# Service difficulty reports: N378QS, cancelled Jul 2, 2026

A list on [N378QS, cancelled Jul 2, 2026](https://openairdocs.org/deregistered/N378QS-2026-07-02.md).

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

- [SDR DXTA2026022707024](https://openairdocs.org/sdr/DXTA2026022707024.md): Bearing · defective · Feb 24, 2026 · N378QS · Cessna 680SOV · Landing Gear Position and Warning
  > AFTER TAKEOFF, GEAR RETRACTED NORMALLY. DURING CLIMB OUT (APPROXIMATELY 10000-12000 FEET) THE RED GEAR UNLOCK LIGHT ILLUMINATED. RAN QRH. DURING THE GVI OF THE NLG ASSEMBLY FOUND THE UPLOCK BEARING WAS COMPLETLY MISSING FROM THE NOSE GEAR CAUSING THE UPLOCK S
- [SDR JGVR20251117005](https://openairdocs.org/sdr/JGVR20251117005.md): Doubler · corroded · Nov 17, 2025 · N378QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED AREAS OF CORROSION ON RT WING FUEL FILLER ASSEMBLY DOUBLER PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251117004](https://openairdocs.org/sdr/JGVR20251117004.md): Skin · corroded · Nov 17, 2025 · N378QS · Cessna 680CE · Emergency Exits
  > BLENDED 4 AREAS OF CORROSION LOCATED ON OUTER SKIN OF E-EXIT ALONG CONTOUR RING INNER EDGE, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251117003](https://openairdocs.org/sdr/JGVR20251117003.md): Hinge Bracket · corroded · Nov 17, 2025 · N378QS · Cessna 680CE · Vertical Stabilizer
  > BLENDED CORRODED AREA ON THE VERTICAL STABILIZER MIDDLE RUDDER HINGE UPPER BRACKET, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR DXTA2025042903233](https://openairdocs.org/sdr/DXTA2025042903233.md): Strut · contaminated · Apr 26, 2025 · N378QS · Cessna 680SOV · Nose/Tail Landing Gear Strut/Axle
  > GEAR POSITION & WARNING: AFTER NORMAL TAKEOFF TRIED TO RETRACT THE GEAR, HEARD AND FELT A THUD. GEAR DID NOT RETRACT. RAN QRH AND UNEXPECTED THREAT FLOW CHART. RETURNED AND LANDED AT KIAD. DID NOT DECLARE AN EMERGENCY. JACKED ACFT & PERFORMED OPS CHECK OF THE
- [SDR DXTA2024082800343](https://openairdocs.org/sdr/DXTA2024082800343.md): Switch · defective · Aug 27, 2024 · N378QS · Cessna 680SOV · Emergency Lighting
  > WHEN PLACED IN THE "ON" POSITION, THE EMER LTS SWITCH IS INOP. WHEN PLACED IN THE "OFF" OR "ARMED" POSITION THE SWITCH AND LIGHTS FUNCTION NORMALLY. CORRECTIVE ACTION: INSTALLED NEW TOGGLE SWITCH. P/N A3-201-01A. PERFORMED EMERGENCY LIGHTING OPERATIONAL CHECKS
- [SDR DXTA2024070312250](https://openairdocs.org/sdr/DXTA2024070312250.md): Duct · blown · Jul 3, 2024 · N378QS · Cessna 680CE · Pneumatic Distribution System
  > AT 39,000 FEET WHILE IN CRUISE WE HEARD A LOUD BANG. AT THAT TIME, CABIN ALTITUDE BEGAN RISING 750' PER MINUTE. WE WERE AT AROUND 9.0 PSI DIFFERENTIAL AROUND 6000 FEET CABIN ALT. WITHIN MINUTES WE KEPT CLIMBING TO 14000' CABIN ALTITUDE. EMERGENCY DESCENT AND
- [SDR DXTA2024061812087](https://openairdocs.org/sdr/DXTA2024061812087.md): Target · detached · Jun 18, 2024 · N378QS · Cessna 680CE · Door Warning System
  > CABIN DOOR OPEN CAS ILLUMINATED WHEN PREPARING FOR FLT. CYCLED DOOR IAW QRC. LIGHT REMAINED. PERFORMED OPS CHKS & CLOSED MED. TURNED OFF BLEED AIR & FOUND CAS MESSAGE. WENT INTO CMC & FOUND LOWER LOCK VENT DOOR SHOWING OPEN. FOUND DOOR BRUSH SEAL DAMAGED
- [SDR DXTA2024060711976](https://openairdocs.org/sdr/DXTA2024060711976.md): Proximity Switch · out of adjust · Jun 6, 2024 · N378QS · Cessna 680CE · Door Warning System
  > MAIN DOOR: CABIN DOOR OPEN CAS MESSAGE DOES NOT EXTINGUISH WHEN DOOR CLOSED. ALL DOOR LOCKED PEEPHOLE INDICATORS INDICATE LOCKED. //SIGNOFF// ADJUSTED MED VENT DOOR PROXIMITY SWITCH IAW CE-680 MM 52-10-40. OPS CHECK GOOD
- [SDR DXTA2024041011456](https://openairdocs.org/sdr/DXTA2024041011456.md): Precatch · malfunctioned · Apr 9, 2024 · N378QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR PRECATCH NOT WORKING PROPERLY. DOOR DOES NOT SET PROPERLY. VERIFIED THE PRECATCH IS INTERMITTENT, AND OCCASIONALLY BOUNCE OUT OF PRECATCH. GAINED ACCESS TO PRECATCH MECHANISM. PERFORMED RIGGING OF PRECATCH, IAW MM CHAP 52-10-00. OPS CHECK GOOD. CLOSE
- [SDR DXTA2022091270160](https://openairdocs.org/sdr/DXTA2022091270160.md): None · defective · Sep 10, 2022 · N378QS · Cessna 120 · Emergency Lighting
  > FORWARD EMERGENCY EXIT LIGHT ABOVE RIGHT WING IS MUCH DIMMER THAN THE OTHER EMERGENCY LIGHTS. // SIGNOFF// REMOVED AND REPLACED FOWARD EMER EXIT LIGHT ABOVE RIGHT WING WITH NJA PROVIDED NEW PART. OPERATIONAL CHECKS GOOD. ALL WORK COMPLETED IAW CE-680 AMM 33-5
- [SDR DXTA2022051361700](https://openairdocs.org/sdr/DXTA2022051361700.md): Light · broken · May 12, 2022 · N378QS · Cessna 680A · Emergency Lighting
  > SHARK LIGHT. EMERGENCY EXIT LIGHT IN RIGHT LANDING GEAR LENS INOP. REMOVED AND REPLACED RH EMERGENCY EXIT LIGHT IN RIGHT WING LANDING GEAR LIGHT REF E680 AMM 33-50-00. OPS CHECK GOOD AT THIS TIME.
- [SDR DXTA2022022157120](https://openairdocs.org/sdr/DXTA2022022157120.md): Not Reported · not reported · Feb 20, 2022 · N378QS · Cessna 680CE · Emergency Lighting
  > CABIN EMERG LIGHT: REPEAT WRITEUP. EMER LIGHTS FAILED PRE BATTERY CONNECTED TEST AND POST BATTERY CONNECTING TESTING, THEY NEVER CAME ON. ALSO, AFTER CONNECTING MAIN BATTERIES, COCKPIT MAIN BATTERY SWITCHES AND APU MASTER WERE LEFT IN "ON" POSITION BY MAINTEN
- [SDR JGVR20210420003](https://openairdocs.org/sdr/JGVR20210420003.md): Panel · corroded · Apr 20, 2021 · N378QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > FOUND 200 AREAS OF CORROSION ON INNER THRESHOLD PANELS. REMOVED PAINT FROM SUSPECT AREAS ON INNER THRESHOLD PANELS AND FOUND 180 AREAS THAT WERE BEYOND SURFACE CORROSION. MATCH DRILLED AND TRIMMED NEW FWD(P/N: 6911084-11), CENTER(P/N: 6911084-5), AFT(P/N: 6911
- [SDR JGVR20210420002](https://openairdocs.org/sdr/JGVR20210420002.md): Link · corroded · Apr 20, 2021 · N378QS · Cessna 680CE · Main Landing Gear
  > FOUND PITTING CORROSION ON TRAILING LINK UPPER LUGS. REPLACED RH MLG TRAILING LINK ASSEMBLY AND INSTALLED CUSTOMER SUPPLIED INSPECTED TRAILING LINK ASSEMBLY IN SAME LOCATION IAW CESSNA 680 MM 32-10-00.
- [SDR JGVR20210420001](https://openairdocs.org/sdr/JGVR20210420001.md): Skin · corroded · Apr 20, 2021 · N378QS · Cessna 680CE · Wing, Plate/Skin
  > MECHANICALLY BLENDED MULTIPLE SPOTS OF VERIFIED CORROSION ON LH WING UPPER SKIN WHERE FWD AND AFT DRAG ANGLES ATTACH. FOUND CORROSION BLENDS UNDERNEATH AFT AND FWD DRAG ANGLES TO TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS. COMPARED CORROSION BLEND MEASUREMENTS
- [SDR DXTA2021033040260](https://openairdocs.org/sdr/DXTA2021033040260.md): Pressure Switch · defective · Mar 20, 2021 · N378QS · Cessna 680CE · Aircraft Fuel Distribution System
  > FUEL PRESSURE LOW R AMBER CAS: CLIMBING OUT OF 370 AMBER CAS MESSAGE CAME ON WHILE READING CHECKLIST LIGHT WENT OUT, WE LEVELED OFF AT 400 AMBER CAS MESSAGE CAME BACK ON AND STAYED ON COMPLETED THE CHECK LIST WITH NO OTHER PROBLEMS SIGN OFF. OPENED THE RT ENG
- [SDR JGVR20180126005](https://openairdocs.org/sdr/JGVR20180126005.md): Skin · corroded · Jan 26, 2018 · N378QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON TOP OF THE RT HORIZONTAL STAB PANEL 352AC. REMOVED MINOR CORROSION AND APPLIED PROTECTIVE TREATMENT TO BARE METAL. CORROSION DETERMINED TO BE BEYOND LIMITS. BLENDED CORROSION AND POLISHED AREA TO 20:1 RATIO AND VERIFIED SURFACE CRACK AND CORRO
- [SDR JGVR20180126004](https://openairdocs.org/sdr/JGVR20180126004.md): Skin · corroded · Jan 26, 2018 · N378QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON TOP OF LT HORIZONTAL STAB PANEL 351AC. REMOVED MINOR CORROSION. PERFORMED AN EDDY CURRENT CHECK OF BLENDED AREA. INSPECTION REVEALED NO CRACKS OR CORROSION INDICATIONS. PERFORMED AN ULTRASONIC THICKNESS CHECK ON BLENDED AREA. READINGS WERE RE
- [SDR DXTR2017051705](https://openairdocs.org/sdr/DXTR2017051705.md): Cowling · delaminated · May 17, 2017 · N378QS · Cessna 680CE · Engine Cowling System
  > THE LT ENGINE UPPER COWLING HAS AN AREA OF DELAMINATION ON THE INNER SURFACE. THE DAMAGE MEASURES APPROXIMATELY 18.0 INCHES BY 12.0 INCHES. AQRD ERO-895901 PROVIDED ENGINEERING FOR A ONE-TIME FLIGHT TO MOVE THE AIRCRAFT TO KADS WHERE A PERMANENT REPAIR WILL B
- [SDR DXTR2017051703](https://openairdocs.org/sdr/DXTR2017051703.md): Skin · corroded · May 17, 2017 · N378QS · Cessna 680CE · Emergency Exits
  > ESCAPE HATCH ASSY HAS THREE (3) AREAS OF MINOR LEVEL 1 CORROSION ON EXTERIOR SKIN. AQRD ERO-895800 PROVIDES ENGINEERING FOR A PERMANENT MAJOR REPAIR IN ZONE 284 AT WL 154, WL 126, & WL 120.5.
- [SDR DXTR2017051702](https://openairdocs.org/sdr/DXTR2017051702.md): Stinger · corroded · May 17, 2017 · N378QS · Cessna 680CE · Aerodynamic Fairings
  > TAIL STINGER ASSY HAS SEVERAL AREAS OF MINOR LEVEL 1 CORROSION ON THE LH SIDE AT FS 718-725 ZONE 331. AQRD ERO-895673 PROVIDED ENGINEERING FOR A PERMANENT REPAIR.
- [SDR DXTR2017051701](https://openairdocs.org/sdr/DXTR2017051701.md): Skin · corroded · May 17, 2017 · N378QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > SURFACE CORROSION FOUND ON LEFT HAND & RIGHT HAND NOSE SKINS ADJACENT TO THE FORWARD & AFT DOOR LATCHES FOR THE AVIONICS DOORS & ON THE AFT BAGGAGE DOOR SKIN DESCRIBED AS ZONES 213, 214, & 831. MEMO DQ8188 DATED 5/16/17 ADDRESSED MINOR CORROSION TO BE TREATED
- [SDR 2017F00073](https://openairdocs.org/sdr/2017F00073.md): Fitting · corroded · Mar 16, 2017 · N378QS · Cessna 680CE · Wing, Attach Fittings
  > CORROSION AT LOWER FITTING IN LEFT WING CENTER SPAR.
- [SDR DXTA221701230660](https://openairdocs.org/sdr/DXTA221701230660.md): Circuit Board · failed · Jan 22, 2017 · N378QS · Cessna 680CE · Landing Gear System Wiring
  > DURING CLIMBOUT THRU 8000 FEET, WOW MISCOMPARE AMBER CAS MESSAGE ILLUMINATED. PERFORMED QRH CHECKLIST. ON GEAR EXTENSION, MESSAGE EXTINGUISHED, THEN CAME BACK ON SHORT FINAL. HAD NO NOSEWHEEL TILLER STEERING, ALL OTHER SYSTEMS NORMAL. DURING TAXI IN MESSAGE
- [SDR DXTR2015030301](https://openairdocs.org/sdr/DXTR2015030301.md): Riser · bent · Mar 3, 2015 · N378QS · Cessna 680CE · Passenger/Crew Doors
  > UPPER FOLDING ENTRY DOOR STEP RISER BENT. R & R FOLDING ENTRY DOOR STEP IAW 52-10-02 MM.
- [SDR DXTA2015021205976](https://openairdocs.org/sdr/DXTA2015021205976.md): Unknown · odor · Feb 11, 2015 · N378QS · Cessna 680CE · Air Distribution System
  > WITH THE APU RUNNING & BLEED AIR TURNED ON, SMOKE WITH A BURNING ODOR IMMEDIATELY FILLED THE COCKPIT & CABIN. RAN LT & RT ENGS TO ISOLATE DISCREPANCY, NOTED NO ODOR OR SMOKE. RAN APU & TURNED BLEED AIR ON, NOTED SLIGHT ODOR BUT NO SMOKE. REMOVED APU ACCESS
- [SDR CWQR20140625003](https://openairdocs.org/sdr/CWQR20140625003.md): Skin · damaged · Jun 25, 2014 · N378QS · Cessna 680CE · Elevator, Plate/Skin
  > AIRCRAFT WAS IN MX TO TROUBLESHOOT A PITCH TRIM DISCREPANCY. THE TECHNICIAN WORKING THE PROBLEM NOTICED A DENT ON THE BOTTOM OTBD END OF RT ELEVATOR & TOUCHUP PAINT. REMOVED PAINT WITH PAINT STRIPPER FROM THE DENT AREA. FOUND A RUBBER SUBSTANCE UNDER PAINT
- [SDR CWQR20130311020](https://openairdocs.org/sdr/CWQR20130311020.md): Heat Exchanger · cracked · Mar 11, 2013 · N378QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 2 CRACKS ABOUT.30" LONG. A NEW HEAT EXCHANGER WAS INSTALLED. WE PREFORMED A LEAK CHECK ON THE DEFEC
- [SDR CWQR20130311019](https://openairdocs.org/sdr/CWQR20130311019.md): Heat Exchanger · cracked · Mar 11, 2013 · N378QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION, WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 4 CRACKS ABOUT.30" LONG. A NEW HEAT EXCHANGER WAS INSTALLED. WE PREFORMED A LEAK CHECK ON THE DEF
- [SDR CWQR20130204007](https://openairdocs.org/sdr/CWQR20130204007.md): Heat Exchanger · cracked · Feb 4, 2013 · N378QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION, REPLACED A DUCT ASSY OFF OF THE HEAT EXCHANGER WITH AN IMPROVED DUCT ASSY. AT DISASSEMBLY, DISCOVERED THAT LT HEAT EXCHANGER HAD CRACKS FROM THE BOLT ATTACH POINTS. THE CRACKS WERE FROM.25 TO.75 IN LENGTH. IT APPEARS THE CR
- [SDR DXTA2012070305026](https://openairdocs.org/sdr/DXTA2012070305026.md): Control Valve · inoperative · Jun 22, 2012 · N378QS · Cessna 680CE · Cabin Pressure Control System
  > AMBER CABIN ALTITUDE CAS MESSAGE ILLUMINATED AT APPROX 36,000 FT, FOLLOWED SHORTLY AFTER BY THE RED CABIN ALTITUDE CAS MESSAGE. PERFORMED PRESSURIZATION CONTROLLER BUILT-IN-TEST. NO DEFECTS NOTED. PERFORMED MANUAL PRESSURIZATION OF ACFT WITH APU. NO EXTERN
- [SDR DXTA2012062505009](https://openairdocs.org/sdr/DXTA2012062505009.md): Warning Message · illuminated · Jun 22, 2012 · N378QS · Cessna 680CE · Cabin Pressure Control System
  > AMBER CABIN ALTITUDE CAS MESSAGE ILLUMINATED AT APPROX 36,000 FEET FOLLOWED SHORTLY THEREAFTER BY THE RED CABIN ALTITUDE CAS MESSAGE.
- [SDR 2010F00128](https://openairdocs.org/sdr/2010F00128.md): Diffuser · cracked · Jun 17, 2010 · N378QS · Cessna 680CE · Wing Main, Frame Structure
  > ((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOC
- [SDR 2010F00127](https://openairdocs.org/sdr/2010F00127.md): Diffuser · cracked · Jun 17, 2010 · N378QS · Cessna 680CE · Wing Main, Frame Structure
  > ((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOC
- [SDR 2010F00126](https://openairdocs.org/sdr/2010F00126.md): Diffuser · cracked · Jun 17, 2010 · N378QS · Cessna 680CE · Airfoil Anti/De-ice System
  > ((JGVR)) FOUND THESE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE D
- [SDR 2010F00125](https://openairdocs.org/sdr/2010F00125.md): Diffuser · cracked · Jun 17, 2010 · N378QS · Cessna 680CE · Wing Main, Frame Structure
  > ((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOC
- [SDR DXTA2010040804063](https://openairdocs.org/sdr/DXTA2010040804063.md): Uplock · sticking · Apr 7, 2010 · N378QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > LANDING GEAR INDICATED UNSAFE (RED LIGHT) DURING RETRACTION. ADDITIONALLY, A LOUD THUMPING NOISE WAS HEARD COMING FROM THE NOSE GEAR AREA. CHECKED NOSE STRUT SERVICING, FOUND WITHIN LIMITS. CHECKED UPLOCK SWITCHES FOR PROPER GROUNDS AT PCB'S, FOUND NORMAL. CH
- [SDR DXTA2010011203943](https://openairdocs.org/sdr/DXTA2010011203943.md): Packing · failed · Jan 11, 2010 · N378QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > WHEN GEAR WAS SELECTED UP, ONLY THE NOSE GEAR CAME UP. TROUBLESHOT SYS AND FOUND NOSE STRUT NO FULLY EXTENDED W/ACFT ON JACKS. CK'D STRUT SERVICING AND FOUND NO PRESSURE IN LOWER CHAMBER. DISASSEMBLED LOWER PISTON FORK ASSY AND REPACKED IAW CMM 32-20-01. REAS
- [SDR DXTA2009112003865](https://openairdocs.org/sdr/DXTA2009112003865.md): Line · leaking · Nov 19, 2009 · N378QS · Cessna 680CE · Hydraulic System, Main
  > LOSS OF HYD CONTENT ON APPROACH TO LAND. AFTER LANDING GEAR WAS SELECTED DOWN. COMPLETED APPROIATE CHECKLIST AND LANDED ACFT USING EMERGENCY BRAKE TO STOP ON RUNWAY. HYD LEAK IN NOSE GEAR WELL. FOUND NOSE WHEEL STEERING UNIT CENTERING LINE RUPTURED AT UPPE
- [SDR DXTA2009102903831](https://openairdocs.org/sdr/DXTA2009102903831.md): Actuator · inoperative · Oct 28, 2009 · N378QS · Cessna 680CE · Landing Gear Steering System
  > ON DEPARTURE NOSE GEAR FAILED TO RETRACT. THE MAINS CAME UP FINE. FOUND NOSE WHEEL STEERING ACTUATOR TO BE FAULTY, REMOVED ACUATOR, AND REPLACED WITH A SERVICABLE NOSE GEAR STEERING ACUATOR. WORK DONE IAW THE MM 32-50-00. OPERATIONAL CHECKS, AND LEAK CHECKS
- [SDR DXTA200802783](https://openairdocs.org/sdr/DXTA200802783.md): Actuator · activated · Jan 21, 2008 · N378QS · Cessna 680CE · Landing Gear Actuator
  > ON GEAR EXTENTION THE RT GEAR INDICATED NOT DOWN AND LOCKED. REMOVED AND INSTALLED A RENTAL ACTUATOR PER MM 32-30-40 AND OPERATIONAL CHECKED PER MM 32-00-00 GROUND OPERATIONAL CHECKED GOOD.
- [SDR DXTA200702522](https://openairdocs.org/sdr/DXTA200702522.md): Landing Gear · inoperative · Oct 3, 2007 · N378QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO RETRACT LANDING GEAR. 10-29-07 ADJUSTED NOSE LANDING GEAR SQUAT SWITCH. OPS CHECKED GOOD. WORK DONE IAW 680 M.M. CHAPTER 32-60-00.

## 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 = 'N378QS' AND deregistration_id = 'N378QS-2026-07-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N378QS-2026-07-02/reports

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