N323QS

Service difficulty reports · 69

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 = 'N323QS' 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.

SDR DXTA2026062308517Engine · making metalENROUTE AT FL410, RT ENG OIL PRESSURE BEGAN SLOWLY DECAYING UNTIL OIL PRESSURE LOW RT CAS ILLUM, FOLLOWED BY A ENG VIBRATION RT CAS. SUBSEQUENTLY SHUT DOWN RT ENG IAW QRH & DIVERTED TO KAPA. CHIP DETECTOR. METAL, SLUDGE & COKE PRESENT. LP & HP ROTATE FREELYJun 20, 2026 · N323QS · Cessna 680SOV · Engine (Turbine/Turboprop)SDR DXTA2026052608183Brake · faultedAFTER TOUCHDOWN WHEN APPLYING BRAKES GRADUALLY BETWEEN 70 AND 80KTS THE LEFT MAIN BRAKE STARTS GRABBING AND SHIMMERING NOTICEABLY. WHEN BELOW ANTI SKID SPEED NO GRABBING NOR SHIMMERING IS OCCURRING. INSPECTED LT INBD AND OTBD BRAKE, WHEEL ASSEMBLIES AND SURMay 21, 2026 · N323QS · Cessna 680SOV · Landing Gear Brake SystemSDR JGVR20250926001Skin · damagedMECHANICALLY BLENDED 8 AREAS ON RT H-STAB LOWER SKIN ON THE AFT EDGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED , TREATED, PRIMED AND TOP COATED AREAS PER NETJETS REQUEST FOR TECHNICAL DISPOSITION REPORT.Sep 26, 2025 · N323QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR DXTA2025062704035Battery Pack · unserviceableMULTIPLE EMERGENCY LIGHTS IN THE CABIN AND EXTERIOR NOT ILLUMINATING WHEN EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. RAN APU FOR 45 MINUTES TO CHARGE BATTERY PACKS, WITH NO SUCCESS. REMOVED # 1 EMERGENCY BATTERY, REMOVED #1 EMERGENCY BATTERY, INSTALLED REPJun 24, 2025 · N323QS · Cessna 680SOV · Emergency LightingSDR DXTA2025040202863Battery · inoperativeFORWARD CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITION. AFT CABIN EMERGENCY LIGHTS DO ILLUMINATE. CORRECTIVE ACTION: TROUBLESHOT EMERGENCY LIGHTING SYSTEM AND VERIFIED THAT THE CABIN DOOR EXIT LIGHT AND FWD RH WORK SURFACE LIGHT WMar 30, 2025 · N323QS · Cessna 680SOV · Emergency LightingSDR 2025F00077Nut Plate · corrodedFOUND 8 NUTPLATES WITH CORROSION LOCATED INSIDE OF PANEL 154BC. NUT PLATES HOLD ON THE MED SPADE DOOR. REMOVED EXISTING MED SPADE DOOR AND 8 NUTPLATES FOR ACCESS. MECHANICALLY BLENDED AREAS OF CORROSION IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYONMar 25, 2025 · N323QS · Cessna 680A · Passenger/Crew DoorsSDR JGVR20250324001Skin · corrodedFOUND THE EMERGENCY EXIT DOOR CORRODED OUTER SKIN ALONG CONTOUR RING EDGE AREA, REMOVED CONTOUR RINGS AND FOUND ADDITIONAL AREAS OF CORROSION. SENT DOOR OUT FOR REPAIRS. NOTE: EMERGENCY EXIT DOOR P/N 6911251-4.Mar 24, 2025 · N323QS · Cessna 680CE · Emergency ExitsSDR 2025F00075Spar · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED IN LH MLG WHEEL WELL, AFT SPAR, LOWER CLIP IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLENDS IAW Mar 21, 2025 · N323QS · Cessna 680A · Wing SparSDR 2025F00073Spar · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION FROM RH WING AFT SPAR, FWD FACE IN RH MLG WHEEL WELL. EVALUATED AND FOUND BLENDED AREAS WERE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLENMar 21, 2025 · N323QS · Cessna 680A · Wing SparSDR 2025F00072Lug · corrodedREMOVED RH MIDDLE FLAP ASSEMBLY TO WORK CORROSION ON FWD, OUTBD LUG. MECHANICALLY REMOVED RH MIDDLE FLAP ROLLER, OUTBD LUG CORROSION, INBD SURFACE IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING .002" OF MATERIMar 21, 2025 · N323QS · Cessna 680A · Trailing Edge FlapsSDR 2025F00074Tail Cone · corrodedMECHANICALLY REMOVED 4 AREAS OF CORROSION LOCATED ON TAILCONE SERVICE DOOR FRAME ASSEMBLY WITH ADDITIONAL 4 AREAS OF CORROSION AFTER FRAME ASSEMBLY WAS REMOVED IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING .Mar 21, 2025 · N323QS · Cessna 680A · Aerodynamic FairingsSDR JGVR20250320007Skin · corrodedREPAIRED 2 AREAS OF CORROSION LOCATED ON LH HORIZONTAL STABILIZER UPPER SKIN FORWARD OF PANEL 351AC, BY BLENDING CORROSION, PERFORMING NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS ENGINEERING ORDER BY CLEANING, TREATING, AND PRIMING AREMar 20, 2025 · N323QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR JGVR20250320006Skin · corrodedREPAIRED THE LH UPPER WING SKIN LOCATED UNDER AND ADJACENT TO THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING STRUCTURE) BY BLENDING CORROSION, PERFORMING NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER TEXTRON FIELD REPAIR BY CLEANING, TREATING, ANDMar 20, 2025 · N323QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20250320005Stringer · corrodedMECHANICALLY BLENDED CORROSION FROM CORROSION FROM CENTER STRINGER UNDER PANELS 154AC AND 154BC, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 20, 2025 · N323QS · Cessna 680CE · Fuselage Main, Longeron/StringerSDR JGVR20250320004Skin · corrodedMECHANICALLY BLENDED CORROSION FROM LH OVER-WING FUEL ADAPTER LAND., PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 20, 2025 · N323QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20250320003Skin · corrodedREMOVED NUT PLATES FROM PANELS LANDS TO ACCESS CORROSION AND MECHANICALLY REMOVED ALL AREAS OF CORROSION BEHIND VERTICAL STABILIZER PANELS 341ER, 341DR, 341CR, 341BR, AND 341AR, 341AL, 341BL, 341CL, AND 341DL, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITIONMar 20, 2025 · N323QS · Cessna 680CE · Vertical Stabilizer, Plate/SkinSDR JGVR20250320002Skin · corrodedBLENDED AREAS OF CORROSION LOCATED ON UPPER EXTERIOR FUSELAGE SKIN IN ZONE 254, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 20, 2025 · N323QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR JGVR20250320001Skin · corrodedBLENDED 5 AREAS OF CORROSION LOCATED ON EXTERIOR FUSELAGE SKIN ALONG THE SEAM NEXT TO THE PILOT DV WINDOW IN ZONE 243 ALONG SEAM, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, Mar 20, 2025 · N323QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR 2025F00059Spar · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON RH GEARWELL AFT SPAR, FWD FACE, LOWER CLIP, INBD OF WS 37.00 IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINALMar 13, 2025 · N323QS · Cessna 680A · Wing SparSDR JGVR20250306003Lug · corrodedBLENDED CORRODED AREAS FROM THE OUTBOARD ROLLER LUG OF THE RH WING MIDDLE FLAP, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 6, 2025 · N323QS · Cessna 680CE · Wing, Control Surface Attach FittingsSDR JGVR20250306002Skin · corrodedBLENDED CORRODED AREA ON THE RH UPPER WING SKIN, JUST AFT OF THE LEADING EDGE AND OUTBOARD OF THE WING WALK, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING Mar 6, 2025 · N323QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20250306001Skin · corrodedBLENDED 6 AREAS OF CORROSION ON THE RH LOWER OUTBOARD WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 6, 2025 · N323QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20250303006Skin · corrodedBLENDED 6 AREAS OF CORROSION ON LH UPPER WING (INBOARD WING) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 3, 2025 · N323QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20250303005Skin · corrodedBLENDED 15 AREAS OF CORROSION ON LH UPPER WING IN ZONES 551 AND 552 (OUTBOARD WING) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 3, 2025 · N323QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20250303004Structure · corrodedBLENDED ONE AREA OF CORROSION FROM LH LOWER WING FORWARD OF THE AILERON, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 3, 2025 · N323QS · Cessna 680CE · Wing StructureSDR JGVR20250303003Structure · corrodedMECHANICALLY REMOVED CORROSION LOCATED AROUND LH OVERWING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER TEXTRON REPAIR MEMO BY CLEANING, TREATING, AND PRIMING AREAS.Mar 3, 2025 · N323QS · Cessna 680CE · Wing StructureSDR JGVR20250303002Rib · corrodedREMOVED EMERGENCY BRAKE LINES AND CARRY THROUGH FITTINGS FROM RH AND LH RIBS AT WS 37, BLENDED CORRODED AREAS, PERFORMED, NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMMar 3, 2025 · N323QS · Cessna 680CE · Wing StructureSDR JGVR20250303001Structure · corrodedMECHANICALLY REMOVED CORROSION LOCATED AROUND RH OVERWING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAID AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 3, 2025 · N323QS · Cessna 680CE · Wing StructureSDR DXTA2025010701863Battery · no testFAILED TO TEST ON PREFLIGHT. LIGHTS DO NOT ILLUMINATE IN ARM POSITION. LIGHTS FUNCTION NORMALLY WHEN SELECTED ON. PERFORMED EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. OPS CHECK GOOD. IAW TC-FLT-33-1001.Jan 6, 2025 · N323QS · Cessna 680SOV · Emergency LightingSDR DXTA2024100100707Precatch · out of rigMAIN DOOR PRE CATCH NOT FLUSH WITH PANEL. ON LAST LEG DOOR WOULD NOT CATCH. CORRECTIVE ACTION: EVALUATED THE PRECHATCH SYSTE. SYSTEM IS COMPLETELY FUNCTIONAL 5/5 CHECKS SATISFACTORY . HANDLE DOES NOT SIT FLUSH AS REPORTED . FROM EVALUATION IT LOOKS AS IF THE HSep 29, 2024 · N323QS · Cessna 680SOV · Passenger/Crew DoorsSDR DXTA2024080600117Door · excess playTHE MAIN CABIN DOOR HAS APPROXIMATELY TWO TO THREE INCHES OF PLAY IN IT WHEN IT IS FULLY DOWN AND LOCKED. FOUND THE OVER CENTER PUSHROD LOOSE. RESECURED THE PUSHROD AND OPERATED THE DOOR SEVERAL TIMES AND FOUND IT SATISFACTORY. WORK DONE IAW CE-680 AMM 51-1Aug 6, 2024 · N323QS · Cessna 680SOV · Passenger/Crew DoorsSDR 2023FA0000598Spar Cap · corrodedNJA CORROSION FOUND ON LEFT-AFT-VERTICAL-STAB SPAR CAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING MEMO DQ41418M1 DATED 10/5/2023.Oct 12, 2023 · N323QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR DXTA2023081492850Unknown · unknownAPU (EXCEPT GENERATOR): IN FLIGHT AT 25,000FT WITH APU ON WITH MAX AIR SELECTED , A STRONG ODOR IN CABIN . TURNED APU OFF AND ODOR VERY SLOWLY DISSIPATED. ODOR DID NOT SMELL ELECTRICAL OR OILY. COMPUED WITH NJA TASK CARDS, THE COALESCER WAS A LLTTLE DIRTY •Aug 11, 2023 · N323QS · Cessna 680CE · Airborne Auxiliary Power Unit (APU) SystemSDR JGVR20210520006Spar · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON VERTICAL STAB, AFT SPAR, LH SPAR CLIP JUST BELOW LOWER CROSS MEMBER. FOUND CORROSION EXCEEDING C680 SRM 51-70-02 LIMITATIONS AND SUBMITTED TO TEXTRON ENGINEERING FOR REPAIRS. REPAIRED CORROSION IAW TEXTRON ENGINEERING May 20, 2021 · N323QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR JGVR20210520005Skin · corrodedBLENDED 2 AREAS OF CORROSION ON UPPER AFT EDGE OF RH VERTICAL STAB SKIN. FOUND CORROSION REMOVED TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02. REPAIR CORROSION PER TEXTRON REPAIR MEMO DQ29966M1, SUBJECT "RIGHT-HAND VERTICAL STABILIZER SKIN CORROSION", DATEDMay 20, 2021 · N323QS · Cessna 680CE · Vertical Stabilizer, Plate/SkinSDR JGVR20210520004Skin · corrodedBLENDED CORROSION ON LOWER FUSELAGE SKIN AROUND TCAS ANTENNA CARRY THRU CONNECTORS. FOUND CORROSION TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02. REPAIRED CORROSION ON LOWER FUSELAGE SKIN AROUND TCAS ANTENNA CARRY THRU CONNECTOR PER TEXTRON REPAIR MEMO DQ 2May 20, 2021 · N323QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR JGVR20210520003Skin · corrodedFOUND CORROSION GOING UNDER RH WING AFT DRAG ANGLE. FOUND ADDITIONAL 80 AREAS OF CORROSION UNDER DRAG ANGLE. MECHANICALLY REMOVED 94 AREAS OF CORROSION FROM RH WING AFT DRAG ANGLE AREA IAW CESSNA 680 SRM 51-70-02. EVALUATED REMAINING THICKNESS AND FOUND TO BE May 20, 2021 · N323QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20210520002Spar · corrodedMECHANICALLY BLENDED CORROSION FROM RUDDER COVE ON VERTICAL STAB AFT SPAR RH CLIP IAW CESSNA 680 SRM 51-70-02. REFER TO SQK 103-2 OF THIS WO FOR NDT. EVALUATED REMAINING THICKNESS AND FOUND TO BE OUT OF LIMITS. SUBMITTED INFO TO ENGINEERING. COMPLIED WITH TEXTMay 20, 2021 · N323QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR JGVR20210520001Torque Tube · crackedREMOVED CRACKED RUDDER TORQUE TUBE P/N UNKNOWN FROM RUDDER P/N 6933000-19 S/N 0134 AND INSTALLED NEW CUSTOMER SUPPLIED RUDDER TORQUE TUBE P/N 6933025-55 PER CESSNA 680 SRM 51-40-03, 51-40-06, 55-40-09, CSPM 20-40-20.May 20, 2021 · N323QS · Cessna 680CE · Rudder StructureSDR JGVR20210113001Panel · corrodedBLENDED 1 AREA OF CORROSION ON TOP OF LT HORIZONTAL STAB JUST FORWARD OF WEDGE PANEL 351AC (INBOARD OF THE LT ELEVATOR) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED PER TEXTRON ENGINEERING MEMO.Jan 13, 2021 · N323QS · Cessna 680A · Horizontal Stabilizer, Plate/SkinSDR DXTA2020092004111Spring · brokenMAIN CABIN DOOR HEAVY TO CLOSE. CABIN DOOR MAKES NUMEROUS CREAKING NOISES AS IT CLOSES. REMOVED AND REPLACED BOTH LUBRICATED SPRINGS DUE TO BROKEN AND CRACKED SPRINGS. RIGGED CABLE TENSIONS, OPERATIONS CHECK GOOD, DOOR CLOSES MUCH EASIER. ALL WORK DONE, IASep 20, 2020 · N323QS · Cessna 680A · Passenger/Crew DoorsSDR DXTA2020081413965Element · damagedSHORT FINAL GOING TO EGE AIRPORT. APROX 8000 FT. EMERGENCY PRESS, ACM BLEED LEAK, BAGGAGE HEAT FAIL AND POSSIBLE ACM OVER TEMP MESSAGE COME ON AND WENT OUT. ELECTRICAL BURNING SMELL, WAS NOTICED SHORTLY AFTER. LANDED UN EVENTFULLY. RAN CHECK LIST FOR ACM BAug 11, 2020 · N323QS · Cessna 680CE · Air Conditioning SystemSDR DXTA2020081213965Warning System · multiple failSHORT FINAL GOING TO AIRPORT. APROX 8000 FT. EMERGENCY PRESS, ACM BLEED LEAK, BAGGAGE HEAT FAIL AND POSSIBLE ACM OVER TEMP MESSAGE COME ON AND WENT OUT. ELECTRICAL BURNING SMELL, WAS NOTICED SHORTLY AFTER. LANDED UN EVENTFULLY. RAN CHECK LIST FOR ACM BLEEDAug 11, 2020 · N323QS · Cessna 680CE · Central WarningSDR JGVR20200807003Hinge Bracket · corrodedBLENDED CORRODED AREA ON THE LOWER HINGE BRACKET OF THE MIDDLE RUDDER HINGE ON THE VERTICAL STABILIZER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED CORRODED PART WITH NEW HINGE PLATE P/N 6931050-60 PER CESSNA 680 SRM 51-40-03, 51-40-06, 51-40-0Aug 7, 2020 · N323QS · Cessna 680CE · Rudder StructureSDR JGVR20200807002Spar Cap · corrodedBLENDED, PERFORMED NDT AND TREATED CORRODED AREAS ON THE LH HORIZONTAL STABILIZER SPAR CAP IAW REPAIR MEMO.Aug 7, 2020 · N323QS · Cessna 680CE · Horizontal Stabilizer, Spar/RibSDR JGVR202008070001Spar Cap · corrodedBLENDED, PERFORMED NDT AND TREATED CORRODED AREAS ON THE LT WING AFT SPAR LOWER CAP, LOCATED BEHIND ACCESS PANEL 730DL, IAW REPAIR MEMO.Aug 7, 2020 · N323QS · Cessna 680CE · Wing SparSDR DXTA2019021200010Drain · leaking1) HYDRAULIC FLUID LEAK - COMPLETE LEFT AND RIGHT HYDRAULIC FLUID LOSS OCCURRED AFTER TAKEOFF WITH GEAR RETRACTED. POSTFLIGHT REVEALED HYDRAULIC FLUID COMING FROM RIGHT ENGINE DRAIN MAST. NO HYDRAULIC FLUID VISIBLE AROUND LEFT OR RIGHT MAIN LANDING GEAR. 2) Feb 11, 2019 · N323QS · Cessna 680A · Hydraulic System, MainSDR DXTA2018080301257Control Unit · malfunctionedRAISED LANDING GEAR AND THE NOSE GEAR DID NOT RETRACT, AS INDICATED BY A GREEN NOSE GEAR LIGHT, THE RED UNLOCK LIGHT, AND AERODYNAMIC NOISE WITH THE GEAR HANDLE SELECTED UP. WE CYCLED THE GEAR AND IT EXTENDED AND RETRACTED NORMALLY. GEAR EXTENSION FOR LANDING Aug 2, 2018 · N323QS · Cessna 680SOV · Landing Gear Steering SystemSDR DXTA2018060801053Shutoff Valve · failedCLIMBING THROUGH FL400, AN ODOR WAS NOTICED BY CREW, FOLLOWED BY VISUAL SMOKE IN BOTH THE CABIN AND COCKPIT. SHORTLY AFTER, TWO AMBER CAS MESSAGES FOR ACM OVERTEMP AND EMERGENCY PRESSURIZATION ILLUMINATED. EMERGENCY DESCENT WAS ACCOMPLISHED ALONG WITH COMPLIAJun 7, 2018 · N323QS · Cessna 680CE · Cabin Cooling SystemSDR DXTA2018022800072Frame · crackedNLG FRAME CRACK. ACCOMPLISHED ENGINEERING LETTER DQ11281M1 DATED FEB 23, 2018, 680-0134 NLG RIGHT SIDE FRAME (P/N 6713072-31) CRACK.Feb 28, 2018 · N323QS · Cessna 680SOV · Fuselage Main, Frame
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