N357QS

Service difficulty reports · 75

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 = 'N357QS' 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 DXTA2026071508821Spring · brokenDOOR HELPER CABLE AND LIFTING MECHANISM SEEMS TO BE STUCK OR NOT WORKING. CABLE IS LOOSE AND DOOR IS UNDER ITS OWN WEIGHT. REMOVED MED STEPS, DISCONNECTED STEP LIGHT ELECTRICAL, REMOVED TRIM, AND TOP STEP. DISPLACED MED STEP TO GAIN ACCESS TO AFT BROKEN SUPPJul 14, 2026 · N357QS · Cessna 680SOV · Passenger/Crew DoorsSDR DXTA2026061008391Light · malfunctionedDURING PREFLIGHT FOUND EMERGENCY LIGHTS INOP. NUMEROUS CABIN EMERGENCY LIGHTS INOP AND ALL BUT ONE EXTERIOR LIGHT INOP. GAINED ACCESS TO AIRCRAFT, EMER LIGHT TOGGLE SWITCH WAS IN THE OFF POSITION. PRIOR TO CHARGING EMER BATTERIES, CYCLED EMER LIGHT TOGGLE SWJun 9, 2026 · N357QS · Cessna 680SOV · Emergency LightingSDR DXTA2026031307235Wire · unsecureREAR AND LAV EMER EXIT SIGN NOT ILLUMINATED. RESERCHED CE-680 WIRE DIAGRAM BUT SHOWED LIMITED INFORMATION. CONTACTED MCC AND ASKED FOR ADDITIONAL WIRE: REFRENCES THAT WE DO NOT HAVE ACCESS TO. RECIVED REFRENCES AND DETERMINTED DISCREPANCY LEAD TO #4 EMERGEMar 12, 2026 · N357QS · Cessna 680SOV · Light System WiringSDR DXTA2025102705425Battery Pack · faultyPREFLIGHT - PORTION/ALL OF CABIN EMERGENCY LIGHTING IS INOP. HERE ARE ALL THE CONDITIONS: APU OFF -EMER LTS SWITCH IN ON (MAIN BATTERIES OFF) - ALL EMER LIGHTS FUNCTION EXCEPT THE 3 EXIT SIGNS AROUND MED AND GALLEY READ LIGHT (BULB IS GOOD) -EMER LTS SWITCH IOct 24, 2025 · N357QS · Cessna 680SOV · Emergency LightingSDR 2025F00214Skin · damagedREPAIRED CORROSION UNDER THE BAGGAGE FLOOR BOARDS ON THE TAILCONE SKIN AND STRINGERS BETWEEN FS 501.25 AND FS 548.50 PER AQRD ERO-985795 REV.A, TITLED "N357QS TAILCONE SKIN CORROSION" DATED AUG 28, 2025. SUPPORTED BY FAA FORM 8110-3 DATED 08/28/2025. THE FATIGAug 29, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/SkinSDR 2025F00201Skin · corrodedMECHANICALLY BLENDED 7 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS534.70 AND FS548.50 IAW SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEEDING 0.002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSIAug 26, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/SkinSDR 2025F00200Skin · corrodedMECHANICALLY BLENDED 12 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS519.37 AND FS534.70 IAW SRM 51-70-02. FOUND 10 AREAS OF CORROSION BLENDING TO BE WITHIN LIMITS IAW SRM 51-70-02. PROTECTED BARE METAL IAW C680 SRM 51-20-01. THIS IS A PSE AREAug 26, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/SkinSDR 2025F00199Skin · corrodedMECHANICALLY BLENDED 17 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS468.05 AND FS484.65 IAW SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEEDING 0.002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSIOAug 26, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/SkinSDR 2025F00198Structure · corrodedMECHANICALLY BLENDED 7 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS501.25 AND FS519.37 IAW SRM 51-70-02. FOUND 5 AREAS OF CORROSION BLENDING TO BE WITHIN LIMITS IAW SRM 51-70-02. PROTECTED BARE METAL IAW C680 SRM 51-20-01. THIS IS A PSE AREA IAug 26, 2025 · N357QS · Cessna 680A · Fuselage Miscellaneous StructureSDR 2025F00188Skin · corroded1 AREA OF CORROSION FOUND ON E-EXIT OUTER SKIN, UPPER /AFT CORNER. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON E-EXIT, EXTERIOR SKIN, UPPER AFT CORNER AREA IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND SRM LIMITS IAW C680 SRM 51-70-02 EXCEEAug 11, 2025 · N357QS · Cessna 680A · Emergency ExitsSDR DXTA2025042503175Acm · faultedCONCURRENT WITH FULL HOT ENVIROMENTAL AIR DISCREPANCY, A STRONG BURNING ODOR WAS NOTED BY BOTH CREWMEMBERS PERMEATING BOTH THE CABIN AND COCKPIT COMPARTMENTS. AGREED ON ODOR DESCRIPTION AS RESEMBLING THAT OF A "BURNT PLASTIC SMELL." STRENGTH DIMINISHED NOTICEAApr 22, 2025 · N357QS · Cessna 680SOV · Cabin Cooling SystemSDR JGVR20250109001Fitting · corrodedREMOVED CORROSION LOCATED AROUND SPOILER PRESSURE HYDRAULIC LINE FITTING AND SPOILER RETURN HYDRAULIC LINE CARRY THRU FITTINGS ON LH AND RH WING AFT SPARS, AFT FACE, JUST INBD OF JACK POINT, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED BLENDS IAJan 9, 2025 · N357QS · Cessna 680CE · Hydraulic System, MainSDR JGVR20241216001Spar · damagedR&R FASTENERS AS REQUIRED, BLENDED 9 AREAS OF CORROSION ON LH WING AFT SPAR, LOWER CLIP, FWD SIDE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED BLENDED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.Dec 31, 2024 · N357QS · Cessna 680CE · Wing SparSDR JGVR20240611001Skin · corrodedBLENDED CORRODED AREAS OF THE FUSELAGE SKIN JUST AFT OF THE MAIN ENTRY DOOR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOPCOATED AREA PER TEXTRON FILED REPAIR.Jun 11, 2024 · N357QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR JGVR20240610002Skin · corrodedREPAIRED CORRODED AREAS OF THE UPPER SKIN OF THE RH HORIZONTAL STABILIZER AT THE INBOARD AFT EDGE JUST FORWARD OF ACCESS PANEL 352AC AND AREA AT THE TRAILING EDGE OUTBOARD ELEVATOR AREA BY BLENDING, PERFORMING NDT, TREATING AND PRIMING IAW NETJETS REQUEST FOR Jun 10, 2024 · N357QS · Cessna 680CE · Horizontal Stabilizer StructureSDR JGVR20240610001Skin · damagedREPAIRED BENDED AREA OF FUSELAGE LH UPPER SKIN AT APPROXIMATELY FS 518.5 AND BL 0.0, TWO AREAS OF FUSELAGE RH UPPER SKIN AT APPROXIMATELY FS 464 AND BL 0.0, AND ONE AREA FS 517 AND BL 0.0 BY BLENDING, PERFORMING NDT, TREATING AND PRIMING AREAS FOUND ACCEPTABLEJun 10, 2024 · N357QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR JGVR20240607001Skin · corrodedREPAIRED THE RH WING UPPER INBOARD SKIN BY BLENDING CORRODED AREAS LOCATED UNDER AND ADJACENT TO THE DRAG ANGLES (WING-TO-FUSELAGE FAIRING AREA), PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH AEJun 7, 2024 · N357QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20240606001Angle · corrodedMECHANICALLY REMOVED 4 AREAS OF CORROSION ON LH SIDE OF RUDDER COVE ON VERTICAL STAB SPAR CLIP AND 1 AREA OF CORROSION EXTENDING UNDERNEATH CROSS BRACKET SUPPORT LH SIDE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS AS REQUIREDJun 6, 2024 · N357QS · Cessna 680CE · Vertical Stabilizer Miscellaneous StructureSDR JGVR20240605001Skin · damagedREPAIRED THE TAILCONE SKINS LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER, FILLER, AND SHIM IN ACCORDANCE WITH TEXTRON FIELD REPAIRJun 5, 2024 · N357QS · Cessna 680CE · Aerodynamic FairingsSDR JGVR20240604003Skin · damagedBLENDED CORRODED AREA ON THE UPPER SURFACE OF THE UPPER INBOARD SKIN ON THE LH WING, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION, TREATED, PRIMED AND TOPCOATED BLENDED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.Jun 4, 2024 · N357QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20240604002Skin · damagedREPAIRED LH VERTICAL STABILIZER SKIN AT THE OPENINGS OF ACCESS PANELS 341AL, 341BL, 341CL, AND 341DL BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATED AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH AEROSPACE QUALITY REJun 4, 2024 · N357QS · Cessna 680CE · Vertical Stabilizer, Plate/SkinSDR JGVR20240604001Skin · damagedREPAIRED THE LH SKIN OF VERTICAL STABILIZER AT THE UPPER AFT CORNER BY BLENDING CORRODED AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH AND DEVELOPMENT ENGINEERINGJun 4, 2024 · N357QS · Cessna 680CE · Vertical Stabilizer, Plate/SkinSDR JGVR20250110001Fitting · corrodedREPAIRED CORROSION AROUND LH AND RH EMERGENCY BRAKE RIB FEED THRU FITTINGS AT WS 37 BY FABRICATING AND INSTALLING REPAIR DOUBLERS PER AEROSPACE QUALITY RESEARCH AND DEVELOPMENT ENGINEERING REPAIR ORDEROct 5, 2023 · N357QS · Cessna 680CE · Wing Main, Frame StructureSDR DXTA2023030381570Battery · dischargedON POSTFLIGHT, NOTICED EXTERIOR EMERGENCY LIGHT ILLUMINATING THE AIRSTAIR DOES NOT ILLUMINATE ON EMERGENCY BATTERY POWER. IT WILL ILLUMINATE ON BATTERY/GENERATOR POWER, EITHER WITH THE ENTRY LIGHT SWITCH OR THE PAX SAFETY SWITCH. *** CORRECTIVE ACTION *** REMOMar 1, 2023 · N357QS · Cessna 680CE · Emergency LightingSDR 2023FA0000099Spar · corrodedCORROSION - EXFOLIATION FOUND IN LOWER SPAR OF LH AND RH MLG WHEEL WELLSFeb 24, 2023 · N357QS · Cessna 680CE · Wing SparSDR 3J7R2023010400001G Switch · activatedDURING MX CHECK FOUND EMER LIGHTS STAY ON WITH SWITCH IN ARM POSITIONJan 3, 2023 · N357QS · Cessna 680CE · Emergency LightingSDR DXTA2022112174380Warning Light · inoperativeUPON APPLYING TAKEOFF POWER FOR DEPARTURE, AROUND 50KTS IAS THE RIGHT THEN LEFT THRUST REVERSER EMERGENCY STOW SWITCH LIGHTS STARTED FLASHING. THEY WORKED FINE ON PREVIOUS LEGS AND WERE NOT TESTED BETWEEN LEGS IAW NORMAL PROCEDURE. FOLLOWED MEL PROCEDURE AND Nov 21, 2022 · N357QS · Cessna 680SOV · Engine Thrust ReverserSDR DXTA2022032959180I/O Card · faultedENGINE CONTROL FAULT L AMBER CAS: AT FL 380 GOT ENGINE CONTROL FAULT L. SUBSEQUENTLY FOLLOWING INDICATIONS WERE AMBER DASHES, N1L, OIL TEMPL, STAB TRIM, ,DC AMP, BATT AMP , HYD PRESS AFTER LOWERING GEAR RECEIVED ANTISKID FAIL CAS. RECEIVED REPAIRED CUSTOM Mar 29, 2022 · N357QS · Cessna 680CE · Fuel Controlling SystemSDR DXTA2021122954390None · brokenNLG LANDING GEAR EXTENSION: HAD AN UNSAFE NOSE GEAR INDICATION, RED UNLOCK LIGHT AND NO DOWN GREEN NOSE GEAR LIGHT. HAD 2 GREEN MAIN GEAR DOWN INDICATIONS. COMPLETED THE GEAR UNSAFE EMERGENCY PROCEDURE. THE NOSE GEAR WAS DOWN, LANDED UNEVENTFULLY.//SIGNOFF/Dec 28, 2021 · N357QS · Gulstm 680 · Landing Gear Retraction/Extension SystemSDR DXTA2021102150600Unknown · odorCOCKPIT ODOR: AN ODOR OF EXHAUST FUMES AFTER TAKEOFF UP TO 12,000 FEET WITH APU OFF. WHILE IN FLIGHT IF THE THROTTLES ARE ADVANCED CLOSE TO MCT WILL RECEIVE ODOR OF EXHAUST FUMES FOR APPROXIMATELY 20 TO 30 SECONDS THEN DISSIPATES. // SIGNOFF // AS REQUESTED ROct 20, 2021 · N357QS · Cessna 680CE · Air Distribution SystemSDR DXTA2021092449370Battery · defectiveCABIN EMERG LIGHT: PHOTO TAKEN WITH EMERGENCY LIGHT SELECTED OFF PRIMARY DOOR EXIT LIGHT AS YOU CAN SEE IS ILUMINATED AND WIRES HANGING DOWN ABOVE DOOR. PRELIMINARY TESTING OF THE LIGHTS DID NOT TEST PROPERLY AND WE ARE UNABLE TO EXTINGUISH EMERGENCY LIGHT OVESep 23, 2021 · N357QS · Cessna 680CE · Emergency LightingSDR DXTA2021092349340Battery · defectiveMAIN EXIT SIGN/LIGHT: EXIT LIGHT OVER MAIN CABIN DOOR AND BOTH EXIT SIGNS ON EITHER SIDE OF DOOR WILL NOT ILLUMINATE. ALSO EXIT SIGNS IN AFT CABIN AND ISLE LIGHTING EXTINGUISHES WHEN PAX SAFETY SWITCH IS ON. // SIGN OFF // ACCESSED AIRCRAFT, REMOVED CARPET FOSep 22, 2021 · N357QS · Gulstm 680 · Emergency LightingSDR DXTA2021031839600Coalescer Bag · odorCOCKPIT ODOR: STRONG OILY SMELL IMMEDIATELY AFTER TAKEOFF. NOTICED ON FIRST TAKEOFF OF THE DAY BUT AFTER SECOND TAKEOFF ODOR SMELLED WORSE. INSTALLED NEW CUSTOMER SUPPLIED COALSCER BAG P/N 98237-12. IAW CE-680 AMM 12-19-00. INSTALLED WATER SEPARATOR IAW CE-Mar 16, 2021 · N357QS · Cessna 680CE · Humidity Control SystemSDR JGVR20210302002Skin · corrodedONE AREA OF VERIFIED CORROSION ON VERTICAL STAB LH SKIN, NEAR TIP CAP. MECHANICALLY BLENDED ONE AREA OF CORROSION ON VERTICAL STAB LH SKIN, NEAR TIP CAP IAW CESSNA 680 SRM 51-70-02. PERFORMED NDT ON BLENDED AREA TO VERIFY CORROSION REMOVAL AND REMAINING MATERIMar 2, 2021 · N357QS · Cessna 680A · Vertical Stabilizer, Plate/SkinSDR JGVR20210302001Spar · corrodedONE AREA OF VERIFIED CORROSION IN THE RH WHEEL WELL, WING LOWER SPAR. MECHANICALLY BLENDED ONE AREA OF CORROSION ON RH WHEEL WELL, WING LOWER SPAR IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION DEPTHS EXCEEDING C680 SRM 51-70-02 LIMITATIONS OF .002". REPAIRED COMar 2, 2021 · N357QS · Cessna 680A · Wing SparSDR DXTA2020110404310Battery · defectiveAFTER TAKE-OFF WE GOT CAS MESSAGE BATTERY OTEMP L. ACCOMPLISHED EMERGENCY/ABNORMAL PROCEDURES CHECKLIST. LANDING GEAR WOULD NOT EXTEND. ACCOMPLISHED EMERGENCY/ABNORMAL CHECKLIST. PULLED LANDING GEAR BLOWDOWN HANDLE. REMOVED AND REPLACED LT MAIN BATTERY WINov 4, 2020 · N357QS · Cessna 680CE · Battery/Charger SystemSDR JGVR20201001001Skin · debondedVERTICAL STAB AFT SPAR LT UPPER ANGLE HAS 2 AREAS OF VERIFIED INTERGRANULAR CORROSION. MECHANICALLY BLENDED 2 AREAS ON VERTICAL STAB AFT SPAR LT UPPER ANGLE, IAW CESSNA 680 SRM 51-70-02. EVALUATED AREA AND FOUND TO BE OUT OF SRM LIMITS. PERFORMED TEXTRON FIOct 1, 2020 · N357QS · Cessna 680A · Wing, Plate/SkinSDR JGVR20201001006Nut Plate · corrodedFOUND CORROSION AROUND THE NUTPLATES FOR SEVERAL VERTICAL STABILIZER ACCESS PANELS. BLENDED CORRODED AREAS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS, PER TEXTRON REPAIR MEMO.Oct 1, 2020 · N357QS · Cessna 680CE · Vertical StabilizerSDR JGVR20201001005Bracket · corrodedFOUND TAILCONE AFT BRACE LT SIDE AND AFT BRACE LOWER MOUNTING BRACKET CORRODED. REPLACED WITH NEW CESSNA PARTS P/N 6912162-12, P/N 6912162-3, AND P/N 6912162-9.Oct 1, 2020 · N357QS · Cessna 680CE · Fuselage Main, Attach FittingsSDR JGVR20201001004Spar · damagedMECHANICALLY BLENDED ONE CORRODED AREA ON RT WING AFT SPAR, LOCATED IN RT MLG WHEEL WELL AT WS 30. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED REPAIR AREA, PER TEXTRON FIELD REPAIR.Oct 1, 2020 · N357QS · Cessna 680CE · Wing SparSDR JGVR20201001003Skin · corrodedFOUND SEVERAL AREAS OF CORROSION ON THE INTERIOR SURFACE OF THE LT TAILCONE BETWEEN FS 642 AND FS 672 AT STRINGER 13. BLENDED CORRODED AREAS, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED REPAIR AREAS, PER TEXTRON REPAIR MEMOOct 1, 2020 · N357QS · Cessna 680CE · Aerodynamic FairingsSDR JGVR20201001002Skin · corrodedFOUND THREE AREAS OF CORROSION ON THE EMERGENCY EXIT DOOR OUTER SKIN. REMOVED THE FWD AND AFT CONTOUR RINGS FROM THE DOOR ASSEMBLY FOR ACCESS AND FOUND AN ADDITIONAL 24 AREAS OF CORROSION. REPLACED CORRODED EMERGENCY EXIT DOOR WITH A REPAIR DOOR, CESSNA P/N Oct 1, 2020 · N357QS · Cessna 680CE · Emergency ExitsSDR 2019F00145Doubler · gougedREPAIR OF SCREW GOUGES, AFT CABIN, ESCAPE HATCH INTERIOR SURROUND, FS 405-FS 423. FIELD REPAIR FR-680-0155-6893 DATED 29 JUL 2019 WITH FAA FORM 8100-9 DATED 30 JUL 2019.Aug 6, 2019 · N357QS · Cessna 680CE · Fuselage Miscellaneous StructureSDR 2020F00011Skin · damagedREPAIR OF LT AND RT WING LEADING EDGE ROOT SKIN/LIGHT COVER ATTACH HOLE DAMAGE (PULLED TROUGH). ENGINEERING LETTER DQ22386M1 DATED JULY 23, 2019. LEADING EDGE ROOT SKINS P/N 6922590-1 / 6922590-2 AND LIGHT COVERS P/N 6922530-45 / 6922530-46.Jul 30, 2019 · N357QS · Cessna 680CE · Wing, Plate/SkinSDR EBVR20180430001Skin · corrodedDURING A VISUAL INSPECTION, FOUND CORROSION AROUND RIGHT FORWARD EQUIPMENT BAY AFT LATCH. CORROSION WAS FOUND TO BE DEEPER THAN THE MAINTENANCE MANUAL ALLOWED. REPAIRED IAW ERO-922424, REV IR.Apr 30, 2018 · N357QS · Cessna 680CE · Electrical/Electronic Compartment DoorsSDR EBVR2018043001Skin · corrodedCORROSION FOUND ON THE FUSELAGE SKIN AROUND THE RT NOSE AVIONICS DOOR AFT LATCH. BLENDED THE CORROSION ON THE FUSELAGE SKIN. INSTALLED A REPAIR DOUBLER IAW ERO-922424, REV IR.Apr 30, 2018 · N357QS · Cessna 680SOV · Fuselage Main, Plate/SkinSDR 2018FA0000064Skin · corrodedCORROSION ON THE RUDDER TE SKIN. ACCOMPLISHED LETTER DQ11021M1.Feb 21, 2018 · N357QS · Cessna 680SOV · Rudder, Plate/SkinSDR DXTA201802210001Skin · corrodedCORROSION ON THE SKIN. ACCOMPLISHED ENGINEERING LETTER DQ11022M1.Feb 21, 2018 · N357QS · Cessna 680SOV · Fuselage Main, Plate/SkinSDR DXTA2018021900110Skin · corrodedCORROSION ON THE USELAGE UPPER SKIN, BS 321, RBL 4.Feb 19, 2018 · N357QS · Cessna 680SOV · Fuselage Main, Plate/SkinSDR 2018FA0000061Fairing · debondedPLY SEPARATION DAMAGE TO THE LEFT WING UPPER DRAG ANGLE FAIRING. ACCOMPLISHED MANUFACTURER LETTER DQ11166M1 REV A.Feb 19, 2018 · N357QS · Cessna 680SOV · Wing, Attach Fittings
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