# Service difficulty reports: N370QS, cancelled Jul 28, 2025

A list on [N370QS, cancelled Jul 28, 2025](https://openairdocs.org/deregistered/N370QS-2025-07-28.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 · 54 reports

- [SDR DXTA2024120201355](https://openairdocs.org/sdr/DXTA2024120201355.md): Counterbalance · out of adjust · Dec 1, 2024 · N370QS · Cessna 680SOV · Passenger/Crew Doors
  > ENTRANCE STAIR: COUNTER BALANCE ON MAIN CABIN DOOR. DOOR IS VERY HEAVY TO CLOSE AND FALLS OPEN EASILY. CORRECTIVE ACTION; ADJUSTED BOTH REELS OPS CHECK GOOD. ALL WORK DONE IN REF, TO CE-680 AMM 52-10-50.
- [SDR 2024F00296](https://openairdocs.org/sdr/2024F00296.md): Skin · nicked · Nov 20, 2024 · N370QS · Gulstm 680 · Vertical Stabilizer, Plate/Skin
  > DURING ELEVATOR TRAVEL CHECKS NOTICED SKIN DAMAGE AROUND THE TRIM ACTUATOR COVE AREA. UPPER ELEVATOR SKIN AND LOWER TRIM ACTUATOR COVE SKIN.
- [SDR 2024F00295](https://openairdocs.org/sdr/2024F00295.md): Spar · chafed · Nov 20, 2024 · N370QS · Gulstm 680 · Vertical Stabilizer, Spar/Rib
  > WHILE ACCOMPLISHING ELEVATOR TRAVEL CHECKS FOUND ELEVATOR CONTROL HORNS HITTING HILOCKS PREVENTING FULL TRAVEL, NEED TO LOOK INTO AQRD REPAIR DEFINITION OF VERTICAL REPAIR.
- [SDR JGVR20231114002](https://openairdocs.org/sdr/JGVR20231114002.md): Unknown · unknown · Nov 14, 2023 · N370QS · Cessna 680A · Horizontal Stabilizer Structure
  > LH/RH H STAB UPPER AND LOWER SKINS ON THE TRAILING EDGE HAVE MULTIPLE AREAS OF CORROSION. MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION ON LH AND RH, UPPER AND LOWER HORIZONTAL STABILIZER TRAILING EDGE SKINS IAW CESSNA 680 SRM 51-70-02. AREAS DETERMINED TO
- [SDR JGVR20231114001](https://openairdocs.org/sdr/JGVR20231114001.md): Unknown · unknown · Nov 14, 2023 · N370QS · Cessna 680A · Horizontal Stabilizer, Plate/Skin
  > REPAIRED HORIZONTAL STABILIZER RH LOWER SKIN DUE TO LEVEL 2 CORROSION. MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION ON RH LOWER HORIZONTAL STABILIZER TRAILING EDGE SKINS. INSTALLED 2 001 DOUBLERS ON LOWER SIDE OF RH HORIZONTAL STAB WITH CR3524-4 AND CSR904
- [SDR JGVR20231113001](https://openairdocs.org/sdr/JGVR20231113001.md): Unknown · unknown · Nov 13, 2023 · N370QS · Cessna 680A · Vertical Stabilizer, Spar/Rib
  > RH VERT AFT SPAR IS HEAVILY CORRODED. LOCATED ABOVE RUDDER UPPER HINGE. REPAIRED 2 BLENDED AREAS OF VERTICAL STABILIZER R/H AFT SPAR CAP AT APPROXIMATELY VFS 172 AND VFS 237 DUE TO CORROSION PER AQRD ERO-108612 REV. IR, TITLED,"RFTS-108612 - N370QS - VERTICAL
- [SDR JGVR20231005002](https://openairdocs.org/sdr/JGVR20231005002.md): Unknown · unknown · Oct 5, 2023 · N370QS · Cessna 680CE · Rudder, Plate/Skin
  > REPAIRED CORRODED AREAS ON THE RUDDER LEADING EDGE NEAR THE BALANCE WEIGHT HARDWARE BY BLENDING AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIMING AND INSTALLING REPAIR DOUBLERS PER NETJETS REQUEST FOR
- [SDR JGVR20201104005](https://openairdocs.org/sdr/JGVR20201104005.md): Support Bracket · corroded · Nov 4, 2020 · N370QS · Cessna 680CE · Vertical Stabilizer
  > FOUND LT AND RT LOWER RUDDER SUPPORT BRACKETS CORRODED BEYOND REPAIR AND REPLACED WITH NEW CESSNA P/NS 6931045-17 AND 69031045-18.
- [SDR JGVR20201104004](https://openairdocs.org/sdr/JGVR20201104004.md): Plate · corroded · Nov 4, 2020 · N370QS · Cessna 680CE · Vertical Stabilizer
  > FOUND SEVERE CORROSION OF THE UPPER RIB PLATE OF THE VERTICAL STABILIZER’S RUDDER TRIM ACTUATOR MOUNT, REPLACED WITH A NEW CESSNA P/N 6961526-5 WET WITH PS870B SEALANT USING NEW HL40-4 HI-LOK PINS WITH NEW HL97DU4 COLLARS AND NAS1097AD4 SOLID RIVETS, REFERENCI
- [SDR JGVR20201104003](https://openairdocs.org/sdr/JGVR20201104003.md): Skin · corroded · Nov 4, 2020 · N370QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED CORRODED AREA ON THE UPPER SURFACE OF THE UPPER WING SKIN, JUST INBOARD OF THE LT OVER-WING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED REPAIR AREA, PER TEXTRON REPAIR.
- [SDR JGVR20201104002](https://openairdocs.org/sdr/JGVR20201104002.md): Spar Cap · corroded · Nov 4, 2020 · N370QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > BLENDED MULTIPLE CORRODED AREAS ON THE LT AND RT SPAR CAPS AND WEB OF THE VERTICAL STABILIZER AFT SPAR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED AND/OR CORRODED FASTENERS AS REQUIRED, TREATED AND PRIMED REPAIR AREAS, PER TEXTRON REP
- [SDR JGVR20201104001](https://openairdocs.org/sdr/JGVR20201104001.md): Skin · corroded · Nov 4, 2020 · N370QS · Cessna 680CE · Wing, Plate/Skin
  > REMOVED THE LT UPPER WING DRAG MIDDLE AND AFT ANGLES (WING-TO-FUSELAGE FAIRINGS) AND BLENDED CORRODED AREAS OF THE UPPER SURFACE OF THE LT UPPER WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED 17 CORRODED HI-LOCS IN THE REPAIR AREA. TR
- [SDR 2020FA0000217](https://openairdocs.org/sdr/2020FA0000217.md): Inlet · damaged · Apr 6, 2020 · N370QS · Cessna 680CE · Engine Air Intake System
  > LH ENGINE INLET DUCT DEEP COUNTERSINK. REFERENCE TEXTRON AVIATION ENGINEERING MEMO: DQ25329M1 RRL DATED: 3/31/2020.
- [SDR 2020FA0000216](https://openairdocs.org/sdr/2020FA0000216.md): Skin · corroded · Apr 6, 2020 · N370QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STABILIZER UPPER SKIN CORROSION. REFERENCE FAA FORM 8100-9, FR-680-0099-7851 REV- DATED: 4/3/2020.
- [SDR 2020FA0000215](https://openairdocs.org/sdr/2020FA0000215.md): Skin · corroded · Apr 6, 2020 · N370QS · Cessna 680CE · Wing, Plate/Skin
  > MINOR CORROSION AROUND HILOCK COLLARS IN LH AND RH MLG WHEEL WELL ABOVE TRUNNION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ25322M1 RRL DATED: APRIL 1, 2020.
- [SDR 2020FA0000214](https://openairdocs.org/sdr/2020FA0000214.md): Door · corroded · Apr 6, 2020 · N370QS · Cessna 680CE · Emergency Exits
  > EMERGENCY EXIT DOOR CORROSION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ25313M1 RRL DATED: MARCH 31, 2020.
- [SDR DXTA2019121203190](https://openairdocs.org/sdr/DXTA2019121203190.md): Unknown · odor · Dec 11, 2019 · N370QS · Cessna 680CE · Air Distribution System
  > COCKPIT ODOR BURNING SMELL - BURNING ODOR NOTICED BY CREW AT 11000 FEET IN CRUISE. SOURCE COULD NOT BE IDENTIFIED AND CRASH/FIRE/RESCUE COULD NOT IDENTIFY A HEAT SOURCE. CFR NOTICED THE ODOR EVEN AFTER AIRCRAFT ON THE GROUND WITH CABIN DOOR OPEN. A LIGHT HAZE
- [SDR 2019F00205](https://openairdocs.org/sdr/2019F00205.md): Fairing · cracked · May 15, 2019 · N370QS · Cessna 680SOV · Aerodynamic Fairings
  > LT LOWER WING FAIRING TRIM CRACK REPAIR RFTS-103325 REV 0 DATED MAY 15, 2019.
- [SDR 2019F00193](https://openairdocs.org/sdr/2019F00193.md): Truss · corroded · May 6, 2019 · N370QS · Cessna 680CE · Nacelle/Pylon, Attach Fittings
  > APU TRUSS MOUNT (FLANGE) CORROSION. REFERENCE ENGINEERING MEMO DQ19368M1 DATED: MAY 3, 2019.
- [SDR DXTA2019011001901](https://openairdocs.org/sdr/DXTA2019011001901.md): Display · overheated · Jan 10, 2019 · N370QS · Cessna 680CE · Central Display
  > DU3 WENT BLANK AND ELECTRICAL SMOKES FUMES NOTICED CLIMBING THROUGH FL360. RAN EMERGENCY CHECKLIST AND DIVERTED INTO KFSM. **SUPPLEMENTAL INFORMATION: REMOVED & INSPECTED NR 3 DU, FOUND TO BE INTERNALLY FAILED & SMELLED FRIED. REMOVED & REPLACED NR 3 DU IAW MM
- [SDR DXTA2018123101854](https://openairdocs.org/sdr/DXTA2018123101854.md): Actuator · faulty · Dec 31, 2018 · N370QS · Cessna 680CE · Landing Gear Actuator
  > AFTER RETRACTING THE GEAR ON TAKEOFF, THE LEFT MAIN INDICATOR CONTINUED TO SHOW IT WAS DOWN AND LOCKED. WE DIDN'T HAVE A RED UNLOCK, OR ANY HORN. PER THE CHECKLIST PROCEDURE, GEAR WAS EXTENDED AND SHOWED ALL NORMAL INDICATORS **SUPPLEMENTAL INFORMATION: REMOVE
- [SDR JGVR20171206002](https://openairdocs.org/sdr/JGVR20171206002.md): Axle · corroded · Dec 6, 2017 · N370QS · Cessna 680CE · Main Landing Gear Strut/Axle/Truck
  > LH MLG AXLE HAS AREAS OF MISSING CHROME AND RUST. REMOVED LH MLG TRAILING LINK FOR AXLE REPLACEMENT AND FOUND BOTH TRUNNION LUGS TO BE CORRODED ON OUTER SURFACES. REPLACE LH MLG TRUNNION AND TRAILING LINK ASSEMBLIES. REMOVED LH MLG TRUNNION AND TRAILING LINK
- [SDR JGVR20171206001](https://openairdocs.org/sdr/JGVR20171206001.md): Panel · corroded · Dec 2, 2017 · N370QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > LEVEL 1 CORROSION AROUND MULTIPLE FASTENERS ON LH AND RH H-STAB IB CLOSEOUT PANELS 351AC AND 352AC. BLENDED LEVEL 1 CORROSION AROUND MULTIPLE FASTENERS ON LH AND RH H-STAB IB CLOSEOUT PANELS 351AC AND 352AC. APPLIED ALODINE, CORROSION RESISTANT PRIMER, AND TOP
- [SDR DXTA2017031906386](https://openairdocs.org/sdr/DXTA2017031906386.md): Circuit Board · failed · Mar 19, 2017 · N370QS · Cessna 680CE · Fire Protection System Wiring
  > ENGINE FIRE DETECT FAIL LEFT CAS MESSAGE DISPLAYED INFLIGHT. CB TRIPPED. TROUBLESHOT TO LEFT ENG FIRE & SMOKE PRINTED CIRCUIT BOARD. REMOVED AND REPLACED THE PCB IAW MM 24-60-10. OPS CHECKED GOOD.
- [SDR JGVR201609210008](https://openairdocs.org/sdr/JGVR201609210008.md): Attach Angle · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Aerodynamic Fairings
  > CORROSION ON UPPER TAIL CONE COVER FAIRING ATTACH ANGLES. THE AREAS THAT CORRODE ONLY HAVE PRIMER PAINT. SHOULD BE PAINTED WITH AN ADDITIONAL CORROSION RESISTANT PAINT FOR A TOP COAT TO PREVENT CORROSION.
- [SDR JGVR201609210007](https://openairdocs.org/sdr/JGVR201609210007.md): Spar Web · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Wing Spar
  > CORROSION ON THE FORWARD WEB IN LT WHEEL WELL AROUND LT INBD BRAKE FITTING. SUGGEST APPLYING CPC TO WHEEL WELL SPARS.
- [SDR JGVR201609210006](https://openairdocs.org/sdr/JGVR201609210006.md): Fitting · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Wing Miscellaneous Structure
  > CORROSION FOUND AROUND EMERGENCY BRAKE LINE FITTING ON OTBD SIDE OF WS 37.00 IN RT MLG WHEEL WELL. SUGGEST APPLYING CPC IN WHEEL WELLS.
- [SDR JGVR201609210005](https://openairdocs.org/sdr/JGVR201609210005.md): Spar Web · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Wing Spar
  > CORROSION ON THE FORWARD WEB IN THE RT MLG WHEEL WELL AROUND THE RT INBD BRAKE FITTING. SUGGEST APPLYING CPC ON THE WHEEL WELL SPARS.
- [SDR JGVR201609210004](https://openairdocs.org/sdr/JGVR201609210004.md): Thrust Reverser · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Engine Thrust Reverser
  > CORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER LOWER BUCKETS. SUGGEST PAINTING WITH A HIGH TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT IS USED ON THE INSIDE OF THE AFTER BODIES.
- [SDR JGVR201609210003](https://openairdocs.org/sdr/JGVR201609210003.md): Thrust Reverser · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Engine Thrust Reverser
  > CORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER BUCKETS. SUGGEST PAINTING WITH A HIGHER TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT IS USED ON THE INSIDE OF THE AFTER BODIES.
- [SDR JGVR201609210002](https://openairdocs.org/sdr/JGVR201609210002.md): Skin · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Elevator, Plate/Skin
  > CORROSION ON UPPER SURFACE OF LT ELEVATOR FORWARD OF TRIM TAB.
- [SDR JGVR201609210001](https://openairdocs.org/sdr/JGVR201609210001.md): Thrust Reverser · corroded · Sep 21, 2016 · N370QS · Cessna 680CE · Engine Thrust Reverser
  > CORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER LOWER BUCKETS. SUGGEST PAINTING WITH A HIGH TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT IS USED ON THE INSIDE OF THE AFTER BODIES.
- [SDR DXTA2015110606118](https://openairdocs.org/sdr/DXTA2015110606118.md): Circuit Board · failed · Nov 7, 2015 · N370QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > UPON GEAR RETRACTION, ENCOUNTERED A LOUD CONTINUOUS BANGING NOISE ALONG WITH SEVERE VIBRATIONS. RED GEAR UNLOCK LIGHT REMAINED ON UNTIL THUMPING STOPPED. PROBLEM APPEARED TO BE COMING FROM THE NOSE WHEEL. DECLARED AN EMERGENCY & LANDED UNEVENTFULLY. INSPE
- [SDR DXTA2014102805918](https://openairdocs.org/sdr/DXTA2014102805918.md): Fire Warning · false activation · Oct 27, 2014 · N370QS · Cessna 680CE · Fire Detection
  > AMBER CAS MESSAGE FOR RT ENGINE FIRE DETECTION ILLUMINATED INFLIGHT 15 - 20 TIMES. PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE FAULT. MEASURED RESISTANCE OF RT ENGINE OUTTER FIRE LOOP, ALL READERS WITH IN LIMITS PER AMM 26-10-30, REMOVED COCKPIT RT CIRCUIT
- [SDR DXTA2014100105902](https://openairdocs.org/sdr/DXTA2014100105902.md): Module · failed · Sep 30, 2014 · N370QS · Cessna 680CE · Fire Detection
  > AMBER CAS MESSAGE FOR THE RT ENGINE FIRE DETECTION FAILED ILLUMINATED 15 MINUTES INTO FLIGHT. RAN ENGS & ATTEMPTED TO DUPLICATE SQUAWK. NO FAIL LIGHT PRESENT AFTER EXTENSIVE RUNS & TAXIING. REPLACED THE RT FIRE DETECTION CIRCUIT BREAKER & THE CUSTOM VO BOA
- [SDR DXTA2014092905898](https://openairdocs.org/sdr/DXTA2014092905898.md): Fire Detector · failed · Sep 26, 2014 · N370QS · Cessna 680CE · Fire Detection
  > AMBER ENGINE FIRE DETECTOR FAILED RT CAS MESSAGE ILLUMINATED DURING FLIGHT. RANG OUT INNER FIRE LOOP, RINGS GOOD. INSPECTED WIRING HARNESS, NO DAMAGE FOUND. R & R INNER FIRE LOOP IAW MM 26-10-1. OPS CHECKED GOOD. RAN ACFT & CHECKED FOR BLEED LEAKS. OP
- [SDR DXTA2014092505892](https://openairdocs.org/sdr/DXTA2014092505892.md): Printed Ckt Board · faulty · Sep 23, 2014 · N370QS · Cessna 680CE · Fire Detection
  > DURING INITIAL CLIMB OUT ENG FIRE DETECT FAIL R CAS MSG POSTED. THE MSG CLEARED & RE-POSTED SEVERAL TIMES DURING FLIGHT. THIS WAS NOT ASSOCIATED WITH ANY THROTTLE MOVEMENTS. PERFORMED ENG FIRE DETECT FUNCTIONAL CHECK WITH NO DEFECTS FOUND. ACCESSED COMS &
- [SDR DXTA2014092205890](https://openairdocs.org/sdr/DXTA2014092205890.md): Fire Loop · faulty · Sep 21, 2014 · N370QS · Cessna 680CE · Fire Detection
  > UPON DEPARTURE ENG FIRE DETECT FAIL R ILLUMINATED STEADY. DURING DESCENT BECAME INTERMITTENT & EXTINGUISHED ITSELF ON SHORT FINAL. R & R RT ENG FIRE LOOP IAW MM 26-10-30. OPERATIONS CHECKED GOOD.
- [SDR 2014F00140](https://openairdocs.org/sdr/2014F00140.md): Coalescer Bag · dirty · Jul 19, 2014 · N370QS · Cessna 680SOV · Humidity Control System
  > TWENTY MINUTES AFTER TAKEOFF AND CRUISING AT 15,000 FT, THE APU WAS STARTED AND A STRONG ELECTRICAL BURNING ODOR WAS NOTED. THE BLEED AIR WAS TURNED OFF AND APU SHUTDOWN. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN ACFT AND INSPECTED ACFT, COULD
- [SDR DXTA2014072105823](https://openairdocs.org/sdr/DXTA2014072105823.md): Coalescer Bag · dirty · Jul 19, 2014 · N370QS · Cessna 680CE · Humidity Control System
  > TWENTY MINUTES AFTER TAKEOFF AT 15000 FT, APU STARTED USING THE APPROPRIATE CHECKLIST. AFTER THE APU STABILIZED & THE BUSS TIE WAS OPENED, A STRONG BURNING ELECTRICAL ODOR WAS NOTED. BLEED AIR WAS OFF. APU WAS IMMEDIATELY SHUTDOWN. DIVERTED TO THE NEARES
- [SDR DXTA2014060505793](https://openairdocs.org/sdr/DXTA2014060505793.md): Brake Assy · worn · Jun 4, 2014 · N370QS · Cessna 680CE · Landing Gear Brake System
  > BRAKES CHATTER AT SLOW SPEED COMING TO A COMPLETE STOP, FEEL GRABBY DURING TAXI, PULLS TO THE LEFT DURING DECELERATION. INSPECTED BRAKES, FOUND NR 2 BRAKE LEFT INBD WEAR PIN FLUSH WITH HOUSING. REMOVED WORN BRAKE & INSTALLED AN OVERHAULED BRAKE ASSEMBLY.
- [SDR CWQR20131031048](https://openairdocs.org/sdr/CWQR20131031048.md): Solenoid · binding · Oct 31, 2013 · N370QS · Cessna 680CE · Passenger/Crew Doors
  > ACFT LANDED, AFTER ENGINES WERE SHUTDOWN, CREW WAS UNABLE TO OPEN CABIN DOOR. LINE CREW AND TECHNICIANS WERE NOT ABLE TO OPEN THE DOOR FROM THE OUTSIDE HANDLE. EGRESS WAS MADE BY EMERGENCY EXIT. TROUBLESHOT SYSTEM, FOUND THAT THE MCD ROTARY SOLENOID WOULD
- [SDR 2013FA0000512](https://openairdocs.org/sdr/2013FA0000512.md): Actuator · malfunctioned · Sep 12, 2013 · N370QS · Cessna 680CE · Alternator-Generator Drive
  > THE AILERON TRIM ACTUATOR WAS INSTALLED ON THE RT AILERON. AFTER THE INSTALLATION, IT WAS FOUND THAT THE COCKPIT EICAS DISPLAY SHOWED THE INDICATOR MOVING IN THE OPPOSITE DIRECTION OTHER THAN WAS SELECTED. FURTHER TROUBLESHOOTING REVEALED THAT THE AILERON TR
- [SDR DXTA2011120104807](https://openairdocs.org/sdr/DXTA2011120104807.md): Display · failed · Nov 30, 2011 · N370QS · Cessna 680CE · Central Warning
  > NR 1MCDU SCREEN GOES BLANK FOLLOWED BY ELECTRICAL SMOKE EMINATING WITHIN THE COCKPIT. AFTER POWER UP WITH AVIONICS ON, FLIGHT PLAN PROGRAMMED AND READY TO GO. NR 1 MCDU SCREEN SUDDENLY GOES BLANK. THE ODOR OF ELECTRICAL SMOKE BEGINS AND THE EICAS MOMENTARILY D
- [SDR DXTA2011031604509](https://openairdocs.org/sdr/DXTA2011031604509.md): Display · failed · Mar 15, 2011 · N370QS · Cessna 680CE · Central Display
  > DURING CRUISE FLIGHT, DU NR 2 WENT BLACK ACCOMPANIED BY A SMALL AMOUNT OF ELECTRICAL SMOKE AND ODOR. WHILE ACCOMPLISHING THE ELECTRICAL SMOKE OR FIRE CHECKLIST, UPON SELECTION OF EICAS BUTTON OFF, THE "REMOTE CB TRIPPED" CAS MESSAGE DISPLYED AND ALL ELECTRICAL
- [SDR DXTA2010072604174](https://openairdocs.org/sdr/DXTA2010072604174.md): Anti-Skid Sys · failed · Jul 24, 2010 · N370QS · Cessna 680CE · Brake Anti-Skid Section
  > ANTI-SKID FAILED ON TAKEOFF ROLL AT 45 KTS. ABORTED TAKEOFF, MESSAGE REMAINED ON UNTIL SPEED DROPPED BELOW 45 KTS. POWERED ACFT, NO ANTI-SKID FAIL. SPUN EACH WHEEL HOLDING BRAKES. ANTI SKID SYS OPS CHECKED GOOD. RANG OUT SKID XDRIVERS FROM CONTROL. ALL REA
- [SDR DXTA2010062804133](https://openairdocs.org/sdr/DXTA2010062804133.md): Unknown · odor · Jun 25, 2010 · N370QS · Cessna 680CE · Air Distribution System
  > CREW REPORTED PUNGENT ODOR IN COCKPIT DURING PREFLIGHT. ODOR DISSIPATED QUICKLY AFTER APU BLEED AIR WAS SELECTED ON. REMOVED ALL FOUR DISPLAY UNITS, INSPECTED DU COOLING FANS AND CLEANED. REINSTALLED DUS AND OPS CHECK GOOD IAW MM 34-23-10. GAINED ACCESS AND C
- [SDR DXTA2010010703932](https://openairdocs.org/sdr/DXTA2010010703932.md): Strut · leaking · Jan 6, 2010 · N370QS · Cessna 680CE · Main Landing Gear Strut/Axle/Truck
  > UPON LANDING GEAR RETRACTION, NOSE GEAR MADE HEAVY BANGING NOISE REPEATEDLY IN WHEEL WELL AND RED NOSE GEAR UNLOCK LIGHT REMAINED ON. EXTENDED GEAR NORMALLY AND RETURNED FOR A NORMAL LANDING. REMOVED LOWER BARREL AND REPACKED THE SEALS. INSTALLED LOWER BARR
- [SDR 2009F00108](https://openairdocs.org/sdr/2009F00108.md): Warning Light · illuminated · Nov 13, 2009 · N370QS · Cessna 680CE · Cabin Pressure Control System
  > RED CAS MESSAGE "CABIN ALTITUDE" CAME ON PASSING THRU 13,500 FT. PRESS CONTROL FAULT LIGHT WAS ON AS WELL AS CABIN DUMP SWITCH IN DUMP.
- [SDR 2008FA0000771](https://openairdocs.org/sdr/2008FA0000771.md): Rudder Pedal · jammed · Oct 26, 2008 · N370QS · Cessna 680CE · Rudder Control System
  > ON ACFT DEPARTURE, THE RUDDER PEDALS JAMMED ON THE COCKPIT SIDE PANELS ON THE TAKEOFF. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED UNEVENTFULLY. DURING THE PREVIOUS MAINT VISIT, THE RUDDER WAS REPLACED WITH A RENTAL UNIT, THE RUDDER WAS PROPERLY INSTALLED

Next page: https://openairdocs.org/deregistered/N370QS-2025-07-28/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 = 'N370QS' AND deregistration_id = 'N370QS-2025-07-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N370QS-2025-07-28/reports

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