAW C680 SRM 51-70-02. EVALUATED AND FOUND BLENDED AREAS TO BE OUT OF LIMITS IAW CESSNA 680 SRM 51-70-02. COMPLIED WITH TEXTRON FIELD REPAIR FR-680-0089-13574, RJul 23, 2024 · N380QS · Cessna 680A · Wing SparSDR DXTA2021102250750Ecs · contaminatedWHEN WE STARTED THE BLEED AIR THE AIRPLANE FILLED UP WITH THICK SMOKE. BOTH THE CABIN AND THE COCKPIT. ACCOMPLISHED APU GROUND RUN. VERIFIED OIL SMELL PRESENT IN COCKPIT/CABIN DUCTS. VISUALLY INSPECTED BLEED DUCTS AT APU, L/H AND R/H BLEED VALVES IN AFT MAINTOct 22, 2021 · N380QS · Cessna 680CE · Cabin Cooling SystemSDR DXTA2020083104036Seal · damagedLANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. COMPLIED WITH QRH AND RETURNED FOR LANDING WITH NORMAL PROCEDURES. NO UNSAFE MESSAGES NOTED. THE AMBER WOW MISCOMPARE MESSAGE APPEARED FOR 20 SEC IN THE DOWNWIND AND WENT AWAY. SIGN OFF. TROUBLESHOT SYSTEM TOAug 31, 2020 · N380QS · Cessna 680A · Nose/Tail Landing Gear Strut/AxleSDR 2019FA0000200Truss · corrodedAPU TRUSS CORRODED. ACCOMPLISHED REPAIR TO APU TRUSS IAW ENGINEERING MEMO DQ21989RR1Jun 26, 2019 · N380QS · Cessna 680A · APU Cowling/ContainmentSDR 2019F00228Cowling · chafedLH ENGINE UPPER COWL CHAFE. REFERENCE MANUFACTURER DOCUMENT S-750-ATA51/01RD REV. A. AND ENGINEERING MEMO DQW21934M1Jun 25, 2019 · N380QS · Cessna 680A · Engine Cowling SystemSDR JGVR20180711002Frame · corrodedBLENDED CORRODED AREAS ON UPPER FRAME IN THE NOSE WHEEL WELL AT FS 77 LOCATED UNDER AND AROUND HYDRAULIC FEED THROUGH FITTINGS, PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED TO ENGINEERING FOR DISPOSITION. CLEANED, TREATED AND PRIMED BARE METAJul 11, 2018 · N380QS · Cessna 680CE · Fuselage Main, FrameSDR JGVR20180711001Spar · corrodedBLENDED CORRODED AREA ON THE RT WING CENTER SPAR INBRD WEB FORWARD FACE AT HYDRAULIC LINE FEED THROUGH RWS 40.62, PERFORMED ULTRASONIC AND EDDY CURRENT INSPECTIONS AND REPORTED FOR DISPOSITION. CLEANED, TREATED, AND TOPCOATED AREA PER REPAIR MEMO.Jul 11, 2018 · N380QS · Cessna 680CE · Wing SparSDR EBVR201707060001Skin · corrodedCORROSION NOTED ON THE LT UPPER AND LOWER BUCKETS AS WELL AS THE RT UPPER. ALL AREAS WERE ON THE OUTER SKINS. AREA BLENDED AND NDT PERFORMED CONFIRMING ALL CORROSION REMOVED.Jul 6, 2017 · N380QS · Cessna 680SOV · Engine Thrust ReverserSDR DXTR20170424017Skin · corrodedLEFT ELEVATOR HAS CORROSION ON UPPER SIDE. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF THE RT ELEVATOR AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED.Apr 17, 2017 · N380QS · Cessna 680CE · Elevator, Plate/SkinSDR DXTR20170424016Skin · corrodedRIGHT UPPER WING AT WS 54 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION AFTER BLENDING IAW NDI MANUAL 6-20-00-02. NO DEFECTS NOTED AT THIS TIME.Apr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR20170424013Skin · corrodedLEFT ELEVATOR HAS CORROSION ON BOTTOM SIDE. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL 6-20-00-02. NO DEFECTS NOTED AT THIS TIME.Apr 17, 2017 · N380QS · Cessna 680CE · Elevator, Plate/SkinSDR DXTR20170424012Skin · corrodedPANEL 352AB HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON PANELS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME. Apr 17, 2017 · N380QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR DXTR20170424011Skin · corrodedPANEL 352AC HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON PANELS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME.Apr 17, 2017 · N380QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR DXTR20170424010Skin · corrodedPANEL 351AC HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON PANELS AFTER BLENDING IAW CE-680 NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME.Apr 17, 2017 · N380QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR DXTR2017042406Thrust Reverser · corrodedLEFT ENGINE THRUST REVERSER HAS CORROSION AT THE 6 O'CLOCK POSITION. ACCOMPLISHED AN EDDY CURRENT INSPECTION IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED.Apr 17, 2017 · N380QS · Cessna 680CE · Engine Thrust ReverserSDR DXTR2017042405Thrust Reverser · corrodedLEFT ENGINE THRUST REVERSER HAS CORROSION AT THE 11 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED.Apr 17, 2017 · N380QS · Cessna 680CE · Engine Thrust ReverserSDR DXTR2017042404Thrust Reverser · corrodedRIGHT ENGINE THRUST REVERSER HAS CORROSION AT THE 9 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE RT T/R AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION.Apr 17, 2017 · N380QS · Cessna 680CE · Engine Thrust ReverserSDR DXTR2017042402Thrust Reverser · corrodedRIGHT ENGINE T/R HAS CORROSION AT THE 2 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE RT T/R AFTER BLENDING IAW 0 NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION.Apr 17, 2017 · N380QS · Cessna 680CE · Engine Thrust ReverserSDR DXTR2017042401Thrust Reverser · corrodedRIGHT ENGINE THRUST REVERSER HAS CORROSION AT THE 1 O'CLOCK POSITION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE RT THRUST REVERSER AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION.Apr 17, 2017 · N380QS · Cessna 680CE · Engine Thrust ReverserSDR DXTR2017042112Tail Cone · corrodedAPU EXHAUST TAIL CONE HAS CORROSION AT ZONE 331. REMOVED THE CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE APU TAILCONE AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED.Apr 17, 2017 · N380QS · Cessna 680CE · APU Exhaust SystemSDR DXTR2017042111Tail Cone · corrodedAPU EXHAUST TAIL CONE HAS CORROSION . REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS ON THE APU TAILCONE AFTER BLENDING IAW NDI MANUAL 6-20-00-02. NO DEFECTS NOTED AT THIS TIME.Apr 17, 2017 · N380QS · Cessna 680CE · APU Exhaust SystemSDR DXTR2017042110Latch · corrodedCARGO DOOR UPPER AFT LATCH HAS CORROSION. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION.680 NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION.Apr 17, 2017 · N380QS · Cessna 680CE · Cargo/Baggage DoorsSDR DXTR2017042109Skin · corrodedLEFT WING WS 78 IN ZONE 522 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME INApr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042108Skin · corrodedLEFT WING WS 75 IN ZONE 522 HAS CORROSION. REMOVED CORROSION AND POLISHED IAW CE-680 SRM 51-10-01.Apr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042107Skin · corrodedLEFT WING WS 72 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01.ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW CE-680 NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE ARApr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042106Skin · corrodedLEFT WING WS 53 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION.Apr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042105Skin · corrodedLEFT WING WS 49 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION.Apr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042104Skin · corrodedLEFT WING WS 43 IN ZONE 512 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN TApr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042103Skin · corrodedLEFT WING WS 27 IN ZONE 512 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION. Apr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042102Skin · corrodedRIGHT UPPER WING AT WS 57 ZONE 612 HAS CORROSION. REMOVED PAINT IAW MM 20-31-00. REMOVED CORROSION AND POLISHED IAW SRM 51-10-01. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TApr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017042101Skin · corrodedRIGHT UPPER WING AT WS 44.5 HAS CORROSION. ACCOMPLISHED EDDY CURRENT INSPECTION OF MULTIPLE AREAS AFTER BLENDING IAW NDI MANUAL PART 6-20-00-02. NO DEFECTS NOTED AT THIS TIME IN THE AREAS OF INSPECTION.Apr 17, 2017 · N380QS · Cessna 680CE · Wing, Plate/SkinSDR DXTR2017041201Thrust Reverser · corrodedLT & RT TR HAS MULTIPLE AREAS OF CORROSION, REPAIRED IAW AQRD ERO-890952. THIS REPAIR IS VALID FOR THE NOTED AMOUNT OF HOURS (500 HOURS), AFTER WHICH THE COMPONENT MUST BE REPLACED OR PERMANENTLY REPAIRED. THE DISCREPANT AREA MUST BE RE-INSPECTED AFTER 250 HOUApr 12, 2017 · N380QS · Cessna 680CE · Engine Thrust ReverserSDR DXTA2016F00178Trunnion · wornREPAIR OF OVERSIZED DOOR ROD PIN HOLE IN MLG TRUNNION. REPORT NR S-680-ATA32/02RD, DATED FEB 28, 2014 WITH FAA FORM 8100-9 DATED 3/7/2014.Sep 1, 2016 · N380QS · Cessna 680CE · Main Landing Gear Attach SectionSDR DXTA2015031205993Wheel · contaminatedHEAVY SMOKE FROM RT BRAKE ASSEMBLY OBSERVED. NO PERFORMANCE ISSUES NOTED. NO FLUID VISIBLE ON DECK. INSPECTED RT MLG WW FOR LEAKS & RT INBD & OTBD BRAKE FUSES, NO DEFECTS NOTED. INSPECTED RT MLG INBD & OTBD BRAKE ASSEMBLY'S FOR LEAKS & EVIDENCE OF POSSIBMar 11, 2015 · N380QS · Cessna 680CE · Landing Gear Brake SystemSDR DXTA2015021905983Pressure Switch · failedRED ENGINE LOW OIL PRESSURE CAS MESSAGE. OCCURRED DURING CLIMB AT APPROX 37,000 FEET. OIL PRESSURE GAUGE IN THE GREEN BAND. REMOVED LOW OIL PRESSURE SWITCH. INSTALLED NEW SERVICEABLE LOW OIL PRESSURE SWITCH IAW EMM 79-30-02. OPS & LEAK CHECKED GOOD.Feb 18, 2015 · N380QS · Cessna 680CE · Engine Oil PressureSDR DXTA2013011705247Hose · leakingUPON GEAR EXTENSION, HYD VOLUME LOW CAS MESSAGE POSTED. CYCLED ON AND OFF UNTIL TOUCHDOW. HYD FLUID IS VISIBLE FROM THE NOSE AND TRAILS THE ENTIRE LENGTH OF THE FUSELAGE. REMOVED AND REPLACED NOSE GEAR ACTUATOR FLEX HYDRAULIC EXTENSION LINE IAW MM 20-10-01. Jan 16, 2013 · N380QS · Cessna 680CE · Hydraulic System, MainSDR DXTR2011122900001Cable · damagedDURING NOSE WHEEL STEERING CHECK, THE TILLER WILL ONLY MOVE HALF WAY TO THE LEFT. IF YOU CONTINUE TO APPLY PRESSURE THERE IS A POP IN THE TILLER AND IT CONTINUES THE REMAINER OF TRAVEL TO THE LT.Dec 29, 2011 · N380QS · Cessna 680CE · Steering UnitSDR DXTA2011080804692Control Handle · failedAFTER TAKEOFF, LANDING GEAR HANDLE WAS STUCK IN DOWN POSITION WITH 3 GREEN & NO RED. MADE AN UNEVENTFUL LANDING. MX ATTEMPTED TO RAISE GEAR. GEAR HANDLE WOULD NOT MOVE FROM DETENT. FOUND GEAR HANDLE WOULD RELEASE FROM DETENT ONLY WHEN SHAKEN. REINSTALLED GEAAug 5, 2011 · N380QS · Cessna 680CE · Landing Gear SelectorSDR DXTA2011071904661Hose · leakingDURING CLIMB, AMBER HYD PRESSURE LOW LT & RT AND HYD VOLUME LOW LIGHTS ILLUMINATED. ON POST FLIGHT, HYD FLUID PRESENT IN NOSE GEAR WELL AND ALONG BELLY OF ACFT. FOUND LEAK AT NOSE WHEEL STEERING UNIT HOSE. REMOVED HOSE. INSTALLED NEW HOSE. BLED HYD AND NOSEJul 18, 2011 · N380QS · Cessna 680CE · Hydraulic System, MainSDR DXTA2011063004638Acm · failedON TAXI OUT, GREY/WHITE SMOKE WAS NOTICED IN COCKPIT ALONG WITH A ODOR OF HOT METAL. APU WAS RUNNING AND APU BLEED VALVE AND ENGINE BLEED VALVES WERE OPEN. REMOVED FAULTY ACM COOLING TURBINE. INSTALLED O/H ACM COOLING TURBINE. OPS CHECK AND LEAK CHECK GOOD.Jun 29, 2011 · N380QS · Cessna 680CE · Cabin Cooling SystemSDR DXTA2011062004624O-Ring · cutTAXIED OUT FROM FBO, WITH APU RUNNING, WITH BLEED AIR ON. GOT TO THE END OF RUNWAY, NEXT FOR TAKEOFF WHEN A LIGHT BLUE COLORED SMOKE STARTED TO FILL THE COCKPIT AND CABIN. TURNED BOTH BLEEDS OFF RETURNED TO GATE, SMOKE DISSAPATED. REPLACED WATER SEPARATOR Jun 19, 2011 · N380QS · Cessna 680CE · APU Oil SystemSDR DXTA2010041904069Landing Gear · malfunctionedUPON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. SHORTLY AFTER, HAD A WOW MISCOMPARE AMBER CAS. GEAR HANDLE WOULD NOT RAISE. JACKED ACFT AND FOUND NOSE GEAR NOT FULLY EXTENDING TO MAKE NOSE GEAR SQUAT SWITCH. CONTACTED MX, REQUESTED TO REPACT AND SERVICE NOSE SApr 18, 2010 · N380QS · Cessna 680CE · Landing Gear Retraction/Extension SystemSDR DXTA2010040704062Trim System · failedIMMEDIATELY AFTER TAKEOFF, WERE UNABLE TO TRIM THE ACFT NOSE DOWN. AFTER A FEW MOMENTS WE RECEIVED THE "PRIMARY STAB TRIM FAIL" CAS MESSAGE. SECONDARY TRIM FUNCTIONED NORMALLY. R & R STAB TRIM PCB NC107. R & R PRIMARY STAB TRIM ACTUATOR. RIG AND OPS CHECK GOApr 6, 2010 · N380QS · Cessna 680CE · Stabilizer Control SystemSDR DXTA2009090403772Bracket · damagedAUTOPILOT/YAW DAMPER DISENGAGED ON IT'S OWN IN FLIGHT AND COULD NOT RE-ENGAGE. YAW DAMP WAS ABLE TO RE-ENGAGE INTERMITTENTLY ON 'B' CHANNEL ONLY. REMOVED AND REPLACED AILERON SERVO BRACKET IAW MM CHA 22-10-00. TENSION, RIGGED, OPS CHECKED GOOD.Sep 3, 2009 · N380QS · Cessna 680CE · Fuselage Miscellaneous Structure
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