# Service difficulty reports: N357QS

A list on [N357QS](https://openairdocs.org/aircraft/N357QS.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 75 reports

- [SDR DXTA2026071508821](https://openairdocs.org/sdr/DXTA2026071508821.md): Spring · broken · Jul 14, 2026 · N357QS · Cessna 680SOV · Passenger/Crew Doors
  > DOOR 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 SUPP
- [SDR DXTA2026061008391](https://openairdocs.org/sdr/DXTA2026061008391.md): Light · malfunctioned · Jun 9, 2026 · N357QS · Cessna 680SOV · Emergency Lighting
  > DURING 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 SW
- [SDR DXTA2026031307235](https://openairdocs.org/sdr/DXTA2026031307235.md): Wire · unsecure · Mar 12, 2026 · N357QS · Cessna 680SOV · Light System Wiring
  > REAR 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 EMERGE
- [SDR DXTA2025102705425](https://openairdocs.org/sdr/DXTA2025102705425.md): Battery Pack · faulty · Oct 24, 2025 · N357QS · Cessna 680SOV · Emergency Lighting
  > PREFLIGHT - 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 I
- [SDR 2025F00214](https://openairdocs.org/sdr/2025F00214.md): Skin · damaged · Aug 29, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/Skin
  > REPAIRED 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 FATIG
- [SDR 2025F00201](https://openairdocs.org/sdr/2025F00201.md): Skin · corroded · Aug 26, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/Skin
  > MECHANICALLY 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 CORROSI
- [SDR 2025F00200](https://openairdocs.org/sdr/2025F00200.md): Skin · corroded · Aug 26, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/Skin
  > MECHANICALLY 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 ARE
- [SDR 2025F00199](https://openairdocs.org/sdr/2025F00199.md): Skin · corroded · Aug 26, 2025 · N357QS · Cessna 680A · Fuselage Main, Plate/Skin
  > MECHANICALLY 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 CORROSIO
- [SDR 2025F00198](https://openairdocs.org/sdr/2025F00198.md): Structure · corroded · Aug 26, 2025 · N357QS · Cessna 680A · Fuselage Miscellaneous Structure
  > MECHANICALLY 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 I
- [SDR 2025F00188](https://openairdocs.org/sdr/2025F00188.md): Skin · corroded · Aug 11, 2025 · N357QS · Cessna 680A · Emergency Exits
  > 1 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 EXCEE
- [SDR DXTA2025042503175](https://openairdocs.org/sdr/DXTA2025042503175.md): Acm · faulted · Apr 22, 2025 · N357QS · Cessna 680SOV · Cabin Cooling System
  > CONCURRENT 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 NOTICEA
- [SDR JGVR20250109001](https://openairdocs.org/sdr/JGVR20250109001.md): Fitting · corroded · Jan 9, 2025 · N357QS · Cessna 680CE · Hydraulic System, Main
  > REMOVED 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 IA
- [SDR JGVR20241216001](https://openairdocs.org/sdr/JGVR20241216001.md): Spar · damaged · Dec 31, 2024 · N357QS · Cessna 680CE · Wing Spar
  > R&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.
- [SDR JGVR20240611001](https://openairdocs.org/sdr/JGVR20240611001.md): Skin · corroded · Jun 11, 2024 · N357QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > BLENDED 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.
- [SDR JGVR20240610002](https://openairdocs.org/sdr/JGVR20240610002.md): Skin · corroded · Jun 10, 2024 · N357QS · Cessna 680CE · Horizontal Stabilizer Structure
  > REPAIRED 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
- [SDR JGVR20240610001](https://openairdocs.org/sdr/JGVR20240610001.md): Skin · damaged · Jun 10, 2024 · N357QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED 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 ACCEPTABLE
- [SDR JGVR20240607001](https://openairdocs.org/sdr/JGVR20240607001.md): Skin · corroded · Jun 7, 2024 · N357QS · Cessna 680CE · Wing, Plate/Skin
  > REPAIRED 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 AE
- [SDR JGVR20240606001](https://openairdocs.org/sdr/JGVR20240606001.md): Angle · corroded · Jun 6, 2024 · N357QS · Cessna 680CE · Vertical Stabilizer Miscellaneous Structure
  > MECHANICALLY 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 REQUIRED
- [SDR JGVR20240605001](https://openairdocs.org/sdr/JGVR20240605001.md): Skin · damaged · Jun 5, 2024 · N357QS · Cessna 680CE · Aerodynamic Fairings
  > REPAIRED 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 REPAIR
- [SDR JGVR20240604003](https://openairdocs.org/sdr/JGVR20240604003.md): Skin · damaged · Jun 4, 2024 · N357QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED 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.
- [SDR JGVR20240604002](https://openairdocs.org/sdr/JGVR20240604002.md): Skin · damaged · Jun 4, 2024 · N357QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > REPAIRED 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 RE
- [SDR JGVR20240604001](https://openairdocs.org/sdr/JGVR20240604001.md): Skin · damaged · Jun 4, 2024 · N357QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > REPAIRED 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 ENGINEERING
- [SDR JGVR20250110001](https://openairdocs.org/sdr/JGVR20250110001.md): Fitting · corroded · Oct 5, 2023 · N357QS · Cessna 680CE · Wing Main, Frame Structure
  > REPAIRED 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 ORDER
- [SDR DXTA2023030381570](https://openairdocs.org/sdr/DXTA2023030381570.md): Battery · discharged · Mar 1, 2023 · N357QS · Cessna 680CE · Emergency Lighting
  > ON 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 *** REMO
- [SDR 2023FA0000099](https://openairdocs.org/sdr/2023FA0000099.md): Spar · corroded · Feb 24, 2023 · N357QS · Cessna 680CE · Wing Spar
  > CORROSION - EXFOLIATION FOUND IN LOWER SPAR OF LH AND RH MLG WHEEL WELLS
- [SDR 3J7R2023010400001](https://openairdocs.org/sdr/3J7R2023010400001.md): G Switch · activated · Jan 3, 2023 · N357QS · Cessna 680CE · Emergency Lighting
  > DURING MX CHECK FOUND EMER LIGHTS STAY ON WITH SWITCH IN ARM POSITION
- [SDR DXTA2022112174380](https://openairdocs.org/sdr/DXTA2022112174380.md): Warning Light · inoperative · Nov 21, 2022 · N357QS · Cessna 680SOV · Engine Thrust Reverser
  > UPON 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
- [SDR DXTA2022032959180](https://openairdocs.org/sdr/DXTA2022032959180.md): I/O Card · faulted · Mar 29, 2022 · N357QS · Cessna 680CE · Fuel Controlling System
  > ENGINE 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
- [SDR DXTA2021122954390](https://openairdocs.org/sdr/DXTA2021122954390.md): None · broken · Dec 28, 2021 · N357QS · Gulstm 680 · Landing Gear Retraction/Extension System
  > NLG 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/
- [SDR DXTA2021102150600](https://openairdocs.org/sdr/DXTA2021102150600.md): Unknown · odor · Oct 20, 2021 · N357QS · Cessna 680CE · Air Distribution System
  > COCKPIT 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 R
- [SDR DXTA2021092449370](https://openairdocs.org/sdr/DXTA2021092449370.md): Battery · defective · Sep 23, 2021 · N357QS · Cessna 680CE · Emergency Lighting
  > CABIN 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 OVE
- [SDR DXTA2021092349340](https://openairdocs.org/sdr/DXTA2021092349340.md): Battery · defective · Sep 22, 2021 · N357QS · Gulstm 680 · Emergency Lighting
  > MAIN 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 FO
- [SDR DXTA2021031839600](https://openairdocs.org/sdr/DXTA2021031839600.md): Coalescer Bag · odor · Mar 16, 2021 · N357QS · Cessna 680CE · Humidity Control System
  > COCKPIT 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-
- [SDR JGVR20210302002](https://openairdocs.org/sdr/JGVR20210302002.md): Skin · corroded · Mar 2, 2021 · N357QS · Cessna 680A · Vertical Stabilizer, Plate/Skin
  > ONE 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 MATERI
- [SDR JGVR20210302001](https://openairdocs.org/sdr/JGVR20210302001.md): Spar · corroded · Mar 2, 2021 · N357QS · Cessna 680A · Wing Spar
  > ONE 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 CO
- [SDR DXTA2020110404310](https://openairdocs.org/sdr/DXTA2020110404310.md): Battery · defective · Nov 4, 2020 · N357QS · Cessna 680CE · Battery/Charger System
  > AFTER 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 WI
- [SDR JGVR20201001001](https://openairdocs.org/sdr/JGVR20201001001.md): Skin · debonded · Oct 1, 2020 · N357QS · Cessna 680A · Wing, Plate/Skin
  > VERTICAL 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 FI
- [SDR JGVR20201001006](https://openairdocs.org/sdr/JGVR20201001006.md): Nut Plate · corroded · Oct 1, 2020 · N357QS · Cessna 680CE · Vertical Stabilizer
  > FOUND 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.
- [SDR JGVR20201001005](https://openairdocs.org/sdr/JGVR20201001005.md): Bracket · corroded · Oct 1, 2020 · N357QS · Cessna 680CE · Fuselage Main, Attach Fittings
  > FOUND 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.
- [SDR JGVR20201001004](https://openairdocs.org/sdr/JGVR20201001004.md): Spar · damaged · Oct 1, 2020 · N357QS · Cessna 680CE · Wing Spar
  > MECHANICALLY 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.
- [SDR JGVR20201001003](https://openairdocs.org/sdr/JGVR20201001003.md): Skin · corroded · Oct 1, 2020 · N357QS · Cessna 680CE · Aerodynamic Fairings
  > FOUND 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 MEMO
- [SDR JGVR20201001002](https://openairdocs.org/sdr/JGVR20201001002.md): Skin · corroded · Oct 1, 2020 · N357QS · Cessna 680CE · Emergency Exits
  > FOUND 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
- [SDR 2019F00145](https://openairdocs.org/sdr/2019F00145.md): Doubler · gouged · Aug 6, 2019 · N357QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > REPAIR 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.
- [SDR 2020F00011](https://openairdocs.org/sdr/2020F00011.md): Skin · damaged · Jul 30, 2019 · N357QS · Cessna 680CE · Wing, Plate/Skin
  > REPAIR 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.
- [SDR EBVR20180430001](https://openairdocs.org/sdr/EBVR20180430001.md): Skin · corroded · Apr 30, 2018 · N357QS · Cessna 680CE · Electrical/Electronic Compartment Doors
  > DURING 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.
- [SDR EBVR2018043001](https://openairdocs.org/sdr/EBVR2018043001.md): Skin · corroded · Apr 30, 2018 · N357QS · Cessna 680SOV · Fuselage Main, Plate/Skin
  > CORROSION 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.
- [SDR 2018FA0000064](https://openairdocs.org/sdr/2018FA0000064.md): Skin · corroded · Feb 21, 2018 · N357QS · Cessna 680SOV · Rudder, Plate/Skin
  > CORROSION ON THE RUDDER TE SKIN. ACCOMPLISHED LETTER DQ11021M1.
- [SDR DXTA201802210001](https://openairdocs.org/sdr/DXTA201802210001.md): Skin · corroded · Feb 21, 2018 · N357QS · Cessna 680SOV · Fuselage Main, Plate/Skin
  > CORROSION ON THE SKIN. ACCOMPLISHED ENGINEERING LETTER DQ11022M1.
- [SDR DXTA2018021900110](https://openairdocs.org/sdr/DXTA2018021900110.md): Skin · corroded · Feb 19, 2018 · N357QS · Cessna 680SOV · Fuselage Main, Plate/Skin
  > CORROSION ON THE USELAGE UPPER SKIN, BS 321, RBL 4.
- [SDR 2018FA0000061](https://openairdocs.org/sdr/2018FA0000061.md): Fairing · debonded · Feb 19, 2018 · N357QS · Cessna 680SOV · Wing, Attach Fittings
  > PLY SEPARATION DAMAGE TO THE LEFT WING UPPER DRAG ANGLE FAIRING. ACCOMPLISHED MANUFACTURER LETTER DQ11166M1 REV A.

Next page: https://openairdocs.org/aircraft/N357QS/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N357QS/reports

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