# Service difficulty reports: N382QS, cancelled Dec 6, 2024

A list on [N382QS, cancelled Dec 6, 2024](https://openairdocs.org/deregistered/N382QS-2024-12-06.md).

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

- [SDR DXTA2024090900440](https://openairdocs.org/sdr/DXTA2024090900440.md): Connector · damaged · Sep 4, 2024 · N382QS · Cessna 680SOV · Light System Wiring
  > EMERGENCY LIGHTING: MAIN EXIT DOOR EXIT SIGNS NOT ILLUMINATING ALING WITH THE GALLEY WORK LIGHT ALL THE REST OF THE EMERGENCY LIGHTS WORK PROPERLY. CORRECTIVE ACTION: RESEATED PUSHED PIN S AT CANNON PLUG PC045. RESEATED PIN, RECONNECTED CANNON PLUG, OPS CHECK
- [SDR DXTA2024071212336](https://openairdocs.org/sdr/DXTA2024071212336.md): Battery · defective · Jul 11, 2024 · N382QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK #4 REMAIN ILLUMINATED WHEN ALL POWER IS REMOVED FROM THE AIRCRAFT. THE EMER LIGHTS WERE NO LONGER ON. WITH THE MAIN BATTERIES DISCONNECTED, CYCLED ERNER LIGHT SWITCH OFF TO ARM TO ON NOTING THAT ALL EMER LIGH
- [SDR 2023F00306](https://openairdocs.org/sdr/2023F00306.md): Web · cracked · Oct 17, 2023 · N382QS · Cessna 680CE · Wing Miscellaneous Structure
  > LH WING FWD WEB P/NP/N 6910269-39. CRACKED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR OF THE LH WING FWD WEB CRACK SR-680A-ATA57-33170 DATED APRIL 25, 2022 AND 8100-9 DATED APRIL 25, 2022; STANDARD REPAIR - CRACK DAMAGE, CENTER WING FAIRINGS, LH AND RH
- [SDR 2023F00287](https://openairdocs.org/sdr/2023F00287.md): Spar Cap · corroded · Sep 25, 2023 · N382QS · Cessna 680CE · Wing Spar
  > RH LOWER REAR SPAR CAP CORRODED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ41229M1 DATED SEPTEMBER 21, 2023; RH LOWER REAR SPAR CAP CORROSION.
- [SDR 2023F00286](https://openairdocs.org/sdr/2023F00286.md): Unknown · unknown · Sep 25, 2023 · N382QS · Cessna 680CE · Wing Spar
  > LH LOWER REAR SPAR CAP CORRODED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ41230M1 DATED SEPTEMBER 21, 2023; LH LOWER REAR SPAR CAP CORROSION.
- [SDR DXTA2023072491650](https://openairdocs.org/sdr/DXTA2023072491650.md): Condenser · dirty · Jul 23, 2023 · N382QS · Cessna 680CE · Pneumatic Distribution System
  > PNEUMATIC DISTRIBUTION: DURING A LONGER FLIGHT, ONCE THE CABIN BECOMES COLD SOAKED, AND THE SUPPLY DUCT TEMPERATURE WARMS UP WE NOTICED A SLIGHT OIL BURNING ODOR COMING FROM THE VENTS. I CHECKED THE VENT SUPPLY TEMPERATURE AND IT WAS ONLY SHOWING ABOUT 140. //
- [SDR DXTA2023060888160](https://openairdocs.org/sdr/DXTA2023060888160.md): Flag · damaged · Jun 7, 2023 · N382QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN CABIN DOOR EXTERIOR FLAG INDICATOR, REMAINS RED WITH THE DOOR HANDLE IN THE STOW DOWN POSITION. NORMAL INDICATION WOULD BE BLACK AND WHITE CROSS MARKS. VERIFIED INDICATOR FAILS IN CLOSED POSITION. REMOVED PAX DOOR SHROUD & ACCESS PANELS & LOCATED THE INT
- [SDR EBVR202305180001](https://openairdocs.org/sdr/EBVR202305180001.md): Unknown · unknown · May 18, 2023 · N382QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > CORROSION FOUND ON VERTICAL STAB SPAR LH CAP ANGLE BETWEEN VFS 180-184. REPAIRED USING TEXTRON FIELD REPAIR FR-680-0245-11912 AND 8100-9 DATED 17MAY2023. THIS IS A MAJOR REPAIR.
- [SDR DXTA2022120775710](https://openairdocs.org/sdr/DXTA2022120775710.md): Counterbalance · out of adjust · Dec 6, 2022 · N382QS · Cessna 680CE · Passenger/Crew Doors
  > DOOR SEEMS TO BE OUT OF RIG. THE BOTTOM STEP APPEARS TO BE 3 TO 4 INCHES HIGHER THAN NORMAL. ALSO THE COUNTERBALANCE IS NOT WORKING WHEN THE DOOR IS CLOSED. IT WILL SLAM SHUT WITH A LOT OF FORCE. ADJUSTED DOOR COUNTER BALANCE SYSTEM IAW AMM 52-10-50. NO OT
- [SDR DXTA2022070565260](https://openairdocs.org/sdr/DXTA2022070565260.md): Battery · inoperative · Jul 3, 2022 · N382QS · Cessna 680A · Emergency Lighting
  > CABIN EMERG LIGHT: DURING POWER ON CHECKLIST ALL EMERERGENCY LIGHTS INOP. WITH BATTERY ON EMERGENCY LIGHTS OPERATIONAL. "CORRECTIVE ACTION" COMPLIED WITH CE-680 EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. NO DEFECTS NOTED IAW TC-FLT-33-1001 REV
- [SDR DXTA2022010354690](https://openairdocs.org/sdr/DXTA2022010354690.md): Not Reported · not reported · Jan 1, 2022 · N382QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHT SWITCH: WHEN YOU TURN THE EMER LIGHTS SWITCH OFF THE FOLLOWING LIGHTS REMAIN ON: AFT OVER WING EMERGENCY LIGHT. EXIT LIGHT IN THE DIVIDER, OVERHEAD LIGHT FORWARD OF THAT EXIT LIGHT, EXIT LIGHT IN LAV, AND OVERHEAD LIGHT ABOVE THE LAV. // SIGNO
- [SDR DXTA2021060743320](https://openairdocs.org/sdr/DXTA2021060743320.md): Structure · bent · Jun 6, 2021 · N382QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR CORNER BENT OUT APPROXIMATELY 3/4 INCH(JUST TO THE RIGHT OF THE HANDLE). // SIGNOFF // MAIN ENTRANCE DOOR LOWER HALF AFT MID SECTION OF DOOR SKIN EXTENTION.LOC: FS 220 AND WS 105.71. AREA OF TWO INCHES X TWO INCHES. PART OF THE LOWER
- [SDR JGVR20210526003](https://openairdocs.org/sdr/JGVR20210526003.md): Spar Cap · corroded · May 26, 2021 · N382QS · Cessna 680A · Wing Spar
  > MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON AFT SPAR, LOWER SPAR CAP AT WS 37.00. FOUND INBD BLEND TO BE WITHIN LIMITS. PER NJA GMM 2.2.2 THIS IS LEVEL 1 CORROSION. FOUND 1 AREA AT WS 37.00 TO BE BEYOND LIMITS IAW C680 SRM 51-70-02. PROTECTED BARE M
- [SDR JGVR20210526002](https://openairdocs.org/sdr/JGVR20210526002.md): Rib · corroded · May 26, 2021 · N382QS · Cessna 680A · Wing, Rib/Bulkhead
  > MECHANICALLY REMOVED AREA OF CORROSION LOCATED IN RH WING GEARWELL BAY 720DR OUTBD RIB LOWER MIDDLE AREA IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM LIMITATIONS. REPAIRED CORROSION BLEND IAW TEXTRON ENGINEERING MEMO REF DQ30071M1 RRL, S
- [SDR JGVR20210526001](https://openairdocs.org/sdr/JGVR20210526001.md): Rib · corroded · May 26, 2021 · N382QS · Cessna 680A · Wing, Rib/Bulkhead
  > MECHANICALLY REMOVED AREA OF CORROSION LOCATED IN LH WING GEARWELL BAY 730DL OUTBD RIB LOWER MIDDLE AROUND HI-LOK IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM LIMITATIONS. REPAIRED CORROSION BLEND IAW TEXTRON ENGINEERING MEMO REF DQ30071M
- [SDR DXTA2021041240650](https://openairdocs.org/sdr/DXTA2021041240650.md): Sensor · defective · Apr 10, 2021 · N382QS · Gulstm 680 · Fire Detection
  > ENG FIRE DETECT FAIL R AMBER CAS: IN CRUISE FLIGHT AT FL380 AMBER 'ENG FIRE DETECT FAIL R' CAS MESSAGE DISPLAYED. REMOVED INTERNAL FIRE & OVERHEAT SENSOR, PN:- 30B5702-01; SN: 121604. FROM RH ENGINE; DUE TO ENG FIRE DETECT FAIL R AMBER CAS MESSAGE DISPLAYED.
- [SDR JGVR20210219003](https://openairdocs.org/sdr/JGVR20210219003.md): Door Frame · corroded · Feb 19, 2021 · N382QS · Cessna 680A · Fuselage Main, Structure
  > REMOVED THE FWD AND AFT CONTOUR RINGS FROM THE EMERGENCY EXIT DOOR AND FOUND SEVERE AREAS OF CORROSION ON THE DOOR STRUCTURE. SENT THE EMERGENCY EXIT DOOR OUT FOR REPAIR.
- [SDR JGVR20210219002](https://openairdocs.org/sdr/JGVR20210219002.md): Structure · corroded · Feb 19, 2021 · N382QS · Cessna 680CE · Passenger/Crew Doors
  > MECHANICALLY BLENDED AREAS OF BUBBLING PAINT AND CORROSION FROM MAIN CABIN DOOR STRUCTURE, LOCATED UNDER MOVABLE STEP BETWEEN THE TWO CENTER ATTACH POINTS, PERFORMED NDT AN REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS IAW TEXTRO
- [SDR JGVR20210219001](https://openairdocs.org/sdr/JGVR20210219001.md): Floor Support · corroded · Feb 19, 2021 · N382QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > MECHANICALLY BLENDED SEVEN AREAS OF CORROSION IN CABIN DROP AISLE FLOOR CONSISTING OF TWO AREAS ON LT FWD ANGLE APPROXIMATELY 3.5 AND 8 INCHES AFT OF FWD END OF DROP AISLE, RAISED DOUBLER/FLOOR BOARD SUPPORT WITH TWO AREAS ON THE FWD LT SIDE AND THREE ON FWD R
- [SDR JGVR20200605001](https://openairdocs.org/sdr/JGVR20200605001.md): Rib · corroded · Jun 5, 2020 · N382QS · Cessna 680A · Wing, Rib/Bulkhead
  > CORROSION AROUND 2 HI-LOKS ON UPPER OUTBOARD RIB ABOVE LT MLG AT APPROXIMATELY MIDLINE. REMOVED 2 HI-LOK FASTENERS AND MECHANICALLY BLENDED CORROSION IN AREA AROUND HOLES ON UPPER OUTBOARD RIB ABOVE LT MLG AT APPROXIMATELY MIDLINE, IAW SRM 51-10-01. PERFORMED
- [SDR 2TJR201910210001](https://openairdocs.org/sdr/2TJR201910210001.md): Spar Cap · corroded · Oct 21, 2019 · N382QS · Cessna 680SOV · Vertical Stabilizer, Spar/Rib
  > CORROSION WAS FOUND AT THREE LOCATIONS ON THE 6931012-1 LH AFT SPAR CAP OF THE VERTICAL STABILIZER. ALL CORROSION WAS REMOVED BY BLENDING IAW CESSNA FIELD REPAIR - CORROSION, VERTICAL STABILIZER, LH REAR SPAR CAP, VFS 115 TO 163 DWG NO. FR-680-0245-7226 DATE
- [SDR DXTA2018052100157](https://openairdocs.org/sdr/DXTA2018052100157.md): Skin · corroded · May 21, 2018 · N382QS · Cessna 680CE · Aerodynamic Fairings
  > TAILCONE SKIN CORRODED.
- [SDR DXTA2018FA0000156](https://openairdocs.org/sdr/DXTA2018FA0000156.md): Drag Angle · cracked · May 21, 2018 · N382QS · Cessna 680CE · Wing Miscellaneous Structure
  > RT WING DRAG ANGLE CRACKED.
- [SDR DXTA2016020206175](https://openairdocs.org/sdr/DXTA2016020206175.md): Switch · faulty · Feb 1, 2016 · N382QS · Cessna 680CE · Landing Gear Position and Warning
  > LEFT MAIN GEAR STAYED DOWN AFTER GEAR RETRACTION WITH A LT GEAR DOWN GREEN INDICATION & NO RED INDICATION. OHMED OUT LT GEAR UPLOCK SWITCH SG007 & FOUND WITH THE GEAR DOWN. THE SWITCH IS LIGHTLY TAPPED BETWEEN PINS E & F, RESISTANCE GOES FROM.2 OHMS UP TO 3
- [SDR DXTA2015101206106](https://openairdocs.org/sdr/DXTA2015101206106.md): Brake Assy · locked · Oct 6, 2015 · N382QS · Cessna 680CE · Landing Gear Brake System
  > EMERGENCY BRAKING WAS USED & RT OTBD TIRE APPEARS TO HAVE LOCKED UP & BLOWN. REMOVED FAULTY RT NR 3 & 4 WHEEL & TIRE ASSEMBLY. INSTALLED OVERHAULED NR 3 & 4 WHEEL & TIRE ASSEMBLY IAW MM 32-41-20. SERVICED RT NR 3 & 4 MAIN TIRES WITH NITROGEN IAW MM CH 12-13
- [SDR DXTA2015100606103](https://openairdocs.org/sdr/DXTA2015100606103.md): Hydraulic Line · faulty · Oct 6, 2015 · N382QS · Cessna 680CE · Hydraulic System, Main
  > IMMEDIATELY AFTER GEAR EXTENSION & 3 GREEN GEAR DOWN & LOCK LIGHTS, RECEIVED AMBER HYD VOLUME LOW CAS MSG. EMER BRAKING WAS USED & RT OTBD TIRE APPEARS TO HAVE LOCKED UP & BLOWN. REMOVED FAULTY NLG ACTUATOR EXTENSION HOSE AND INSTALLED NEW EXTENSION HOSE IAW
- [SDR CWQR20130305013](https://openairdocs.org/sdr/CWQR20130305013.md): Heat Exchanger · cracked · Mar 5, 2013 · N382QS · 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. THE OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN 2 OF THE 4 CORNERS.
- [SDR CWQR20130305014](https://openairdocs.org/sdr/CWQR20130305014.md): Heat Exchanger · cracked · Mar 5, 2013 · N382QS · Cessna 680CE · Pneumatic Distribution System
  > HEAT EXCHANGER SIDE PLATE HAD TWO CRACKS ABOUT.37 INCH LONG. THE OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN THREE OF THE FOUR CORNERS. A NEW HEAT EXCHANGER WAS INSTALLED. PREFORMED A LEAK CHECK ON THE DEFECTIVE UNIT AND FOUND THE CRACKS EXTENDED IN
- [SDR CWQR20121221054](https://openairdocs.org/sdr/CWQR20121221054.md): Tube · cracked · Dec 21, 2012 · N382QS · Cessna 680CE · Engine Bleed Air System
  > ACFT CAME IN WITH A REPORTED TREND SHIFT IN ITT. DURING AN ENGINE RUN, FOUND A BLEED AIR LEAK ON THE TOP SIDE OF THE RT ENGINE. REMOVED CLAMP AND FOUND THE TUBE MATING FLANGE CRACKED.
- [SDR DXTA2012092405133](https://openairdocs.org/sdr/DXTA2012092405133.md): Door Frame · corroded · Sep 24, 2012 · N382QS · Cessna 680CE · Fuselage Main, Structure
  > MINOR CORROSION FOUND ADJACENT TO AFT SHEAR TIE ON CABIN DOOR FRAME..023 DEEP, OUT OF LIMITS, DOOR FRAME WILL BE CHANGED.
- [SDR DXTA2011092004733](https://openairdocs.org/sdr/DXTA2011092004733.md): Brake · leaking · Sep 19, 2011 · N382QS · Cessna 680CE · Landing Gear Brake System
  > MAIN WHEEL LEAKING HYD FLUID. BRAKES VERY RIGID ON BOTH RUDDER PEDALS WHEN BRAKES APPLIED ON TAXI/TAKEOFF/LANDING ROLLOUT. BOTH PILOT BRAKE APPLICATIONS REQUIRED MORE BRAKE APPLICATION THEN NORMAL TO STOP. R & R THE LT OTBD WHEEL & BRAKE ASSY AND INSTALLED
- [SDR DXTA2010092804253](https://openairdocs.org/sdr/DXTA2010092804253.md): Landing Gear · malfunctioned · Sep 27, 2010 · N382QS · Cessna 680CE · Nose/Tail Landing Gear
  > RED MLG UNLOCK INDICATION REMAIND ILLUMINATED AFTER MLG HANDLE WAS PLACED IN THE UP POSITION. 3 GREEN MLG INDICATORS EXTINGUISHED. MLG DEPLOYED NORMALLY. JACKED ACFT AND DUPLICATED PROBLEM AFTER 3 GEAR SWINGS. REPOSITIONED HYD SYS & FOUND NOSE GEAR ABOUT TO
- [SDR DXTA2010032304049](https://openairdocs.org/sdr/DXTA2010032304049.md): Strut · malfunctioned · Mar 22, 2010 · N382QS · Cessna 680CE · Main Landing Gear Strut/Axle/Truck
  > ON DEPARTURE, LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION, LANDING GEAR REMAINED DOWN AND LOCKED. APPROX 1-2 MINS LATER THE "WOW MISCOMPARE" CAS MSG ILLUMINATED FOR 30 SECONDS THEN EXTINGUISHED. REMOVED LOWER STRUT, CLEANED AND REPACKED WITH NEW
- [SDR DXTA2009111003856](https://openairdocs.org/sdr/DXTA2009111003856.md): Landing Gear · malfunctioned · Nov 9, 2009 · N382QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > WHILE ENROUTE AT FL400, APPROX 25 MINUTES INTO FLIGHT, NOSE GEAR EXTENDED UNCOMMANDED, NOSE DOORS OPENED, THEN NOSE GEAR RETRACTED VERY ABRUPTLY. INDICATIONS ON GEAR DISPLAY WERE ONE RED, NO GREEN. RED LIGHT STAYED ON TILL GEAR HANDLE WAS SELECTED DOWN FOR L
- [SDR DXTA2009111003852](https://openairdocs.org/sdr/DXTA2009111003852.md): Landing Gear · malfunctioned · Nov 9, 2009 · N382QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > WHILE EN ROUTE AT FL400, APPROX 25 MINUTES INTO FLIGHT, NOSE GEAR EXTENDED UNCOMMANDED, NOSE DOORS OPENED, THEN NOSE GEAR RETRACTED VERY ABRUPTLY. INDICATIONS ON GEAR DISPLAY WERE ONE RED, NO GREEN. RED LIGHT STAYED ON TILL GEAR HANDLE WAS SELECTED DOWN FOR LA
- [SDR DXTA2008122703444](https://openairdocs.org/sdr/DXTA2008122703444.md): Switch · shorted · Dec 27, 2008 · N382QS · Cessna 680CE · Air Conditioning System
  > AT APPROX 13,000 FT ON APPROACH, GOT AN "AMC O' HEAT" TEMP CAS MESSAGE FOLLOWED BY AN EMER PRESS ACTIVATION. SHORTLY AFTER EMER PRESS CAME ON CABIN STARTED TO AQUIRE SMOKE. IT GOT TO A "HAZY CLOUD" THICKNESS AND THEN STABILIZED. SMOKE SMELL ASSOCIATED. VERI
- [SDR DXTA2008122903444](https://openairdocs.org/sdr/DXTA2008122903444.md): Unknown · smoke · Dec 27, 2008 · N382QS · Cessna 680CE · Air Distribution System
  > SMOKE IN COCKIT DURING APPROACH
- [SDR DXTA20082935](https://openairdocs.org/sdr/DXTA20082935.md): Uplock Sensor · malfunctioned · Mar 12, 2008 · N382QS · Cessna 560CESSNA · Landing Gear Position and Warning
  > UPON GEAR RETRACTION, OUT OF DEPARTURE, RT GEAR WOULD NOT RETRACT. REMOVED AND REPLACED RT UPLOCK SWITCH WITH NEW. C/W FULL GEAR FUNCTIONAL CHECK. ALL OPS CHECK GOOD AT THIS TIME. IAW MM 32-61-00.
- [SDR DXTA20082880](https://openairdocs.org/sdr/DXTA20082880.md): Landing Gear · malfunctioned · Feb 17, 2008 · N382QS · Cessna 560CESSNA · Landing Gear Retraction/Extension System
  > MANUAL GEAR EXTENSION WITH BLOW DOWN DUE TO NOSE GEAR NOT EXTENDED DURING LANDING. RESET BLOWDOWN BOTTLE AND SERVICED SWING GEAR MULTIPLE TIMES. UNABLE TO DUPLICATE PROBLEM. REF: MM SEC 32-30-00

## 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 = 'N382QS' AND deregistration_id = 'N382QS-2024-12-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N382QS-2024-12-06/reports

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