# Service difficulty reports: N376QS

A list on [N376QS](https://openairdocs.org/aircraft/N376QS.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 · 70 reports

- [SDR DXTA2026101210089](https://openairdocs.org/sdr/DXTA2026101210089.md): Light · inoperative · Oct 8, 2026 · N376QS · Cessna 680SOV · Emergency Lighting
  > THE EXTERIOR AFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. IAW MM 33-50-00
- [SDR DXTA2026090409512](https://openairdocs.org/sdr/DXTA2026090409512.md): Door · unsecure · Aug 31, 2026 · N376QS · Cessna 680SOV · Emergency Exits
  > EMERGENCY EXIT DOOR OPEN. ON PREFLIGHT, NOTICED THERE TO BE A GAP ON THE EMERGENCY EXIT DOOR AND NOT FLUSH WITH THE FUSELAGE. ABLE TO MOVE (ROCK) THE DOOR WHEN IT SHOULDN'T MOVE AT ALL. I ALSO WENT INSIDE OPENED (APPX 5) AND CLOSED THE DOOR TO RE-SEAT EMERGEN
- [SDR DXTA2026063008606](https://openairdocs.org/sdr/DXTA2026063008606.md): Battery Pack · unserviceable · Jun 28, 2026 · N376QS · Cessna 680SOV · Emergency Lighting
  > UPON TESTING THE EMERGENCY LIGHTS BEFORE STARTING THE APU THE LIGHTS WOULD NOT ILLUMINATE IN BOTH THE ARM AND ON POSITIONS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS, PERFORMED E-LIGHT SYSTEM OPERATIONAL CHECK. OPS CHECK GOOD AT THIS TIME. REF, AMM 3
- [SDR DXTA2026062908581](https://openairdocs.org/sdr/DXTA2026062908581.md): Pushrod · broken · Jun 25, 2026 · N376QS · Cessna 680SOV · Passenger/Crew Doors
  > AFTER TAKEOFF, WE HEARD A LOUD NOISE COMING FROM THE CABIN. AFTER LANDING WE NOTICED A GAP IN BETWEEN THE MAIN CABIN DOOR FAIRING AND THE BOTTOM OF THE DOOR. AFTER CYCLING THE DOOR A FEW TIMES, ONE OF THE ARMS ON THE FAIRING BROKE OFF FROM ITS ATTACHMENT. REM
- [SDR 2026FA0000341](https://openairdocs.org/sdr/2026FA0000341.md): Skin · corroded · May 8, 2026 · N376QS · Cessna 680CE · Wing, Plate/Skin
  > CORROSION WAS FOUND ON RIGHT HAND WING UPPER SKIN COMMON TO AFT SPAR
- [SDR DXTA2026030507109](https://openairdocs.org/sdr/DXTA2026030507109.md): Power Supply · defective · Mar 3, 2026 · N376QS · Cessna 680SOV · Emergency Lighting
  > BOTH THE EMERGENCY EXIT LIGHT NEAR THE CABIN DOOR AND THE GALLEY EMERGECY LIGHT ARE NOT STAYING BRIGHT FOR VERY LONG BEFORE DIMMING TO UNEXCEPTABLE LEVELS. EVEN AFTER A LONG FLIGHT. SUGGESTING THE BATTERY PACK IS GOING BAD. CORRECTIVE ACTION: REMOVED AND REPL
- [SDR DXTA2026022406986](https://openairdocs.org/sdr/DXTA2026022406986.md): Cable · loose · Feb 21, 2026 · N376QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR CABLE LOOSE. REMOVED AND REPLACED CABIN DOOR COUNTERBALANCE LUBRICATED SPRING IAW CE-680 AMM 52-10-50. PERFORMED CABIN DOOR COUNTERBALANCE SYSTEM ADJUSTMENT TEST IAW AMM 52-10-50 / AND FOUND SYSTEM WORKING NORMAL.
- [SDR JGVR20250521002](https://openairdocs.org/sdr/JGVR20250521002.md): Skin · corroded · May 21, 2025 · N376QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED CORRODED AREA LOCATED ON THE UPPER INBOARD WING SKINS ALONG THE DRAG ANGLES (WING-TO-FUSELAGE FAIRING STRUCTURE) REMOVED THE MIDDLE AND AFT DRAG ANGLES FOR ACCESS AND BLENDED ADDITIONAL AREAS. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED
- [SDR JGVR20250521001](https://openairdocs.org/sdr/JGVR20250521001.md): Support Bracket · corroded · May 21, 2025 · N376QS · Cessna 680CE · Vertical Stabilizer
  > REMOVED THE CORRODED UPPER RUDDER SUPPORT UPPER BRACKET, RECEIVED FABRICATED NEW BRACKET PART NUMBER AQRD-6931050-64 AND INSTALLED PER TEXTRON 680 SRM 51-40-03 AND AEROSPACE QUALITY RESEARCH AND DEVELOPMENT MRO ENGINEERING REPAIR ORDER AND NETJETS REQUEST FOR
- [SDR JGVR20250520002](https://openairdocs.org/sdr/JGVR20250520002.md): Hinge · corroded · May 20, 2025 · N376QS · Cessna 680CE · Ailerons
  > BLENDED AREA OF CORROSION LOCATED ON LH AILERON, INBOARD HINGE, INBOARD SIDE WHERE BOND JUMPER ATTACHES, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20250520003](https://openairdocs.org/sdr/JGVR20250520003.md): Skin · corroded · May 20, 2025 · N376QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED MULTIPLE CORRODED AREAS OF THE RH WING UPPER INBOARD SKINS LOCATED ALONG THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING STRUCTURE), PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED BLENDED AREAS BY TREATING, PRIMING AND TOP COATING AREAS PER T
- [SDR JGVR20250520001](https://openairdocs.org/sdr/JGVR20250520001.md): Skin · damaged · May 20, 2025 · N376QS · Cessna 680CE · Wing, Plate/Skin
  > MECHANICALLY REMOVED CORROSION ALONG LH AND RH WING LOWER TRAILING EDGE SKIN NEAR THE AFT DRAG ANGLE OUTBOARD EDGES, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED CORROSION BLEND BY CLEANING, TREATING AND PRIMING PER NETJETS REQUEST FOR TECHNICAL
- [SDR JGVR202505140003](https://openairdocs.org/sdr/JGVR202505140003.md): Skin · corroded · May 14, 2025 · N376QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > BLENDED CORRODED AREA LOCATED SKIN OF THE VERTICAL STABILIZER AT THE TRAILING EDGE UPPER END, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED BLENDED AREA BY FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH AN
- [SDR JGVR20250514002](https://openairdocs.org/sdr/JGVR20250514002.md): Structure · corroded · May 14, 2025 · N376QS · Cessna 680CE · Wing Main, Frame Structure
  > BLENDED CORRODED AREA LOCATED IN THE LH MAIN LAND GEAR WHEEL WELL LOCATED UNDER THE EMERGENCY BRAKE FEED THRU FITTING AT WS37, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED BLENDED AREA BY FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE W
- [SDR JGVR20250514001](https://openairdocs.org/sdr/JGVR20250514001.md): Skin · damaged · May 14, 2025 · N376QS · Cessna 680CE · Emergency Exits
  > BLENDED 5 AREAS OF CORROSION LOCATED ON THE OUTER SKIN OF THE EMERGENCY EXIT DOOR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED BLENDED AREA PER TEXTRON STANDARD REPAIR.
- [SDR DXTA2025031702572](https://openairdocs.org/sdr/DXTA2025031702572.md): Shutoff Valve · malfunctioned · Mar 3, 2025 · N376QS · Cessna 680SOV · Engine Temperature Indicating System
  > LEFT ENGINE ITT EXCEEDANCE. WHILE IN CLIMB ABOUT 38,000 FEET WITH THRUST SET AT MCT, THE LEFT ENGINE ITT WENT INTO THE YELLOW BAND. AFTER 20 SECONDS THE YELLOW BAND TURNED RED AND THEN WE PULLED THE POWER BACK TO REDUCE THE ITT. HIGHEST ITT OBSERVED WAS 930, A
- [SDR DXTA2025030702572](https://openairdocs.org/sdr/DXTA2025030702572.md): Engine · overtemp · Mar 3, 2025 · N376QS · Cessna 680SOV · Engine Temperature Indicating System
  > LEFT ENGINE ITT EXCEEDANCE. WHILE IN CLIMB ABOUT 38,000 FEET WITH THRUST SET AT MCT, THE LEFT ENGINE ITT WENT INTO THE YELLOW BAND. AFTER 20 SECONDS THE YELLOW BAND TURNED RED AND THEN WE PULLED THE POWER BACK TO REDUCE THE ITT. HIGHEST ITT OBSERVED WAS 930, A
- [SDR DXTA2025010601842](https://openairdocs.org/sdr/DXTA2025010601842.md): Fuse · inoperative · Jan 4, 2025 · N376QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHTING: ALL EMERGENCY LIGHTS INOP WITH SWITCH IN ARM, WORKS MORMALLY WITH SWITCH ON CORRECTIVE ACTION: REPLACED FUSE IN #1 EMERGENCY BATTERY PACK. OPS CHECK GOOD. IAW CE-680 AMM 33-50-00.
- [SDR DXTA2024122601674](https://openairdocs.org/sdr/DXTA2024122601674.md): Fuse · defective · Dec 23, 2024 · N376QS · Cessna 680SOV · Emergency Lighting
  > MAIN EXIT SIGN/LIGHT: THE MAIN CABIN DOOR EMERGENCY EXIT SIGN IS INOP ALONG WITH THE EXIT SIGNS ON EACH SIDE OF THE DOOR WITH BATTERIES OFF AND EMERGENCY LIGHT SWITCH ON. THEY ARE ALSO INOP WITH THE APU RUNNING, EMERGENCY LIGHT SWITCH SET TO ARM AND PAX SAFET
- [SDR DXTA2024122401624](https://openairdocs.org/sdr/DXTA2024122401624.md): Fuse · blown · Dec 20, 2024 · N376QS · Cessna 680SOV · Emergency Lighting
  > SAW RT WING INSPECTION LIGHT GO OFF. IT SHOULD BE ON WITH THE EMERGENCY LIGHTS ARMED & PAX SAFETY SWITCH ON. ON INVESTIGATION, MAIN CABIN ENTRY DOOR EMERGENCY LIGHT WAS OFF ALONG WITH LAV BULKHEAD EMERGENCY LIGHT, WITH THE APU RUNNING, EMERGENCY LIGHTS ARMED
- [SDR DXTA2024121201481](https://openairdocs.org/sdr/DXTA2024121201481.md): Battery Pack · defective · Dec 11, 2024 · N376QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY SWITCH ON POSITION NO EMERG EXIT SIGN/ LIGHT. REMOVED AND REPLACED EMER BATTERY, P.ERFORMED CONTINUITY CHECKS ALONG WITH CHARGING OF THE EMER BATTERY FOR TWO HOURS. OPERATIONAL CHECKS GOOD, RETURNED AIRCRAFT TO ORIGINAL CONFIGURATION. NO FURTHER MA
- [SDR DXTA2024121101435](https://openairdocs.org/sdr/DXTA2024121101435.md): Battery · defective · Dec 7, 2024 · N376QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHTS NOT TURNING ON WHEN PAX SAFTEY BUTTON IS SELECTED ON. EMERGENCY LIGHTS DO TURN ON WHEN EMER LTS SWITCH IS SELECTED TO ON ARRIVED AT AC AND TURNED ON ERNER LIGHTS AND FOUND THAT THE ONLY EMER LIGHTS THAT DID NOT ILLUMINATE WERE THE FWD MOST LIG
- [SDR 2024F00260](https://openairdocs.org/sdr/2024F00260.md): Skin · corroded · Oct 25, 2024 · N376QS · Cessna 680SOV · Wing, Plate/Skin
  > LOWER WING SKIN CORROSION REF (ENGINEERING REPAIR ORDER ERO-979789)
- [SDR DXTA2023110699920](https://openairdocs.org/sdr/DXTA2023110699920.md): Unknown · unknown · Nov 5, 2023 · N376QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR IS VERY DIFFICULT TO PULL CLOSED FROM INSIDE. IT ALSO SWINGS DOWN AGGRESSIVELY WHEN OPENING. REMOVED MED STEPS, INSPECTED ALL MED LINKAGES. NO DEFECTS NOTED. INSPECTED MED CABLES, FOUND CABLES TO BE SERVICEABLE AND CABLES AT PROPER
- [SDR 2023F00249](https://openairdocs.org/sdr/2023F00249.md): Rudder · damaged · Aug 14, 2023 · N376QS · Cessna 680CE · Rudder Structure
  > TOP OF THE RUDDER IN THE RUDDER CAP HAS SMALL BURN HOLE FROM POSSIBLE LIGHTING STRIKE.
- [SDR 2023FA0000119](https://openairdocs.org/sdr/2023FA0000119.md): Wing · corroded · Mar 9, 2023 · N376QS · Cessna 680SOV · Wing Structure
  > EXFOLIATION FOUND IN FOUR LOCATIONS ALONG THE REAR AFT SPAR OF THE LH & RH MLG. REQUIRES HI-LOK REMOVAL, CORROSION REMOVAL AND MAPPING
- [SDR 2023F00307](https://openairdocs.org/sdr/2023F00307.md): Spar · corroded · Mar 8, 2023 · N376QS · Cessna 680CE · Wing Spar
  > FOUND DURING MM TASK 57-00-00-2200: EXFOLIATION FOUND IN FOUR LOCATIONS ALONG THE REAR AFT SPAR OF THE LH & RH MLG.
- [SDR DXTA2023011678540](https://openairdocs.org/sdr/DXTA2023011678540.md): Downlock Switch · failed · Jan 14, 2023 · N376QS · Cessna 680CE · Landing Gear Position and Warning
  > MAIN RIGHT GEAR WOULD NOT RETRACT. AFTER GEAR RETRACTION NOSE AND LEFT MAIN RETRACTED. RIGHT MAIN REMAINED DOWN AND LOCKED (GREEN). ALSO CONFIRMED BY TOWER ON DEPARTURE NOSE AND LEFT RETRACKED, RIGHT MAIN DOWN. NO RED UNLOCK LIGHT. PER QRH LOWERED GEAR, 3 GRE
- [SDR DXTA2023010377590](https://openairdocs.org/sdr/DXTA2023010377590.md): Light · inoperative · Dec 31, 2022 · N376QS · Cessna 680CE · Emergency Lighting
  > CABIN EMERG LIGHT: REPEAT WRITE UP (6TH THIS MONTH). CABIN EMERGENCY LIGHTS INOP IN ARM POSITION (NOTICED DURING PREFLIGHT). MOST LIGHTS COME ON WITH SWITCH IN 'ON' POSITION. WITH EMER LIGHT SWITCH IN 'ARM' POSITION AND THEN SELECTING PAX SAFETY SWITCH TO ON
- [SDR DXTA2022122777050](https://openairdocs.org/sdr/DXTA2022122777050.md): Battery Pack · defective · Dec 24, 2022 · N376QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTING: WHILE EXECUTING THE POWER ON CHECKLIST, WE DISCOVERED THE EMER LIGHTS WILL NOT ILLUMINATE IN THE ARM POSITION, BUT SOME WILL ILLUMINATE IN THE ON POSITION. REMOVED AND REPLACED ALL 4 EMERGENCY BATTIERES IAW MM 33-50-10.
- [SDR DXTA2022121976560](https://openairdocs.org/sdr/DXTA2022121976560.md): Battery Pack · inoperative · Dec 18, 2022 · N376QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTING: WHILE CONDUCTING THE POWER ON CHECKLIST WE DISCOVERED WHEN THE EMER LTS ARE PLACED IN THE ARM POSITION, THE LIGHTS DO NOT ILLUMINATE. WHEN THE SWITCH IS PLACED IN THE ON POSITION, THE LIGHTS WORK. // SIGNOFF // TROUBLESHOT AND DETERMINED FA
- [SDR DXTA2022120975830](https://openairdocs.org/sdr/DXTA2022120975830.md): Fuse · blown · Dec 8, 2022 · N376QS · Cessna 680A · Emergency Lighting
  > CABIN EMERG LIGHT: DURING POWER ON CHECKS WITH EMERGENCY LIGHTS SWITCH TO ARM, NONE OF THE EMERGENCY LIGHTS ILLUMINATE. WITH THE SWITCH TO ON, ALL ILLUMINATE EXCEPT THE WORK TABLE LIGHT, THE EXIT SIGN OVER MAIN CABIN DOOR AND THE 2 RED EXIT SIGNS ON EITHER SID
- [SDR DXTA2022120775660](https://openairdocs.org/sdr/DXTA2022120775660.md): Fuse · blown · Dec 6, 2022 · N376QS · Cessna 680CE · Emergency Lighting
  > DURING THE POWER ON CHECKLIST, WITH THE EMERGENCY LIGHTS SWITCH ARMED AND THE BATTERY SWITCHES OFF, NONE OF THE EMERGENCY LIGHTS ILLUMINATE. WITH THE EMERGENCY LIGHTS SWITCH IN THE ON POSITION AND THE THE BATTERY SWITCHES STILL OFF, ALL OF THE EMERGENCY LIGHTS
- [SDR DXTA2022112274510](https://openairdocs.org/sdr/DXTA2022112274510.md): Circuit Breaker · tripped · Nov 22, 2022 · N376QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHTING: WHEN THE EMER LIGHTS ARE TESTED (EMER SWITCH IN ON POSITION, PASS SAFETY SWITCH OFF) ALL EMER LIGHTS WORK CORRECTLY, INTERIOR AND EXTERIOR. WHEN THE EMER LIGHT SWITCH IS IN THE ARM POSITION AND THE PASS SAFETY SWITCH IS ON, ALL THE INTERIO
- [SDR DXTA2022110973540](https://openairdocs.org/sdr/DXTA2022110973540.md): Battery Pack · inoperative · Nov 8, 2022 · N376QS · Cessna 680CE · Emergency Lighting
  > MAIN EXIT SIGN/LIGHT: EMERGENCY EXIT LIGHT ABOVE MCD WILL NOT ILLUMINATE. REMOVED FAULTY #1 EMERGENCY BATTERY AND INSTALLED A REPAIRED BATTERY AND COMPLETED OPS CHECKS WITH NO DEFECTS NOTED IAW AMM 33-50-10 AND 33-50-00.
- [SDR DXTA2022102772820](https://openairdocs.org/sdr/DXTA2022102772820.md): Battery Pack · defective · Oct 26, 2022 · N376QS · Cessna 680CE · Emergency Lighting
  > WITH EMER LTS SWITCH IN "ARM" POSITION AND PAX SAFETY SWITCH ON (BATTS ON), NONE OF THE 17 LIGHTS WILL ILLUMINATE. WITH THE EMER LTS SWITCH IN THE "ON" POSITION, REGARDLESS OF BATTS OR PAX SAFETY SWITCH, ALL LIGHTS ILLUMINATE EXCEPT FOR THE THREE INTERIOR MAI
- [SDR DXTA2022091970570](https://openairdocs.org/sdr/DXTA2022091970570.md): None · none · Sep 16, 2022 · N376QS · Cessna 120 · Passenger/Crew Doors
  > MAIN DOOR: MAIN DOOR FREE FALLS OPEN WHEN UNLATCHED. BOTH DAMPENERS ON DOOR ARE WEAK AND MAY REQUIRE REPLACEMENT. //SIGNOFF// OPERATED DOOR MULTIPLE TIMES AND NOTED NO FREEFALL, SUBMITTED VIDEO TO MCC. DOOR REQUIRED ASSISTANT TO COME DOWN INTO THE LOCKED POSIT
- [SDR DXTA2022091570440](https://openairdocs.org/sdr/DXTA2022091570440.md): None · none · Sep 15, 2022 · N376QS · Cessna 120 · Emergency Lighting
  > EMERG EXIT SIGN/LIGHT: WHEN THE EMERGENCY LIGHTS TOGGLE IS SWITCHED TO ON, ABOUT HALF OF THE EXIT LIGHTS ILLUMINATE. WHEN THE TOGGLE IS IN THE ARMED POSITION AND THE PAX SAFETY SWITCH IS ACTIVATED THE CHIME SOUNDS BUT NONE OF THE EMERGENCY EXIT SIGNS ILLUMINAT
- [SDR DXTA2022090669770](https://openairdocs.org/sdr/DXTA2022090669770.md): None · none · Sep 6, 2022 · N376QS · Cessna 680SOV · Emergency Lighting
  > CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS INOP. REPEAT WRITE-UP. NO MAIN DC, EMER LIGHTS ON/ARM FORWARD DOOR EXIT, OVER GALLEY AND DOOR LIGHTS INOP. MAIN DC ON, EMER LIGHTS ON OR ARM AND PAX SAFETY ON ALL CABIN EXIT/EMER LIGHTS INOP. CHIME AND NO SMOKING LIGHT
- [SDR DXTA2022090669670](https://openairdocs.org/sdr/DXTA2022090669670.md): None · none · Sep 5, 2022 · N376QS · Cessna 680A · Emergency Lighting
  > EMERGENCY LIGHTING: CANIN EMERGENCY LIGHTS INOP. NO MAIN DC, EMER LIGHTS ON/ARM FORWARD DOOR EXIT, OVER GALLEY, AND DOOR LIGHTS INOP. MAIN DC ON, EMER LIGHTS ARM, PAX SAFETY ON, ALL CABIN EXIT/EMER LIGHTS INOP. CHIME AND NO SMOKING LIGHTS DO COME ON THOUGH.//C
- [SDR DXTA2021121353460](https://openairdocs.org/sdr/DXTA2021121353460.md): None · none · Dec 12, 2021 · N376QS · Cessna 680CE · Stabilizer Control System
  > PRIMARY STAB TRIM FAIL AMBER CAS: WE INTIALLY INCURRED A AMBER PRIMARY STAB TRIM FAIL MESSAGE FOLLOWED BY A AMBER SECONDARY STAB TRIM FAIL CAS MESSAGE. BEFORE THE MESSAGE WE COULD TRIM UP BUT NOT DOWN BELOW 1.5 ON THE STAB TRIM INDICATOR. // SIGNOFF // ONCE AR
- [SDR DXTA2020031003570](https://openairdocs.org/sdr/DXTA2020031003570.md): Module · defective · Mar 9, 2020 · N376QS · Cessna 680CE · Trailing Edge Flap Control System
  > FLAP POSITION INDICATION - AFTER DEPARTURE THE FLAPS WERE RAISED AT 400'. AT THAT POINT THE FLAP RESET AMBER LIGHT CAME ON. USING THE QRC. IT WOULDN'T RESET. A FLAP-LESS LANDING WAS MADE AT DENVER ///SIGN-OFF///REMOVED FAULTY SOFT START MODULE, PIN 6238405-30
- [SDR JGVR20200224001](https://openairdocs.org/sdr/JGVR20200224001.md): Spar · corroded · Feb 24, 2020 · N376QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > MECHANICALLY BLENDED CORRODED AREA FROM THE VERTICAL STABILIZER LH SPAR CLIP, APPROXIMATELY FOUR INCHES BELOW THE MIDDLE RUDDER HINGE, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTIONS AND REPORTED TO TEXTRON FOR REPAIR DISPOSITION. CLEANED, T
- [SDR JGVR20190919006](https://openairdocs.org/sdr/JGVR20190919006.md): Rib · cracked · Sep 19, 2019 · N376QS · Cessna 680CE · Rudder, Spar/Rib
  > REPAIRED RUDDER BY REPLACING CRACKED LOWER AFT RIB AND CLIP WITH NEW RIB P/N 6933160-3 AND CLIP P/N 6933160-2 PER SRM 51-40-03, 51-40-06, 51-40-09, AND CSPM 20-40-20.
- [SDR JGVR20190919005](https://openairdocs.org/sdr/JGVR20190919005.md): Doubler · chafed · Sep 19, 2019 · N376QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > REPAIRED CHAFE HOLE IN THE INNER DOUBLER OF THE E-EXIT SURROUND NEAR FS 409.26 BY BLENDING, PERFORMING NDT, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING REPAIR ORDER.
- [SDR JGVR20190919004](https://openairdocs.org/sdr/JGVR20190919004.md): Doubler · chafed · Sep 19, 2019 · N376QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > REPAIRED CHAFE HOLE IN THE INNER DOUBLER OF THE E-EXIT SURROUND NEAR FS 409.26 BY BLENDING, PERFORMING NDT, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING REPAIR ORDER.
- [SDR JGVR20190919001](https://openairdocs.org/sdr/JGVR20190919001.md): Structure · corroded · Sep 19, 2019 · N376QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > REPAIRED CORRODED AREAS OF THE CENTER DROPPED AISLE FLOOR FROM FS 164 TO FS 202 BETWEEN STRINGERS 16L AND 16R BY BLENDING CORRODED AREAS, PERFORMING NDT, TREATING, PRIMING, AND INSTALLING REINFORCEMENT AS REQUIRED IN ACCORDANCE WITH FIELD REPAIR.
- [SDR JGVR20190911001](https://openairdocs.org/sdr/JGVR20190911001.md): Drag Angle · not reported · Sep 11, 2019 · N376QS · Cessna 680CE · Wing Miscellaneous Structure
  > R&R THE LT FORWARD, MIDDLE, AND AFT WING/FUSELAGE DRAG ANGLES AND BLENDED CORRODED AREAS OF THE LT UPPER WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. TREATED AND PRIMED ALL REPAIR AREAS PER FIELD REPAIR.
- [SDR DXTA2019032302198](https://openairdocs.org/sdr/DXTA2019032302198.md): Control Valve · unserviceable · Mar 23, 2019 · N376QS · Cessna 680CE · Cabin Temperature Control System
  > CAN NOT CONTROL COCKPIT TEMP IN MANUAL OR AUTOMATIC MODE. COULD NOT SELECT A CABIN TEMP COOLER THAN 85 DEGREES. AT ONE POINT IT GOT SO HOT SMOKE WAS COMING OUT OF THE COCKPIT AREA. SUPPLY TEMP WAS STEADY AT 210 DEGREES. //SIGNOFF// REMOVED AND REPLACED TEMP
- [SDR JGVR20180905001](https://openairdocs.org/sdr/JGVR20180905001.md): Skin · corroded · Sep 5, 2018 · N376QS · Cessna 680CE · Aerodynamic Fairings
  > FOUND CORRODED AREA ON THE BELLY SKIN OF THE TAILCONE, JUST FORWARD OF THE AIRCRAFT MANUFACTURE'S DATA TAG. REMOVED THE AFT TAILCONE/MAINTENANCE DOOR FAIRING FOR ACCESS. REPAIRED LT & RT LOWER TAILCONE SKIN CORROSION BY BLENDING, TREATING, AND INSTALLING REINF

Next page: https://openairdocs.org/aircraft/N376QS/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 = 'N376QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N376QS/reports

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