# Service difficulty reports: N308QS

A list on [N308QS](https://openairdocs.org/aircraft/N308QS.md).

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

- [SDR DXTA2026012006591](https://openairdocs.org/sdr/DXTA2026012006591.md): Battery Pack · faulty · Jan 19, 2026 · N308QS · Cessna 680SOV · Emergency Lighting
  > RIGHT FORWARD EXTERIOR EMERGENCY LIGHT DOES NOT COME ON DURING EMERGENCY LIGHT TEST. REMOVED NR 3 BATTERY. INSTALLED CUSTOMER SUPPLIED NEW EMER BATTERY. OPS CHECKED GOOD. WORK DONE IAW AMM 33-50-10. NO DEFECTS NOTED.
- [SDR DXTA2026011606557](https://openairdocs.org/sdr/DXTA2026011606557.md): Light · inoperative · Jan 15, 2026 · N308QS · Cessna 680SOV · Emergency Lighting
  > DURING EMERGENCY LIGHT PREFLIGHT CHECK THE FORWARD OVER WING LIGHT, SEAT 8 LIGHT, AND AFT WALL EXIT SIGN LIGHT DID NOT ILLUMINATE. WE POWERED UP THE AIRPLANE TO DO THE REST OF THE PREFLIGHT CHECKS AND ALL EMERGENCY LIGHTS ILLUMINATED EXCEPT THE AFT WALL EXIT S
- [SDR DXTA2025053003669](https://openairdocs.org/sdr/DXTA2025053003669.md): G Switch · tripped · May 28, 2025 · N308QS · Cessna 680SOV · Emergency Lighting
  > UPON SHUTDOWN EMER LIGHTS WOULD NOT EXTINGUISH. RESET PILOT/CP 5G SWITCH AND ATTEMPTED POWER CYCLE RESET WITH NEGATIVE RESULT. CORRECTIVE ACTION: CONFIRMED THE ISSUE AND WORKED THROUGH T/S WITH MCC. AND DETERMINED THAT A G·SWITCH HAS BEEN ACTIVATED, FOUND THE
- [SDR DXTA2025052303593](https://openairdocs.org/sdr/DXTA2025052303593.md): Actuator · tight · May 22, 2025 · N308QS · Cessna 680SOV · Nose/Tail Landing Gear
  > DURING CLIMBOUT PASSING 32000 WE GOT A VERY NOTICABLE THUD IN THE COCKPIT FLOOR, A "BUMP IN THE NIGHT". IT COULD BE FELT AND HEARD. IT HAPPENED 3 MORE TIMES AND WERE LESS INTENSE. THE LAST ONE OCCURRED AT CRUISE AT 40000. THERE WERE NO ABNORMAL COCKPIT IND
- [SDR DXTA2025031702721](https://openairdocs.org/sdr/DXTA2025031702721.md): Battery · defective · Mar 16, 2025 · N308QS · Cessna 680SOV · Battery/Charger System
  > BATTERY O'TEMP L RED CAS: AT APPROXIMATELY 4000 FEET ON CLIMB OUT RED MASTER, WARNING, LIGHT, ORAL ALERT, AND BATTERY OVER TEMP LEFT CAS MESSAGE ILLUMINATED. ACCOMPLISHED QRC CHECKLIST. LEFT BATTERY APPEARED TO BE APPROXIMATELY AT 50°C AND RIGHT AT 35°C ONCE
- [SDR JGVR20250214001](https://openairdocs.org/sdr/JGVR20250214001.md): Door · corroded · Feb 14, 2025 · N308QS · Cessna 680CE · Emergency Exits
  > BLENDED MULTIPLE AREAS OF CORROSION ON THE EMERGENCY EXIT DOOR P/N 6911251-4, REMOVED CONTOUR RING FOR ACCESS AND BLENDED ADDITIONAL AREAS OF CORROSION PERFORMED NDT AND SENT DOOR OUT FOR REPAIRS. REINSTALLED REPAIRED DOOR P/N 6911251-4.
- [SDR JGVR20250123001](https://openairdocs.org/sdr/JGVR20250123001.md): Spar · corroded · Jan 23, 2025 · N308QS · Cessna 680CE · Wing Spar
  > MECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED IN LH MLG WHEEL WELL, AFT WING SPAR LOWER CLIP INBOARD OF BAY 730DL PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER TEXTRON REPAIR MEMO.
- [SDR JGVR20250117001](https://openairdocs.org/sdr/JGVR20250117001.md): Skin · corroded · Jan 17, 2025 · N308QS · Cessna 680CE · Wing, Plate/Skin
  > MECHANICALLY BLENDED 3 AREAS OF CORROSION UNDER RH LOWER WING SKIN, AFT SIDE, INBD OF FLAP PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR DXTA2024111401130](https://openairdocs.org/sdr/DXTA2024111401130.md): Pressure Switch · faulted · Nov 12, 2024 · N308QS · Cessna 680SOV · Aircraft Fuel Distribution System
  > FUEL PRESSURE LOW L AMBER CAS: AFTER TAKEOFF ABOUT 300 FT AGL WE RECEIVED THE FUEL PRESSURE LOW L CAS MESSAGE. RAN THE QRH MESSAGE DID NOT CLEAR. ON FINAL BACK INTO PWK THE MESSAGE CLEARED CORRECTIVE ACTION; REPLACED LH ENGINE FUEL PRESSURE SWITCH IAW CE 680 A
- [SDR 2024F00201](https://openairdocs.org/sdr/2024F00201.md): Spar Cap · corroded · Aug 24, 2024 · N308QS · Cessna 680CE · Wing Spar
  > CORROSION WAS FOUND ON THE 6922435-4 REAR SPAR CAP, LOWER FORWARD ANGLE-RH, NEAR RWS 41. ACCOMPLISHED FIELD REPAIR: FR-680-0116-1466 REV -, FIELD REPAIR-CORROSION, RH WING LOWER AFT SPAR CAP, RWS 39.4-43.2.THE DAMAGE WAS BLENDED OUT AND THE REMAINING THICKNESS
- [SDR EBVR450D121923001](https://openairdocs.org/sdr/EBVR450D121923001.md): Attach Fitting · corroded · Dec 19, 2023 · N308QS · Cessna 680CE · Horizontal Stabilizer, Attach Fittings
  > FRETTING CORROSION ON AFT HORIZONTAL ATTACH FITTINGS, ON THE HORIZONTAL STAB AND VERTICAL STAB. TEXTRON ENGINEERING PER MINOR RECOMMENDED REPAIR MEMO DQ40986M1 DATED 9-8-2023 RESTORE PAINT PROTECTION AND APPLY CORROSION INHIBITING SOLID FILM LUBRICANT.
- [SDR DXTA2023012378980](https://openairdocs.org/sdr/DXTA2023012378980.md): Fuse · blown · Jan 21, 2023 · N308QS · Cessna 680CE · Emergency Lighting
  > CABIN EMERGENCY LIGHTS INOP. EXIT SIGN OVER MAIN CABIN DOOR INOPERATIVE. EXIT SIGNS LT AND RT OF MAIN CABIN DOOR INOPERAITVE. EMERGENCY LIGHT OVER GALLEY INOPERATIVE. AFTER REPLACING #1 BATTERY PACK BLOWN FUSE AND PERFORMING FULL OPERATIONAL CHECK OF THE BATT
- [SDR DXTA2023011778680](https://openairdocs.org/sdr/DXTA2023011778680.md): Apu · defective · Jan 16, 2023 · N308QS · Cessna 680CE · APU Core Engine
  > AFTER STARTING APU, AND AFTER TURNING BLEEDS ON CABIN, AND FLIGHT DECK STARTED TO FILL WITH A THICK HAZE FROM THE INTERIOR OUTLETS. APU REMOVED AND REPLACED IAW AMM 49-00-00
- [SDR 3J7R2023011200001](https://openairdocs.org/sdr/3J7R2023011200001.md): Power Supply · blown · Jan 11, 2023 · N308QS · Cessna 680SOV · Emergency Lighting
  > THE FORWARD EMERGENCY LIGHTS IN THE CABIN AT THE CABIN DOOR ARE INOP, AT LEAST THREE SIGNS ARE OUT. THESE INCLUDE THE EXIT SIGN IN THE OVERHEAD AND THE EXIT SIGNS AT KNEE LEVEL IN THE DOOR WAY.TROUBLESHOT AND FOUND THE FUSE BLOWN ON THE #1 POWER SUPPLY. ISOLAT
- [SDR DXTA2022122376910](https://openairdocs.org/sdr/DXTA2022122376910.md): Battery Pack · defective · Dec 23, 2022 · N308QS · Cessna 680SOV · Emergency Lighting
  > WHEN THE PASSENGER SAFETY PUSH SWITCH WAS TURNED ON DURING DESCENT, NONE OF THE EMERGENCY LIGHTS ILLUMINATED. WITH THE EMERGENCY LIGHTS SWITCH IN THE ARM POSITION AND THE PAX SAFETY SWITCH ON, ALL EMERGENCY LIGHTS SHOULD ILLUMINATE. UPON FURTHER INVESTIGATION
- [SDR DXTA2021122854310](https://openairdocs.org/sdr/DXTA2021122854310.md): Unknown · unknown · Dec 27, 2021 · N308QS · Gulstm 680 · Emergency Lighting
  > CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS INOP. WOULD NOT COME ON DURING PREFLIGHT, LIGHTS WORK ON NORMAL BATTERY POWER. (PRE-FLIGHT) // SIGNOFF // COMPLIED WITH TC-FLT ·33-1001;CESSNA 680 / 680A / 700 / EMBRAER EMERGENCY LIGHTING POWER SUPPLY REV 0 DATED 15D
- [SDR JGVR20210429001](https://openairdocs.org/sdr/JGVR20210429001.md): Spar · corroded · Apr 29, 2021 · N308QS · Cessna 680CE · Wing Spar
  > BENDED CORRODED ARE AROUND THE LH WING MIDDLE SPAR AFT SIDE AROUND THE BRAKE LINE BULKHEAD FITTING, PERFORMED ULTRASONIC THICKNESS INSPECTION AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED BLENDED AREA, APPLIED PRIMER AND TOPCOAT IAW TEXTRON REPAIR
- [SDR DXTA030120213881](https://openairdocs.org/sdr/DXTA030120213881.md): Pcb · defective · Feb 28, 2021 · N308QS · Cessna 680CE · Ice/Rain Protection System Wiring
  > WING ANTI-ICE COLD L AMBER CAS: AT FL220 IN ICING CONDITIONS, WING ANTI-ICE COLD L&R AMBER MSG ILLUMINATED. DUE TO ATC CONDITIONS AND COMM ISSUES, WE DECLARED AN EMERGENCY TO GET AN IMMIDIATE CLIMB TO FL270 AND OUT OF ICING CONDITIONS. ONCE AT FL270, AND CLEAR
- [SDR 2020FA0000558](https://openairdocs.org/sdr/2020FA0000558.md): Spar Cap · corroded · Dec 20, 2020 · N308QS · Cessna 680SOV · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER AFT SPAR CAP DAMAGE (CORROSION). ENGINEERING MEMO DQ28088M1 DATED DECEMBER 7, 2020.
- [SDR DXTA2020111504357](https://openairdocs.org/sdr/DXTA2020111504357.md): Battery Pack · inoperative · Nov 15, 2020 · N308QS · Cessna 680A · Emergency Lighting
  > EMERGENCY LIGHTS ON RIGHT SIDE INOPERABLE. 2 RIGHT SIDE EXTERIOR OVER WING, RIGHT SIDE SHARK LIGHT, INTERIOR LAV OVERHEAD AND EXIT LIGHTS, AFT FLOOR LIGHTING, RIGHT SIDE AFT READING LIGHT ALL INOPERABLE. APU WAS RUN FOR 1/2 HOUR AND NO CHANGE TO STATUS. CORR
- [SDR DXTA2020092804144](https://openairdocs.org/sdr/DXTA2020092804144.md): Battery Pack · inoperative · Sep 28, 2020 · N308QS · Cessna 680A · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SWITCH IS PLACED TO ARM WITH BATTERIES OFF. FOUND DURING PREFLIGHT. R & R THE NR 1 EMERGENCY BATTERY, CHARGED BATTERY WITH AIRCRAFT SYSTEM ON PERFORMED OPERATIONAL CHECK, ALL CHECKED GOOD. WORK DONE, IAW CE-680 CHAPT
- [SDR DXTA2020011303322](https://openairdocs.org/sdr/DXTA2020011303322.md): Actuator · malfunctioned · Jan 9, 2020 · N308QS · Cessna 680CE · Landing Gear Actuator
  > RIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - RIGHT MAIN DID NOT RETRACT. THE NOSE AND LEFT MAIN RETRACTED NORMALLY. THE RED UNLOCK LIGHT WENT OUT WITH THE RIGHT MAIN DOWN AND LOCKED GREEN LIGHT ON. THE RIGHT MAIN NEVER UNLOCKED AND RETRACTED. DISCONNE
- [SDR DXTA2019123093266](https://openairdocs.org/sdr/DXTA2019123093266.md): Converter · dirty · Dec 29, 2019 · N308QS · Cessna 680CE · Air Distribution System
  > CABIN ODOR OIL SMELL - AT 45000 SLIGHT ORDER AND A LOT OF HAZE IN CABIN. DROPPED OX MASK, RAN CHECK LIST. SELECTED L PRESSURE SOURCE, CABIN CLEARED. REMOVED OILED LEFT OZONE CONVERTER WITH NEW UNIT IAW MM 21-71-00. REMOVED DIRTY COALECER SOCK WITH NEW UNIT
- [SDR DXTA2019071502611](https://openairdocs.org/sdr/DXTA2019071502611.md): Engine · malfunctioned · Jul 12, 2019 · N308QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > REPEAT WRITE UP. DECENDING FROM FL410, POWER WAS REDUCED TO IDLE. AIRCRAFT BEGN TO SHUDDER AND RIGHT ENGINE SHUTDOWN CAS MESSAGE DISPLAYED. RIGHT ENGINE UNCOMMANDED SHUTDOWN FOLLOWED BY AUTO RELIGHT. DID NOT REDUCE POWER TO IDLE AGAIN UNTIL LANDING. NO OTHER
- [SDR DXTA2019061402501](https://openairdocs.org/sdr/DXTA2019061402501.md): Bleed Valve · abnormal · Jun 14, 2019 · N308QS · Cessna 680CE · Compressor Bleed Valve
  > AT FLIGHT LEVEL 43000 WE WERE CLEARED TO DECENT TO 35000. AS WE REDUCED THRUST LEVERS TO IDLE, FELT A RUMBLE, CYAN RIGHT ENGINE SHUTDOWN CAS MESSAGE. RIGHT ENGINE SHUTDOWN FOR A SPLIT SECOND AND RE-LIT IMMEDIATELY. REST OF FLIGHT INTO KMDW NORMAL.// SIGNOFF//P
- [SDR DXTA2019052302430](https://openairdocs.org/sdr/DXTA2019052302430.md): Solenoid · abnormal · May 23, 2019 · N308QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > SHORTLY AFTER INITIATING DESCENT FROM FL430, AND EVENTUALLY AT FLIGHT IDLE, EXPERIENCED TWO SHORT BURSTS OF ENGINE VIBRATION, AND NOTICED THAT THE CYAN ENGINE SHUTDOWN R CAS MESSAGE BRIEFLY DISPLAYED THEN EXTINGUISHED. NO FURTHER VIBRATIONS WERE FELT DURING
- [SDR DXTA2019F00018](https://openairdocs.org/sdr/DXTA2019F00018.md): Spar Cap · damaged · Feb 22, 2019 · N308QS · Cessna 680CE · Wing Spar
  > RT WING FORWARD SPAR CAP ANGLE REPAIR. ACCOMPLISHED IAW AQRD ENGINEERING ORDER ERO-102798 DATED 01/15/2019.
- [SDR JGVR20180316002](https://openairdocs.org/sdr/JGVR20180316002.md): Structure · corroded · Mar 16, 2018 · N308QS · Cessna 680CE · Emergency Exits
  > CORRODED AREAS ON THE UPPER AND LOWER SURFACES OF THE EMERGENCY EXIT DOOR ALONG THE CONTOUR RINGS. BLENDED THE CORROSION. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS, NO CRACKING INDICATIONS FOUND. PERFORMED ULTRASONIC THICKNESS INSPECTION. REPLACED TWO BL
- [SDR JGVR20180316001](https://openairdocs.org/sdr/JGVR20180316001.md): Skin · corroded · Mar 16, 2018 · N308QS · Cessna 680CE · Wing, Plate/Skin
  > REPAIRED TWO CORRODED AREAS ON THE UPPER LT WING SKIN AT WS 37 NEAR THE DRAG ANGLE.
- [SDR DXTA20170406156](https://openairdocs.org/sdr/DXTA20170406156.md): Skin · debonded · Apr 6, 2017 · N308QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIR OF NOSE SKIN DISBONDS AROUND ACCESS DOOR OPENINGS. REPAIRED.
- [SDR DXTA2014060905797](https://openairdocs.org/sdr/DXTA2014060905797.md): Bearing · failed · Jun 6, 2014 · N308QS · Cessna 680CE · Landing Gear Brake System
  > WHEN STOPPING THE ACFT ON THE RAMP BOTH MAIN GEAR BRAKES GROWL & GRAB WHEN MAKING A COMPLETE STOP. TAXIED ACFT FOUND LT & RT BRAKE GROWLING AT VERY SLOW SPEEDS. JACKED ACFT & REMOVED ALL FOUR MAIN WHEEL ASSEMBLIES, REMOVED ALL BEARINGS & CLEANED BEARINGS. C
- [SDR DXTA2014021005643](https://openairdocs.org/sdr/DXTA2014021005643.md): Water Separator · dirty · Feb 8, 2014 · N308QS · Cessna 680CE · Humidity Control System
  > INFLIGHT AT FL 430 PAX COMPLAINED OF SOMETHING BURNING. WE SMELLED IT IN THE FLIGHT DECK., I WENT TO THE BACK & THE ODOR WAS STRONGEST NEAR THE LAVATORY. CREW DONNED MASKS UPON INITIAL SMELL, RAN ALL CHECKLISTS & DIVERTED THE FLIGHT. PERFORMED OZONE CONVERT
- [SDR DXTA2013090305491](https://openairdocs.org/sdr/DXTA2013090305491.md): Converter · failed · Sep 2, 2013 · N308QS · Cessna 680CE · Air Distribution System
  > WHILE RUNNING APU, NOTICED ODOR LIKE DIRTY SOCK. AFTER TAKEOFF, NOTICED ODOR LIKE BURNING OIL. NO SMOKE SEEN. REMOVED AND CLEANED OZONE CONVERTERS REMOVED AND CLEANED HEAT EXCHANGER. RE-INSTALLED HEAT EXCHANGER, PER NETJETS REPLACED R/H OZONE CONVERTER. C
- [SDR DXTA2013081905478](https://openairdocs.org/sdr/DXTA2013081905478.md): Coalescer Bag · contaminated · Aug 18, 2013 · N308QS · Cessna 680CE · Humidity Control System
  > ON GROUND, DURING APU START WITH BATTERIES, CABIN FILLED WITH WHITE SMOKE. APU BLEED AIR AND GENERATOR SWITCHES ON. ENVIROMENTAL SWITCHES AUTO AND COLD. WHITE SMOKE SEEMED TO BE ATOMIZED OIL AND NOT A HARSH ODOR. REMOVED WATER SEPARATOR AND FOUND SOCK TO B
- [SDR DXTA2013081305474](https://openairdocs.org/sdr/DXTA2013081305474.md): Pump · leaking · Aug 11, 2013 · N308QS · Cessna 680CE · Turbine Engine Oil System
  > ENVIRONMENTAL SMOKE NOTICED FROM FRONT WEMAC VENTS. MORE PRONOUNCED IN HP MODE AND DURING POWER REDUCTION. CHECKLIST WAS USED AND IT WOULD SEEM TO BE ISOLATED TO THE LEFT PRESSURE SOURCE. DETERMINED SMOKE TO BE FROM RT ENGINE. REPLACED RT ENGINE OIL PUMP DU
- [SDR DXTA2013020705278](https://openairdocs.org/sdr/DXTA2013020705278.md): Strut · damaged · Feb 7, 2013 · N308QS · Cessna 680CE · Main Landing Gear Strut/Axle/Truck
  > ON DEPARTURE GEAR WOULD NOT RETRACT. 3 GREEN AND RED UNLOCK ILLUMINATED. PUT THE GEAR HANDLE BACK DOWN TO MATCH 3 GREEN CONDITION. SHORTLY AFTER, AMBER "WOW MISCOMPARE" CAS MESSAGE ILLUMINATED. RAN CHECKLIST AND DIVERTED. CAS MESSAGE EXTINGUISHED ON TOUCHD
- [SDR CWQR20120613040](https://openairdocs.org/sdr/CWQR20120613040.md): Cable · frayed · Jun 13, 2012 · N308QS · Cessna 680CE · Brake
  > DURING A SCHEDULED MX EVENT, FOUND THE PILOT'S RT BRAKE CONTROL CABLE FRAYED ABOUT 50 PERCENT. DID NOT SEE ANY ISSUES WITH THE CABLE RUN OR RUBBING ON STRUCTURE, ETC.
- [SDR DXTA2011121904826](https://openairdocs.org/sdr/DXTA2011121904826.md): Flap System · failed · Dec 17, 2011 · N308QS · Cessna 680CE · Trailing Edge Flap Control System
  > WHEN SELECTING FLAPS 15, FLAPS FAILED, AMBER CAS MESSAGE DURING APPROACH AT 180KTS. OBSERVED BITE CODES 5 & 8 ON AFT BAY CONTROLLER. OPS CK OF FLAPS GOOD. MCC REQUEST INSTALLED NEW SOFT START MODULE. OPS CHECKED GOOD. WORK DONE IAW MM 27-51-00.
- [SDR DXTA2011030704495](https://openairdocs.org/sdr/DXTA2011030704495.md): Packing · damaged · Mar 5, 2011 · N308QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > UPON GEAR RETRACTION, NOSE GEAR MADE SEVERAL LOUD "BANGS" WHILE ENTIRE AIRCRAFT SHUDDERED AND VIBRATED. AFTER APPROX 10 SECONDS, NOSE GEAR FINALLY FULLY RETRACTED AND UNSAFE LIGHT EXTINQUISHED. ON GEAR EXTENSION FOR LANDING, WOW MISCOMPARE CAUTION ILLUMINATED
- [SDR DXTA2010111504306](https://openairdocs.org/sdr/DXTA2010111504306.md): Ecu · inoperative · Nov 14, 2010 · N308QS · Cessna 680CE · Cabin Cooling System
  > WITH APU "ON" AND APU BLEED "ON", SMOKED FILLED COCKPIT. FOUND ECU TURBINE TO BE NOT OPERATING. R & R ECU TURBINE. OPS AND LEAK CHECKED GOOD. IAW MM 21-51-00.
- [SDR DXTA2010031904042](https://openairdocs.org/sdr/DXTA2010031904042.md): Downlock Switch · failed · Mar 18, 2010 · N308QS · Cessna 680SOV · Landing Gear Position and Warning
  > RT GREEN GEAR INDICATOR LIGHT ILLUMINATED DURING FLIGHT. NO GEAR UNSAFE LIGHT WAS ASSOCIATED WITH IT. REMOVED RT MAIN GEAR DOWNLOCK SWITCH AND INSTALLED NEW SWITCH IAW MM 32-30. OPS CHECK IS GOOD.
- [SDR DXTA200702562](https://openairdocs.org/sdr/DXTA200702562.md): Warning Light · false indication · Oct 23, 2007 · N308QS · Cessna 680CE · Landing Gear Position and Warning
  > GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CYCLED GEAR ONE TIME. PERFORMED VISUAL INSPECTION OF LANDING GEAR UPLOCK SYSTEM. NO DEFECTS NOTED. VERIFIED PROPER ENGAGMENT OF ALL (3) UPLOCK SWITCHES WITH GEAR IN THE WELL. CYCLED GEAR SEVERAL TIMES AND PERFORMED INDIC
- [SDR DXTA200702309](https://openairdocs.org/sdr/DXTA200702309.md): Lever · out of adjust · Jun 29, 2007 · N308QS · Cessna 680CE · Drag Control System
  > SPEED BRAKE LEVER DOES NOT STAY IN THE FULLY DEPLOYED DETENT, IT TENDS TO (SPRING) BACK TO A HALF DEPLOYED POSTION. ADJUSTED SPEED BRAKE LEVER DETENT. OPERATIONAL CHECK NORMAL IAW MM 76-10-00.

## 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 = 'N308QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N308QS/reports

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