# Service difficulty reports: N381QS, cancelled Dec 2, 2024

A list on [N381QS, cancelled Dec 2, 2024](https://openairdocs.org/deregistered/N381QS-2024-12-02.md).

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

- [SDR JGVR20240212001](https://openairdocs.org/sdr/JGVR20240212001.md): Spar · corroded · Feb 12, 2024 · N381QS · Cessna 680SOV · Vertical Stabilizer, Spar/Rib
  > FOUND 2 SPOTS OF CORROSION ON AFT VERTICAL SPAR. FOUND DURING TASK 55-30-00-2200 DURING CORROSION BLEND OUT, FOUND CORROSION TO BE GOING UNDER FASTENER HEAD ON VERTICAL STABILIZER AFT SPAR LH LOWER AREA. MECHANICALLY BLENDED 2 AREAS OF CORROSION ON AFT VERTICA
- [SDR 2023F00268](https://openairdocs.org/sdr/2023F00268.md): Rib · cracked · Sep 10, 2023 · N381QS · Cessna 680CE · Horizontal Stabilizer, Spar/Rib
  > LH ELEVATOR WEDGES PANEL INBOARD ATTACH RIB IS CRACK. ACCOMPLISHED LH HORIZONTAL STABILIZER INBOARD RIB DAMAGE REPAIR IAW TEXTRON AVIATION REPAIR MEMO DQ41081M1.
- [SDR DXTA2023082193590](https://openairdocs.org/sdr/DXTA2023082193590.md): Battery · inoperative · Aug 21, 2023 · N381QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTING: ALL THE EMERGENCY LIGHTS ASSOCIATED WITH NUMBER 4 BATTERY PACK ARE INOP. GAINED ACCESS TO AND REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTERY. CHARGED BATTERY AS CHECKS GOOD.CLOSED UP ALL. ACCESS. IAW CE680 MM 33-50-10
- [SDR DXTA2023061288450](https://openairdocs.org/sdr/DXTA2023061288450.md): Unknown · unknown · Jun 12, 2023 · N381QS · Cessna 680SOV · Cabin Pressure Control System
  > ONCE DESCENDING PRESSURIZATION WILL RAPIDLY SPIKE UP TO 1000FT/MIN THEN STABILIZE CAUSING DISCOMFORT FOR PASSENGERS. CONTINUING THE DESCENT PRESSURIZATION WILL SPORADICALLY INCREASE AND DECREASE BETWEEN 500FT/MIN.
- [SDR 3J7R2023052200001](https://openairdocs.org/sdr/3J7R2023052200001.md): Battery Pack · discharged · May 21, 2023 · N381QS · Cessna 680SOV · Emergency Lighting
  > FOUR LIGHTS OF THE EMERGENCY LIGHTING SYSTEM FAIL TO ILLUMINATE. THE LAV OVERHEAD LIGHT, THE TABLE OVERHEAD LIGHTS OF SEATS 5 AND 9, AND THE EMERGENCY EXIT FORWARD WING LIGHT.
- [SDR DXTA2023051886480](https://openairdocs.org/sdr/DXTA2023051886480.md): Rod · broken · May 17, 2023 · N381QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: WHILE CLOSING THE DOOR SOME MINOR BINDING WAS ENCOUNTERED. THE DOOR WOULD NOT EXTEND FREELY ON OPENING AND FORCE WAS REQUIRED TO OVERCOME THE BINDING. THE RIGHT BOTTOM STRUT SEGMENT DISPLAYS BENDING. REMOVED AND REPLACED MED AFT TELESCOPING ROD IA
- [SDR DXTA2022030958180](https://openairdocs.org/sdr/DXTA2022030958180.md): Light · disconnected · Mar 8, 2022 · N381QS · Cessna 680CE · Emergency Lighting
  > LAV EXIT SIGN/LIGHT: EMERGENCY EXIT SIGN ON BASE OF LAVATORY SEAT DOES NOT ILLUMINATE. //SIGNOFF/ FOUND EMERGENCY EXIT SIGN ON BASE OF LAVATORY SEAT TO BE DISCONNECTED, RECONNECTED AS REQUIRED AND OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR DXTA2022022156970](https://openairdocs.org/sdr/DXTA2022022156970.md): None · none · Feb 18, 2022 · N381QS · Cessna 680A · Air Conditioning System
  > CABIN ODOR: AT 41,000FT, APU OFF, ANY POWER SETTING, ODOR FROM BOTH BLEEDS. CREW EYES AND THROAT STINGING, HEADACHE. RH ENGINE REMOVED AND REPLACED. ENG CAL AND LEAK CHECKS GOOD NO DEFECTS NOTED.
- [SDR DXTA2021040840550](https://openairdocs.org/sdr/DXTA2021040840550.md): Sign · inoperative · Apr 7, 2021 · N381QS · Cessna 680CE · Emergency Lighting
  > MAIN EXIT SIGN/LIGHT: EMERGENCY LIGHT INOP. REMOVED FAILED SPLICE FROM AFT LH BULKHEAD EMERGENCY EXIT SIGN AND REPLACED WITH NEW UNIT. IAW CE-680 SPM 20-30-25. OPS CHECK GOOD. IAW CE-680 AMM 33-50-00.
- [SDR JGVR20200922001](https://openairdocs.org/sdr/JGVR20200922001.md): Drag Angle · corroded · Sep 22, 2020 · N381QS · Cessna 680A · Wing Main, Frame Structure
  > LEFT WING AFT DRAG ANGLE HAS 2 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 8 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. RIGHT UPPER WING AFT DRAG ANGLE HAS 1 AREA OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 7 AREAS OF VERIFIED C
- [SDR 2019FA0000235](https://openairdocs.org/sdr/2019FA0000235.md): Splice Strap · debonded · Jul 29, 2019 · N381QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > HORIZONTAL STABILIZER LEFT SIDE LOWER SKIN SPLICE STRAP DE-BONDED. ACCOMPLISHED ENGINEERING LETTER DQ22440M1 DATED JULY 25, 2019; 680-0097 HORIZONTAL STABILIZER LEFT SIDE LOWER SKIN SPLICE STRAP DE-BONDED.
- [SDR JGVR28180402001](https://openairdocs.org/sdr/JGVR28180402001.md): Torque Tube · cracked · Apr 2, 2018 · N381QS · Cessna 680CE · Rudder Structure
  > CRACKED RUDDER TORQUE TUBE FROM RUDDER. REPLACED THE RUDDER TORQUE TUBE IAW SRM 51-40-03, 51-40-06, 51-60-03, 55-40-09, AND MM 20-40-20.
- [SDR JGVR20170613002](https://openairdocs.org/sdr/JGVR20170613002.md): Skin · cracked · Jun 13, 2017 · N381QS · Cessna 680SOV · Rudder, Plate/Skin
  > CRACK ON LOWER RUDDER SKIN ON RT SIDE EXTENDING FROM BOTTOM OF RUDDER ONE INCH INTO A RIVET. REPAIRED THE RUDDER SKIN IAW ERO-897400, REV IR. PERFORMED EDDY CURRENT ON CUTOUT AREA. INSPECTION REVEALED NO CRACK INDICATIONS.
- [SDR DXTA2016092506308](https://openairdocs.org/sdr/DXTA2016092506308.md): Switch · out of adjust · Sep 25, 2016 · N381QS · Cessna 680CE · Door Warning System
  > AT 500' ON CLIMBOUT AMBER, NOSE DOOR OPEN RT, CAS ILLUMINATED. WHEN TURNING FINAL AND AT A SLOWER SPEED IT EXTINGUISHED. ADJUSTED BOTH RT DOOR SWITCHES AND OPS CHECKED GOOD IAW MM 52-40-00.
- [SDR DXTA2014111605928](https://openairdocs.org/sdr/DXTA2014111605928.md): Fire Loop · failed · Nov 16, 2014 · N381QS · Cessna 680CE · Fire Detection
  > RECEIVED AN ENGINE FIRE DETECTOR FAIL ON RT CAS. R & R RT ENG OUTER FIRE LOOP. PERFORMED OPERATIONS CHECK, OPERATIONS CHECKED GOOD AT THIS TIME IAW MM 26-10-01.
- [SDR DXTA2013122005602](https://openairdocs.org/sdr/DXTA2013122005602.md): Fitting · corroded · Dec 4, 2013 · N381QS · Cessna 680CE · Wing Miscellaneous Structure
  > CORRODED WING RIB FITTINGS. REPAIRED IAW REPAIR DEF S-680-ATA57/01RD
- [SDR CWQR20130408028](https://openairdocs.org/sdr/CWQR20130408028.md): Heat Exchanger · cracked · Apr 8, 2013 · N381QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION, NOTICED HEAT EXCHANGER SIDE PLATE HAD 3. 35" LONG CRACK AND THE OPPOSITE SIDE WAS ALSO CRACKED IN ONE CORNER. WE PERFORMED A LEAK DOWN TEST OF THE DEFECTIVE HEAT EXCHANGER AND FOUND THAT THE CRACK EXTENDED INTO THE INTERNAL POR
- [SDR CWQR20130408027](https://openairdocs.org/sdr/CWQR20130408027.md): Heat Exchanger · cracked · Apr 8, 2013 · N381QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION, HEAT EXCHANGER SIDE PLATE HAD A.35" LONG CRACK AND THE OPPOSITE SIDE WAS ALSO CRACKED IN ONE CORNER. PERFORMED A LEAK DOWN TEST OF THE DEFECTIVE HEAT EXCHANGER AND FOUND THAT THE CRACK EXTENDED INTO THE INTERNAL PORTION OF THE
- [SDR DXTA2012061804999](https://openairdocs.org/sdr/DXTA2012061804999.md): Uplock · out of adjust · Jun 16, 2012 · N381QS · Cessna 680CE · Landing Gear Position and Warning
  > LANDING GEAR UNLOCK ANNUNCIATOR ILLUMINATED AT FL430 AND REMAINED ON UNTIL GEAR HANDLE WAS SELECTED TO THE DOWN POSITION. PERFORMED SEVERAL LANDING GEAR RETRACTIONS AND EXTENSIONS. NO DEFECTS NOTED. FROZE ALL 3 MLG UPLOCK SWITCHES. OPERATED MLG. NO FAUL
- [SDR DXTA2011051604583](https://openairdocs.org/sdr/DXTA2011051604583.md): Strut · discharged · May 13, 2011 · N381QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. WOW MISCOMPARE CAS MSG ILLUMINATED. GEAR HANDLE WOULD NOT MOVE. CHECKED SQUAT SWITCH RIGGING ON ALL 3 GEARS. NO DEFECTS NOTED, T-SHOT, FOUND THAT NLG STRUT COULD BE COMPRESSED +/- 1" WHICH WOULD DISENGAGE NLG SQ
- [SDR DXTA2010122304376](https://openairdocs.org/sdr/DXTA2010122304376.md): Valve · leaking · Dec 22, 2010 · N381QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > GEAR WOULD NOT RETRACT (HANDLE LOCKED OUT) WOW MISCOMPARE. VISUALLY INSPECTED SQUAT SWITCHES. OPS CHECKED ALL SQUAT SWITCHES AND VERIFIED INPU IN OT IAW PCB JACKED ACFT AND PERFORMED GEAR SWING. NO DISPREANCIES FOUND. CHECKED SERVICE OF NOSE STRUT, FOUND UP
- [SDR DXTA2010120704352](https://openairdocs.org/sdr/DXTA2010120704352.md): Oil System · overserviced · Dec 6, 2010 · N381QS · Cessna 680CE · APU Oil System
  > AFTER LANDING AND WITHIN 3-5 MINS OF STARTING APU AND SELECTING THE BLEED AIR "ON", THE CABIN FILLED WITH SMOKE AND AN ODOR OF OIL. FOUND APU OIL OVER SERVICED. OIL COMING FROM GEAR CASE VENT TUBE. REMOVED 56 CC OF OIL. SERVICED OIL IAW RE-100CS, & MM 49-20
- [SDR DXTA2009051803656](https://openairdocs.org/sdr/DXTA2009051803656.md): Controller · malfunctioned · May 17, 2009 · N381QS · Cessna 680CE · Stabilizer Control System
  > PRIMARY PITCH TRIM FAIL - POSSIBLY RAN AWAY BUT CAUGHT BY THE CREW. SECONDARY TRIM WORKED AS NEEDED. TOOK BOTH CREW MEMBERS TO INITIALLY LEVEL THE PLANE. LANDED WITH NO OTHER EVENT. CDMS LISTED ACTUATOR OR CONTROLLER AS FAULT. TESTED OTHER COMPONENTS OF SYST
- [SDR DXTA2009031603545](https://openairdocs.org/sdr/DXTA2009031603545.md): Display · shorted · Mar 14, 2009 · N381QS · Cessna 680CE · Central Display
  > APPROX 1.5 HR AFTER TAKEOFF THE LT MCDU (FMS CDU) BECAME INOP (BLANK SCREEN / NO RED X) LT MCDU CB WAS NOT TRIPPED. APPROX 5-10 MINS LATER STARTED SMELLING SLIGHT ELECTRICAL ODOR WHICH GREW INTO A STRONG ELECTRICAL ODOR WITHIN 5 MIN. REMOVED AND REPLACED MFD C
- [SDR DXTA200803205](https://openairdocs.org/sdr/DXTA200803205.md): Warning System · false activation · Jul 29, 2008 · N381QS · Cessna 680CE · Stabilizer Control System
  > AFTER TAKEOFF INFLIGHT ANYTIME PITCH TRIM IS ACTIVATED EITHER NOSE UP OR DOWN, AMBER "AP STAB TRIM INOP" & AMBER "PRIMARY STAB TRIM FAIL" & CYAN "AP FAIL A & B" CAS MESSAGES DISPLAYED. PERFORMED OPS CK OF THE PITCH TRIM SWITCHING FOR SEVERAL HOURS WITH ACFT.
- [SDR DXTA200802861](https://openairdocs.org/sdr/DXTA200802861.md): Cabin Pressure · malfunctioned · Feb 10, 2008 · N381QS · Cessna 680CE · Cabin Pressure Control System
  > ON CLIMBOUT, AC PRESSURIZED UNTIL 9.3 PSI SWITCHED TO MANUAL AND WAS ABLE TO CONTROL PRESSURIZATION, SWITCHED BACK TO AUTO FOR THE DESCENT AND APPEARED TO OPERATE NORMALLY IN DESCENT. OPERATIONALLY CHECKED PRESSURIZATION SYS IAW MM CH 21-30-00, NO DISCREPANCI
- [SDR DXTA200802804](https://openairdocs.org/sdr/DXTA200802804.md): Heater · malfunctioned · Jan 28, 2008 · N381QS · Cessna 680CE · Ice Detection
  > AMBER PITOT STATIC COLD R CAME ON DURING T/O ROLL. CYCLED SEVERAL TIMES, INTERMITTENT THEREAFTER. TROUBLESHOT PITOT STATIC SYS AND FOUND SYS TO WORK NORMAL SEVERAL TIMES. COMPLIED WITH PITOT STATIC AND STANDBY HEATER CHECK IAW MM CH 34-11-00. INSPECTED RT PIT
- [SDR DXTA200702245](https://openairdocs.org/sdr/DXTA200702245.md): Unknown · unknown · Jun 6, 2007 · N381QS · Cessna 680CE · Rudder Tab Control System
  > AIRCRAFT REQUIRES 2/3 SCALE LT RUDDER TRIM TO MAINTAIN COORDINATED FLIGHT. [07-09-07] RUDDER SKIN DAMAGED AT UPPER, MIDDLE AND LOWER RUDDER HINGE AREA. REMOVED RUDDER AND REPLACED WITH REPAIRED UNIT FROM CESSNA ICT RS CNQR918C PER 680 MM CH 55-40-00. OPERA
- [SDR DXTA200702229](https://openairdocs.org/sdr/DXTA200702229.md): Coupler · inoperative · May 31, 2007 · N381QS · Cessna 680CE · Drag Control System
  > ON TAKEOFF, WE RECEIVED A (NO TO CAS) MESSAGE THAT WAS CAUSED BY THE SPOILERS. REMOVED AND REPLACED RT SPEED BRAKE COUPLER. PERFORMED ELECTRONIC RIGGING IAW MM 27-60-00. OPS CHECK GOOD.
- [SDR DXTA200601822](https://openairdocs.org/sdr/DXTA200601822.md): Transfer Pump · inoperative · Dec 28, 2006 · N381QS · Cessna 680CE · Fuel Pressure Indicator
  > CROSS FEED (ON) IN AIR (2 OCCASIONS). CROSS FEED VALVES FAILED TO OPEN, BOTH FUEL BOOST PUMPS (LOW PRESS) CAME ON. EICAS MESSAGES APPROPRIATE AMBER FUEL PRESS LOW L-R ON. TROUBLESHOT PROBLEM TO LT BOOST PUMP. REMOVED FAILED BOOST PUMP AND INSTALLED A NEW BOO

## 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 = 'N381QS' AND deregistration_id = 'N381QS-2024-12-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N381QS-2024-12-02/reports

---
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