# Service difficulty reports: N361QS

A list on [N361QS](https://openairdocs.org/aircraft/N361QS.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 · 51 reports

- [SDR DXTA2026093009937](https://openairdocs.org/sdr/DXTA2026093009937.md): Spring · broken · Sep 28, 2026 · N361QS · Cessna 680SOV · Passenger/Crew Doors
  > WHEN CLOSING THE MAIN ENTRY DOOR, THERE WAS A LOUD POP AND THE FORWARD CLOSING ASSIST CABLE BECAME SLACK. INSPECTED MED FOUND BROKEN FWD COUNTERBALANCE SPRING AND BROKEN MED OVER CENTER PUSHROD. REMOVED AND REPLACED MED FWD FAILED COUNTERBALANCE SPRING, AND
- [SDR 2026F00110](https://openairdocs.org/sdr/2026F00110.md): Landing · corroded · May 18, 2026 · N361QS · Cessna 680A · Fuselage Miscellaneous Structure
  > FOUND SIGNS OF CORROSION UNDER 9 NUTPLATES UNDER PANEL 154BC. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED WHERE 8 NUTPLATES WERE PREVIOUSLY REMOVED INSIDE FUSELAGE BAY 154BC IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESS
- [SDR 2026F00109](https://openairdocs.org/sdr/2026F00109.md): Landing · corroded · May 18, 2026 · N361QS · Cessna 680A · Fuselage Miscellaneous Structure
  > BUBBLING PRIMER AND WHITE POWDER AROUND AND UNDER 26 NUTPLATES UNDER PANEL 154AC. MECHANICALLY REMOVED CORROSION LOCATED WHERE 26 NUTPLATES WERE PREVIOUSLY REMOVED IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-7
- [SDR 2026F00108](https://openairdocs.org/sdr/2026F00108.md): Support · corroded · May 18, 2026 · N361QS · Cessna 680A · Fuselage Miscellaneous Structure
  > FOUND CORROSION UNDER MULTIPLE NUTPLATES FOR PANEL 342AB.MECHANICALLY REMOVED CORROSION LOCATED WHERE 13 NUTPLATES WERE PREVIOUSLY REMOVED ON INNER AND OUTER SKIN SURFACES INCLUDING AREAS OF CORROSION LOCATED ALONG ANGLE STRAP EDGES IAW CESSNA 680 SRM 51-70-02
- [SDR 2026F00104](https://openairdocs.org/sdr/2026F00104.md): Stringer · corroded · May 12, 2026 · N361QS · Cessna 680A · Fuselage Main, Longeron/Stringer
  > CENTER STRINGER UNDER PANEL 164BC HAS 3 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 3 AREAS AND VERIFIED CORROSION LOCATED INSIDE FUSELAGE BAY 164BC ON CENTER STRINGER. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSION
- [SDR 2026F00103](https://openairdocs.org/sdr/2026F00103.md): Landing · corroded · May 12, 2026 · N361QS · Cessna 680A · Fuselage Main, Structure
  > CORROSION ON PANEL LANDS FOR PANEL 164AC. REPAIRED CORROSION ON PANEL LANDS FOR PANEL 164AC IN REFERENCE TO NETJETS REQUEST FOR TECHNICAL SERVICES (RFTS): RFTS-117178 REV. 0; TITLED: N361QS (680-0235) PANEL 164AC NUTPLATE CORROSION; DATED: 11 MAY 2026.
- [SDR 2026F00102](https://openairdocs.org/sdr/2026F00102.md): Stringer · corroded · May 12, 2026 · N361QS · Cessna 680A · Fuselage Main, Longeron/Stringer
  > CENTER STRINGER UNDER PANEL 164AC HAS 5 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 5 AREAS LOCATED IN FUSELAGE BAY 164AC ON CENTER STRINGER AND VERIFIED CORROSION. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSION BLE
- [SDR DXTA2025052203557](https://openairdocs.org/sdr/DXTA2025052203557.md): Battery · discharged · May 19, 2025 · N361QS · Cessna 680SOV · Emergency Lighting
  > RIGHT REAR CABIN, EXTERIOR FORWARD WING AND WING INSPECTION EMERGENCY LIGHTS WOULD NOT ILLUMINATE AFTER 30 MINUTE CHARGE APPLIED AND POWER REMOVED. PERFORMED OPERATIONAL CHECK OF INTERIOR AND EXTERIOR EMERGENCY LIGHTS IAW CE-680 AMM 33-50-10. SOPS CHECK GOOD.
- [SDR DXTA2025051903541](https://openairdocs.org/sdr/DXTA2025051903541.md): Battery Pack · inoperative · May 18, 2025 · N361QS · Cessna 680SOV · Emergency Lighting
  > CABIN EMERG LIGHT: RIGHT REAR CABIN LIGHT DID NOT ILLUMINATE AFTER CHARGING FOR 30 MINUTES CORRECTIVE ACTION; C/W TC-FLT-33-1001 CESSNA 680 EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. OPS CHECK GOOD IAW CE-680 MM 33-50-00.
- [SDR 2025FA0000064](https://openairdocs.org/sdr/2025FA0000064.md): Spar · corroded · Jan 29, 2025 · N361QS · Cessna 680A · Spoilers
  > FOUND AREA OF CORROSION AROUND SPOILER EXTEND HYDRAULIC LINE FITTING ON RH WING AFT SPAR. MECHANICALLY REMOVED CORROSION WHERE SPOILER AND SPEED BRAKE HYD LINES WERE DISCONNECTED AT CARRY THRU FITTING ON AFT FACE OF AFT SPAR LOCATED ON RH WING IN INBD FLAP COV
- [SDR 2024FA0000962](https://openairdocs.org/sdr/2024FA0000962.md): Spar Cap · corroded · Dec 13, 2024 · N361QS · Cessna 680CE · Wing Spar
  > REPAIRED CORRODED AREA ON THE LH LOWER WING SPAR CAP LOCATED IN THE LH MLG WHEEL WELL BEHIND PANEL 730DL, BY R&R FASTENERS AS NEEDED, MECHANICAL BLENDS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AREAS ACCEPTABLE AREAS AS-IS.
- [SDR 2024FA0000954](https://openairdocs.org/sdr/2024FA0000954.md): Skin · corroded · Dec 10, 2024 · N361QS · Cessna 680A · Horizontal Stabilizer, Plate/Skin
  > REPAIRED SEVERAL CORRODED AREAS OF THE UPPER AND LOWER TRAILING EDGE SKINS OF THE RH HORIZONTAL STABILIZER BY BLENDING, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS IAW REQUEST FOR TECHNICAL SERVICES
- [SDR DXTA2024111401140](https://openairdocs.org/sdr/DXTA2024111401140.md): Throttle Control · faulted · Nov 13, 2024 · N361QS · Cessna 680SOV · Power Lever
  > DURING TAXI OUT AND RUDDER BIAS CHECK NOTICED RIGHT THROTTLE CATCHING AS ITS ADVANCES. FEELS LIKE IT IS BINDING ON ITSELF. CORRECTIVE ACTION; ACCESSED THROTTLE QUADRANT, REMOVED DUST COVER PLATE TO ACCESS FRICTION PLATE MECHANISM. CLEANED THROTTLE FRICTION LEV
- [SDR DXTA2024071912402](https://openairdocs.org/sdr/DXTA2024071912402.md): Door · malfunctioned · Jul 18, 2024 · N361QS · Cessna 680CE · Passenger/Crew Doors
  > ENTRANCE STAIR: MAIN CABIN DOOR VERY HEAVY WHEN CLOSING AND WHEN OPENING FALLS TO FALLS OPEN WITHOUT ANY FORCE OF THE LOCKING HANDLE. MADE ADJUSTMENST TO MED COUNTER BALANCE SYSTEM, FWD/AFT SUPPORT STRUTS, MED CLOSING HANDLE AND PUSH ROD AS REQUIRED. OPS CHEC
- [SDR JGVR20240417001](https://openairdocs.org/sdr/JGVR20240417001.md): Skin · corroded · Apr 16, 2024 · N361QS · Cessna 680A · Wing, Plate/Skin
  > MECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED ON RH WING UPPER BONDED SKIN FWD END OF AFT DRAG ANGLE, AFT END OF MIDDLE DRAG ANGLE AND MID AREA OF MIDDLE DRAG ANGLE. FOUND 2 AREAS OF CORROSION BLENDS LOCATED AT AFT END OF MIDDLE DRAG ANGLE TO BE BEYOND LIM
- [SDR JGVR20240416002](https://openairdocs.org/sdr/JGVR20240416002.md): Skin · corroded · Apr 16, 2024 · N361QS · Cessna 680A · Emergency Exits
  > MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED ON E-EXIT DOOR OUTER SKIN SURFACE. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED BLENDED AREAS AND FOUND CORROSION BLENDS TO BE WITHIN LIMITS IAW ENGINEERING FIELD REPAIR SR-680-ATA52-18636
- [SDR DXTA2023082493730](https://openairdocs.org/sdr/DXTA2023082493730.md): Bellcrank · defective · Aug 23, 2023 · N361QS · Cessna 680CE · Passenger/Crew Doors
  > REPEAT WRITE UP, MAIN CABIN DOOR PRE CATCH RELEASE LEVER WILL NOT STOW. REMAINS IN A 90 DEGREE POSITION WITH THE MAIN HANDLE IN THE LOCKED POSITION. WITH THE HANDLE IN THE OPEN POSITION, PRE CATCH MOVES TO A 70 DEGREE POSITION. FOUND DOOR PRE CATCH LATCH HANDL
- [SDR 2023F00228](https://openairdocs.org/sdr/2023F00228.md): Unknown · unknown · Jul 16, 2023 · N361QS · Cessna 680CE · Vertical Stabilizer
  > MINOR CORROSION FOUND ON LH VERTICAL STAB REAR SPAR CAP. ACCOMPLISHED VERTICAL STAB AFT SPAR CORROSION REPAIR IAW TEXTRON AVIATION REPAIR LETTER DQ40368.
- [SDR 2023F00227](https://openairdocs.org/sdr/2023F00227.md): Spar Cap · corroded · Jul 16, 2023 · N361QS · Cessna 680CE · Wing Spar
  > MINOR CORROSION FOUND ON RH WING AFT SPAR CAP IN THE WHEEL WELL AREA. ACCOMPLISHED RH WING AFT SPAR CORROSION REPAIR IAW TEXTRON AVIATION REPAIR LETTER DQ40332M1DATED JULY 12,2023.
- [SDR DXTA2022102172510](https://openairdocs.org/sdr/DXTA2022102172510.md): Socket · damaged · Oct 20, 2022 · N361QS · Gulstm 680 · Light System Wiring
  > CABIN EMERG LIGHT: C. BETWEEN SEAT 8 AND 10. WHILE PERFORMING BATTERY EXERCISE PROCEDURE AND PERFORMING OTHER MX ON AIRCRAFT, NOTED EMER LIGHTS CONNECTED TO #3 BATTERY WENT OUT. CHECKED FUSE ON PACK #3, NEW FUSE FOUND BLOWN.REMOVED RH FWD EXTERIOR EMER LIGHT
- [SDR DXTA2022091970560](https://openairdocs.org/sdr/DXTA2022091970560.md): Door Seal · defective · Sep 16, 2022 · N361QS · Cessna 120 · Emergency Exits
  > EMERG EXIT DOOR SEAL: DURING FLIGHT AT 23,000FT PAX NOTIFIED US THAT THERE WAS A LOUD NOISE COMING FROM THE LAV. I WENT BACK TO LAV AND THERE WAS A LOUD HIGH PITCH NOISE COMING FROM THE UPPER RIGHT PORTION OF THE EMERGENCY EXIT DOOR WHEN FACING THE IT. WHEN I
- [SDR DXTA2022091270070](https://openairdocs.org/sdr/DXTA2022091270070.md): None · none · Sep 9, 2022 · N361QS · Cessna 120 · Passenger/Crew Doors
  > MAIN DOOR PRECATCH LEVER: MAIN CABIN DOOR PRECATCH WILL NOT RETRACT. MOVES WITH DOOR OPENING BUT SEEMS LIKE IT SKPPED A NOTCH ON THE GEAR. DOOR SECURES CORRECTLY PRECATCH STICKS STRAIGHT OUT. MEL DOES NOT APPLY AS CANT SECURE PRECATCH. // SIGNOFF // CONFIRMED
- [SDR DXTA2022082268660](https://openairdocs.org/sdr/DXTA2022082268660.md): Acm · inoperative · Aug 21, 2022 · N361QS · Cessna 120 · Air Distribution System
  > ACM O'TEMP AMBER CAS: ACM O'TEMP MSG ILLUMINATED AT 45,000'. CHECKLIST ACCOMPLISHED.
- [SDR DXTA2022060863540](https://openairdocs.org/sdr/DXTA2022060863540.md): Battery Pack · defective · Jun 8, 2022 · N361QS · Cessna 680CE · Emergency Lighting
  > CABIN EMERG LIGHT: MULTIPLE EMERGENCY LIGHTS IN BACK HALF OF CABIN DO NOT ILLUMINATE. // SIGNOFF// REMOVED AND REPLACED #4 EMERGENCY BATTERY DUE TO AFT LIGHT NOT ILLUMINATING OPS CHECKS GOOD CHARGED BATTERY, ALL WORK DONE I.AW. CE-680 AMM CH 33-50-00. REMOVED
- [SDR DXTA2022022857460](https://openairdocs.org/sdr/DXTA2022022857460.md): Lamp · defective · Feb 28, 2022 · N361QS · Cessna 680CE · Emergency Lighting
  > WITH BATTERIES OFF, EXTERIOR SHARK LIGHT WILL NOT ILLUMINATE WITH THE EMER LTS SWITCH IN EITHER THE ON OR ARM POSITION.//CORRECTIVE ACTION// REMOVED AND INSTALLED NEW LAMP PN 1495X
- [SDR DXTA2022020956420](https://openairdocs.org/sdr/DXTA2022020956420.md): Battery · defective · Feb 8, 2022 · N361QS · Cessna 680CE · Emergency Lighting
  > UNABLE TO ACTIVATED THE CABIN EMERGENCY LIGHTS WITH THE EMERGENCY LIGHT SWITCH SELECTED IN THE ON POSITION AND BATTERIES OFF. WITH THE EMERGENCY SWITCH POSITIONED TO ARM WE ONLY GET THE EXIT SIGN OVER THE CABIN DOOR THE EXIT SIGNS LEFT AND RIGHT OF MAIN CABIN
- [SDR 2020F00422](https://openairdocs.org/sdr/2020F00422.md): Skin · damaged · Oct 5, 2020 · N361QS · Cessna 680CE · Wing, Plate/Skin
  > RIGHT WING INBOARD LEADING EDGE PANELS DAMAGED (OVERSIZED ATTACH FASTENER HOLES). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ27059M1 DATED SEPT. 18, 2020; 680-0235 (N361QS). RIGHT WING INBOARD LEADING EDGE PANELS DAMAGED (OVERSIZED ATTACH FASTENER HO
- [SDR 2020F00418](https://openairdocs.org/sdr/2020F00418.md): Doubler · gouged · Sep 30, 2020 · N361QS · Cessna 680A · Emergency Exits
  > SCREW GOUGES, AFT CABIN, ESCAPE HATCH INTERIOR SURROUND, FS 400-FS 430. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0235-8382 REV-, DATED SEP 17, 2020 AND FAA FORM 8100-9 DATED 9/18/2020. FIELD REPAIR-SCREW GOUGES, AFT CABIN, ESCAPE HATCH INTERIOR SUR
- [SDR 2020F00417](https://openairdocs.org/sdr/2020F00417.md): Stringer · corroded · Sep 30, 2020 · N361QS · Cessna 680A · Fuselage Main, Longeron/Stringer
  > CORROSION, FUSELAGE, DROP AISLE, FS 164 TO FS 209. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0235-8359 REV-, DATED SEP 9, 2020 AND FAA FORM 8100-9 DATED 9/11/2020. FIELD REPAIR-CORROSION, FUSELAGE, DROP AISLE, FS 164 TO FS 209.
- [SDR 2020F00398](https://openairdocs.org/sdr/2020F00398.md): Frame · cracked · Sep 15, 2020 · N361QS · Cessna 680A · Fuselage Main, Structure
  > NLG MID FRAME CRACK. ACCOMPLISHED NETJETS RFTS-104151 REV 0 DATED 03SEP20; N361QS (S/N 680-0235) NLG MID FRAME CRACK PERMANENT REPAIR.
- [SDR DXTA2020031703590](https://openairdocs.org/sdr/DXTA2020031703590.md): Cooling Fan · contaminated · Mar 16, 2020 · N361QS · Cessna 680CE · Air Distribution Fan
  > APU START - INFLIGHT APU START AT 1500 FEET PRIOR TO LANDING. FMS 1 WENT BLANK DURING APU START. SMELLED SOMETHING AFTER FMS 1 WAS BACK ONLINE. WE SHUT DOWN THE APU. //SIGNOFF// WE GAINED ACCESS TO THE BACK SIDE OF APU CONTROL PANEL AND COPILOTS CIRCUIT BREAKE
- [SDR JGVR20200214002](https://openairdocs.org/sdr/JGVR20200214002.md): Spar · corroded · Feb 14, 2020 · N361QS · Cessna 680CE · Wing Spar
  > CORROSION ALONG FWD SIDE OF THE LH WING AFT SPAR, LOWER CLIP AS VISIBLE FROM INSIDE THE GEAR WELL
- [SDR JGVR20200214001](https://openairdocs.org/sdr/JGVR20200214001.md): Spar · corroded · Feb 14, 2020 · N361QS · Cessna 680CE · Wing Spar
  > CORROSION ALONG FWD SIDE OF THE RH WING AFT SPAR, LOWER CLIP AS VISIBLE FROM INSIDE THE GEAR WELL.
- [SDR JGVR20190919003](https://openairdocs.org/sdr/JGVR20190919003.md): Skin · corroded · Sep 19, 2019 · N361QS · Cessna 680CE · Wing, Plate/Skin
  > REPAIRED CORRODED AREAS OF THE LT & RT WINGS UPPER SKINS LOCATED UNDER AND ADJACENT TO THE LT FORWARD, MIDDLE, AND AFT, AND RT FORWARD AND AFT FUSELAGE/WING DRAG ANGLES (WING/FUSELAGE FAIRING) BY R&R THE DRAG ANGLES FOR ACCESS, BLENDING, PERFORMING NDT, TREATI
- [SDR JGVR20190919002](https://openairdocs.org/sdr/JGVR20190919002.md): Skin · corroded · Sep 19, 2019 · N361QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED CORRODED AREAS OF THE LT AND RT FORWARD FUSELAGE SKINS, LOCATED UNDER AND ADJACENT TO THE FORWARD CHIN FAIRINGS, BY R&R THE FORWARD CHIN FAIRINGS FOR ACCESS, BLENDING, PERFORMING NDT, FABRICATING AND INSTALLING DOUBLERS AND FILLERS AS REQUIRED IN ACCO
- [SDR JGVR20190917001](https://openairdocs.org/sdr/JGVR20190917001.md): Skin · corroded · Sep 17, 2019 · N361QS · Cessna 680CE · Aerodynamic Fairings
  > REPAIRED CORRODED AREAS OF THE TAILCONE SKINS LOCATED UNDER THE AFT CHIN FAIRINGS BY R&R CHIN FAIRING FOR ACCESS, BLENDING, PERFORMING NDT AND INSTALLING REPAIR DOUBLERS PER REPAIR DRAWING.
- [SDR 2019F00062](https://openairdocs.org/sdr/2019F00062.md): Cowling · eroded · Aug 23, 2018 · N361QS · Cessna 680SOV · Nacelle/Pylon, Main Frame
  > LEFT ENGINE LOWER COWLING DAMAGE (EROSION) ENGINEERING LETTER # DQ14437M1
- [SDR 2017FA0000072](https://openairdocs.org/sdr/2017FA0000072.md): Spar · corroded · Feb 19, 2017 · N361QS · Cessna 680CE · Wing Spar
  > LT WING SPAR CORRODED.
- [SDR 2016F00210](https://openairdocs.org/sdr/2016F00210.md): Skin · corroded · Oct 17, 2016 · N361QS · Cessna 680SOV · Passenger/Crew Doors
  > CORROSION ON LOWER CABIN DOOR SKIN.
- [SDR 2016FA0000477](https://openairdocs.org/sdr/2016FA0000477.md): Skin · gouged · Oct 9, 2016 · N361QS · Cessna 680SOV · APU Cowling/Containment
  > APU BAY RIGHT INSIDE SKIN GOUGED. REPAIRED IAW EO DQ5840M1.
- [SDR 2016FA0000476](https://openairdocs.org/sdr/2016FA0000476.md): Skin · corroded · Oct 9, 2016 · N361QS · Cessna 680SOV · Passenger/Crew Doors
  > CORROSION ON LOWER CABIN DOOR SKIN.
- [SDR DXTA2014072105824](https://openairdocs.org/sdr/DXTA2014072105824.md): Brake Assy · worn · Jul 20, 2014 · N361QS · Cessna 680CE · Landing Gear Brake System
  > DURING LANDING, BRAKES GRAB & GRIND WITH LOUD METAL TO METAL NOISE. VERY PRONOUNCED EVEN WHEN PARKING. BRAKE WEAR PINS ON LT MAIN INBD HAS MINIMAL INDICATION. FOUND NR 1 & 2 BRAKES GRABBING & MAKING NOISE. R & R NR 1 & 2 BRAKE ASSEMBLIES. BLED SYS, OPS &
- [SDR DXTA2014060605795](https://openairdocs.org/sdr/DXTA2014060605795.md): Seal · torn · Jun 5, 2014 · N361QS · Cessna 680CE · Landing Gear Brake System
  > WHEN STOPPING THE ACFT ON THE RAMP THE RT BRAKE GROWLS & AS THE ACFT STOPS THE BRAKE GRABS. REMOVED NR 3 & NR 4 MAIN WHEEL ASSEMBLIES IAW AMM 32-41-20. FOUND NR 3 INNER GREASE SEAL DAMAGED, RUBBER HAS A TEAR. VISUALLY INSPECTED NR 3 & NR 4 BRAKE ASSEMBLIES
- [SDR CWQR20130305017](https://openairdocs.org/sdr/CWQR20130305017.md): Heat Exchanger · cracked · Mar 5, 2013 · N361QS · Cessna 680CE · Pneumatic Distribution System
  > HEAT EXCHANGER SIDE PLATE HAD TWO CRACKS ABOUT.35 INCH LONG. THE OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN TWO OF THE FOUR CORNERS. A NEW HEAT EXCHANGER WAS INSTALLED. PREFORMED A LEAK CHECK ON THE DEFECTIVE UNIT AND FOUND THE CRACKS EXTENDED INTO
- [SDR CWQR20130305016](https://openairdocs.org/sdr/CWQR20130305016.md): Heat Exchanger · cracked · Mar 5, 2013 · N361QS · Cessna 680CE · Pneumatic Distribution System
  > HEAT EXCHANGER SIDE PLATE HAD FOUR CRACKS ABOUT.35 INCH LONG. THE OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN FOUR OF THE FOUR CORNERS. A NEW HEAT EXCHANGER WAS INSTALLED. PREFORMED A LEAK CHECK ON THE DEFECTIVE UNIT AND FOUND THE CRACKS EXTENDED INTO
- [SDR DXTA2010012903961](https://openairdocs.org/sdr/DXTA2010012903961.md): Steering Unit · malfunctioned · Jan 28, 2010 · N361QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > AFTER LIFING UP LANDING GEAR HANDLE DURING TAKEOFF, RED GEAR UNLOCK LIGHT ILLUMINATED STEADY WITH A NOSE GEAR DOWN LIGHT INDICATION. LATER EXTENDED LANDING GEAR HANDLE WITH NORMAL GEAR EXTENDED INDICATION. REPLACED NLG STEERING UNIT IAW MM 32-50-00.
- [SDR DXTA2009062403697](https://openairdocs.org/sdr/DXTA2009062403697.md): Schrader Valve · malfunctioned · Jun 23, 2009 · N361QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > NOSE WHEEL WOULD NOT RETRACT AFTER TAKEOFF. RESERVICED NOSE STRUT AFTER CHANGING SCHRADER VALVE. OP/LEAK CHECKS GOOD.
- [SDR DXTA2009012903478](https://openairdocs.org/sdr/DXTA2009012903478.md): Strut · discharged · Jan 29, 2009 · N361QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > FOUND NOSE STRUT LWR NITROGEN SERVICE AT 0 PSI. SERVICED NOSE STRUT WITH 5606 HYD FLUID AND NITROGEN. JACKED ACFT AND PERFORMED LANDING GEAR OPS CHECK. OPS AND LEAK CHECK GOOD. DOWNJACKED ACFT. WORK PERFORMED REF MM 32-20-00 AND 32-00-00.
- [SDR DXTA2009013003478](https://openairdocs.org/sdr/DXTA2009013003478.md): Landing Gear · unknown · Jan 29, 2009 · N361QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > NOSE GEAR DID NOT RETRACT ON TAKE-OFF.
- [SDR DXTA200803133](https://openairdocs.org/sdr/DXTA200803133.md): Control Valve · out of adjust · Jun 18, 2008 · N361QS · Cessna 560CESSNA · Brake Anti-Skid Section
  > BRAKES VERY INEFFECTIVE ON LANDING ROLL-OUT. REPLACED ANTI-SKID POWER CONTROL VALVE IAW MM 32-42-05 OP'S CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N361QS/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 = 'N361QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N361QS/reports

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