# Service difficulty reports: N315QS

A list on [N315QS](https://openairdocs.org/aircraft/N315QS.md).

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

- [SDR 2026F00213](https://openairdocs.org/sdr/2026F00213.md): Spar Cap · corroded · Sep 23, 2026 · N315QS · Gulstm 680 · Vertical Stabilizer, Spar/Rib
  > CORROSION, VERTICAL STABILIZER, LH AFT SPAR CAP, VFS 116 - VFS 121. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0220-54511 REV -; FIELD REPAIR - CORROSION, VERTICAL STABILIZER, LH AFT SPAR CAP, VFS 116 - VFS 121 DATED 8 SEP 2026. FAA FORM 8100-9 DATED 10
- [SDR DXTA2026072809019](https://openairdocs.org/sdr/DXTA2026072809019.md): Strut · discharged · Jul 26, 2026 · N315QS · Cessna 680SOV · Nose/Tail Landing Gear Strut/Axle
  > WE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA, & THE RED, GEAR UNLOCK LIGHT ILLUMINATED & STAYED ON FOR THE DURATION OF THE FLT UNTIL SELECTED GEAR DOWN AGAIN FOR LANDING. GOT LIGHT IN CLIMB & AT THE TIME WE WERE CLIMBING A
- [SDR 2026072609019](https://openairdocs.org/sdr/2026072609019.md): Landing Gear · faulted · Jul 26, 2026 · N315QS · Cessna 680SOV · Nose/Tail Landing Gear
  > WE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, "GEAR UNLOCK" LIGHT ILLUMINATED AND STAYED ON FOR THE DURATION OF THE FLIGHT UNTIL WE SELECTED GEAR DOWN AGAIN FOR LANDING. WE GOT THE LIGHT IN THE CLIMB
- [SDR DXTA2026072709019](https://openairdocs.org/sdr/DXTA2026072709019.md): Warning Message · illuminated · Jul 26, 2026 · N315QS · Cessna 680SOV · Nose/Tail Landing Gear
  > WE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, GEAR UNLOCK LIGHT ILLUMINATED AND STAYED ON FOR THE DURATION OF THE FLIGHT UNTIL WE SELECTED GEAR DOWN AGAIN FOR LANDING. WE GOT THE LIGHT IN THE CLIMB AN
- [SDR JGVR20251209002](https://openairdocs.org/sdr/JGVR20251209002.md): Skin · corroded · Dec 9, 2025 · N315QS · Cessna 680CE · Wing, Plate/Skin
  > MECHANICALLY BLENDED CORRODED AREA ON LOWER AFT RT WING SKIN, INBOARD OF FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS IAW REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251209001](https://openairdocs.org/sdr/JGVR20251209001.md): Drag Angle · corroded · Dec 9, 2025 · N315QS · Cessna 680CE · Wing Main, Frame Structure
  > BLENDED AREAS OF CORROSION ON THE LOWER AFT DRAG ANGLE, LEFT WING INBD OF FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS WITH NEW, CLEANED, TREATED AND PRIMED AREAS PER REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR DXTA2025111005625](https://openairdocs.org/sdr/DXTA2025111005625.md): Battery · inoperative · Nov 9, 2025 · N315QS · Cessna 680SOV · Emergency Lighting
  > ON PREFLIGHT INSPECTION THE ONLY EMERGENCY LIGHTS THAT ILLUMINATE ARE ADJACENT TO THE MAIN CABIN DOOR AND THE FORWARD AISLE LIGHTS. ALL OTHER INTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED EMERGENCY BATTERY #1 P/N CBS28-1 S/N 3730M, BATTERY#2 P/N CBS28-1 S
- [SDR JGVR20250710001](https://openairdocs.org/sdr/JGVR20250710001.md): Spar · corroded · Jul 10, 2025 · N315QS · Cessna 680CE · Wing Spar
  > MECHANICALLY BLENDED 1 EA. AREA OF CORROSION ON AFT SPAR, LOWER CLIP OUTBD AREA, IN THE RH MLG WHEEL WELL, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREA BY CLEANING, TREATING, AND PRIMING PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR DXTA2025053003695](https://openairdocs.org/sdr/DXTA2025053003695.md): Elec Connector · open · May 9, 2025 · N315QS · Cessna 680SOV · Landing Gear System Wiring
  > GEAR SELECTED DOWN. RIGHT MAIN GEAR DID NOT ILLUMINATE DOWN. AND THE UNLOCKED LIGHT WAS ILLUMINATED. WE RAN THE FULL GEAR DID NOT EXTEND QRH WITH NO CHANGE TO THE INDICATIONS. CORRECTIVE ACTION: WE PERFORMED TS OF THE RH MLG INDICATION DISCREPANCY. AT RH CONNE
- [SDR DXTA2025031702683](https://openairdocs.org/sdr/DXTA2025031702683.md): Flap System · faulted · Mar 14, 2025 · N315QS · Cessna 680SOV · Trailing Edge Flap Control System
  > FLAPS FAIL AMBER CAS: WHEN SELECTING FLAP POSITION 15 AMBER CAS FLAP FAIL MESSAGE APPEARED. FLAPS DID NOT MOVE FROM ZERO POSITION. CORRECTIVE ACTION; POWERED UP AIRCRAFT AND DISCOVERED 'BITE 2' AND 'BITE 6' FAULTED ON FLAP CONTROLLER AS A RESULT OF FLAP FAIL.
- [SDR DXTA2025010701838](https://openairdocs.org/sdr/DXTA2025010701838.md): Landing Gear · faulted · Jan 4, 2025 · N315QS · Cessna 680SOV · Landing Gear Retraction/Extension System
  > DURING DEPARTURE OUT OF TNCM RAISED THE GEAR AFTER T/O AND HEARD A NOISE THEN NOTICED THAT BOTH MAIN LANDING GEAR STILL INDICATED DOWN WITH GREEN DOWN GEAR INDICATION. THE NOSE GEAR LIGHT WAS OUT. PERFORMED THE QRH PROCEDURE AND LOWERED GEAR HANDLE AND GOT ALL
- [SDR 2024F00304](https://openairdocs.org/sdr/2024F00304.md): Skin · corroded · Nov 22, 2024 · N315QS · Cessna 680A · Horizontal Stabilizer, Plate/Skin
  > LH AND RH HORIZONTAL STAB UPPER AND LOWER SKIN HAS AREAS OF CORROSION JUST FWD OF ACCESS PANELS 351AC AND 352AC. MECHANICALLY REMOVED CORROSION ON LH UPPER AND LOWER HORIZONTAL STAB SKIN TRAILING EDGE JUST FWD OF ACCESS PANEL 351AC AND CORROSION ON RH UPPER AN
- [SDR 2024F00303](https://openairdocs.org/sdr/2024F00303.md): Fitting · corroded · Nov 21, 2024 · N315QS · Cessna 680A · Wing Main, Frame Structure
  > RH WING SPOILER HYDRAULIC LINE CARRY THRU FITTINGS ON AFT WING SPAR JUST INBD OF WING JACKING POINT HAS 2 CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHANICALLY BLENDED 2 EA. AREAS OF CORROSION AROUND RH WING HYDRAULIC LINE CARRY THROUGH FITTINGS ON AFT
- [SDR 2024F00301](https://openairdocs.org/sdr/2024F00301.md): Stringer · cracked · Nov 21, 2024 · N315QS · Cessna 680A · Fuselage Main, Longeron/Stringer
  > REPAIRED CRACKED TAILCONE/STRINGER FIREWALL WEB CRACK PER NETJETS RFTS-112267. REV.0 TITLED "N315QS (680-0220) TAILCONE FIREWALL WEB CRACK" DATED 18NOV24.
- [SDR 2024F00300](https://openairdocs.org/sdr/2024F00300.md): Control Cable · chafed · Nov 21, 2024 · N315QS · Cessna 680A · Aileron Control System
  > DURING TASK 27-60-00-2200, FOUND RH WING AILERON OUTPUT CABLE CHAFFING DRAIN TUBE NEXT TO SPOILER MIXER BOX. REMOVED EXISTING DRAIN TUBE FROM AIRCRAFT. REPAIRED DRAIN TUBE PER NJA RFTS-112277, REV 0, TITLE: N315QS (680-0220) WATER DRAIN LINE CHAFE, DATED: 15NO
- [SDR 2024F00299](https://openairdocs.org/sdr/2024F00299.md): Stringer · corroded · Nov 21, 2024 · N315QS · Cessna 680A · Fuselage Main, Longeron/Stringer
  > STINGER HAS 1 AREA OF CORROSION ON LOWER AFT SIDE NEAR DRAIN HOLE. MECHANICALLY BLENDED 1 AREA OF CORROSION ON STINGER LOWER AFT SIDE NEAR DRAIN HOLE. EVALUATED AND FOUND AREA TO BE BEYOND LIMITS. SUBMITTED AREA TO NJA ENGINEERING FOR REPAIR. REPAIRED AREA PER
- [SDR 2024F00298](https://openairdocs.org/sdr/2024F00298.md): Hinge · corroded · Nov 21, 2024 · N315QS · Cessna 680A · Rudder Structure
  > FOUND AN AREA OF CORROSION ON LOWER RUDDER HINGE. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON RUDDER LOWER HINGE, AFT END, LH SIDE UPPER AREA. EVALUATED AND FOUND TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02. SUBMITTED TO NJA ENGINEERING AND TEXTRON
- [SDR 2024F00297](https://openairdocs.org/sdr/2024F00297.md): Rib · corroded · Nov 21, 2024 · N315QS · Cessna 680A · Wing, Rib/Bulkhead
  > LH WING INBD FLAP COVE SUPPORT RIB HAS CORROSION WHERE HYD STAND-OFF BRACKET IS ATTACHED. MECHANICALLY REMOVED CORROSION LOCATED ON LH WING INBD FLAP COVE SUPPORT RIB, OUTBD SIDE WHERE HYD STAND-OFF BRACKET IS ATTACHED IAW C680 SRM 51-70-02. FOUND CORROSION BL
- [SDR 2024F00302](https://openairdocs.org/sdr/2024F00302.md): Fitting · corroded · Nov 21, 2024 · N315QS · Cessna 680A · Wing Main, Frame Structure
  > LH WING SPOILER HYDRAULIC LINE CARRY THRU FITTINGS ON AFT WING SPAR JUST INBD OF WING JACKING POINT HAS 2 CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHANICALLY BLENDED 3 EA. AREAS OF CORROSION AROUND LH WING HYDRAULIC LINE CARRY THROUGH FITTINGS ON AFT
- [SDR 2024FA0000859](https://openairdocs.org/sdr/2024FA0000859.md): Spar · corroded · Nov 21, 2024 · N315QS · Cessna 680A · Wing Spar
  > LH MLG WHEEL WELL AFT SPAR, FWD FACE HAS 1 AREA OF CORROSION INBD OF WS 37.00. MECHANICALLY REMOVED CORROSION LOCATED IN LH MLG WHEEL WELL, AFT SPAR, FWD FACE INBD OF WS 37.00 APX 21 INCHES IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW C
- [SDR DXTA2023090594410](https://openairdocs.org/sdr/DXTA2023090594410.md): Unknown · unknown · Sep 1, 2023 · N315QS · Cessna 680CE · Electrical Power System
  > AVIONICS POWER: WITH THE MAIN POWER ON DURING FINAL DESCENT MY SIC IN THE RIGHT SEAT SMELLED A FAINT ELECTRICAL SMELL RIGHT BEFORE I DID. IT SEEMED TO GO AWAY AND WE LANDED VERY SHORTLY AFTERWARD. UPON STARTING APU THE SMELL CAME BACK MUCH STRONGER AND SMELLED
- [SDR DXTA2022112274220](https://openairdocs.org/sdr/DXTA2022112274220.md): Spring · broken · Nov 21, 2022 · N315QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR COUNTER WEIGHT SPRING BROKE UNABLE TO CLOSE DOOR WITHOUT HELP. REMOVED AND REPLACED MED FWD COUNTERBALANCE SPRING. PERFORMED RIGGING OF MED COUNTERBALANCE SYSTEM IAD CE680 AMM 52-10-50. MED COUNTERBALANCE SYSTEM OPS CHECK GOOD
- [SDR DXTA2021121053290](https://openairdocs.org/sdr/DXTA2021121053290.md): None · none · Dec 9, 2021 · N315QS · Cessna 680CE · Landing Gear Brake System
  > RIGHT MLG BRAKE: RIGHT BRAKE REQUIRED MUCH GREATER THAN NORMAL APPLICATION FORCE BEFORE IT WOULD ENGAGE DURING LANDING ROLLOUT (REPORTED FROM RIGHT SEAT PILOT) // SIGNOFF// VISUALLY INSPECTED BOTH INBOARD AND OUTBOARD RH BRAKE ASSEMBLES FOR ANY DEFECTS/ LEAKS.
- [SDR DXTA2021090948510](https://openairdocs.org/sdr/DXTA2021090948510.md): Engine · leaking · Sep 8, 2021 · N315QS · Cessna 680CE · Turbine Engine Oil System
  > COCKPIT ODOR: ABNORMAL ODOR IN COCKPIT AT TAKEOFF POWER. LENGTHY 10-15 MIN TAXI WITH APU OFF. APPLIED TAKEOFF POWER AND WITHIN 5 SECS NOTED UNUSUALLY STRONG ABNORMAL ENVIRON ODOR. ABORTED TAKEOFF AND ODOR APPEARED TO QUICKLY DISSIPATE AS POWER BACK TO IDLE
- [SDR DXTA2021090748310](https://openairdocs.org/sdr/DXTA2021090748310.md): Unknown · odor · Sep 5, 2021 · N315QS · Cessna 680CE · Air Distribution System
  > COCKPIT ODOR: REPEAT WRITE UP. WITH APU OFF UNPLEASANT STRONG ABNORMAL ODOR IN COCKPIT AND CABIN AFTER TAKEOFF. ODOR WAS ENVIONMENTAL IN NATURE AND WAS STRONGEST AFTER TAKEOFF, IT DISSIPATED DURING THE CLIMB BUT DID BECOME STRONGER IN THE DESCENT OR WITH LA
- [SDR DXTA2021090748150](https://openairdocs.org/sdr/DXTA2021090748150.md): Condenser · dirty · Sep 3, 2021 · N315QS · Cessna 680CE · Air Distribution System
  > COCKPIT ODOR: UNPLEASANT UNUSUALLY STRONG ABNORMAL ODOR IN COCKPIT JUST AFTER TAKEOFF. ODOR SEEMED TO BE ENVIRONMENTAL, ALMOST OILY IN NATURE BUT NOT ELECTRICAL OR GAS. NO SMOKE/HAZE OBSERVED. ODOR DISSIPATED AND THEN REOCCURRED ON INITIAL DESCENT AND POWER CH
- [SDR JGVR20200303001](https://openairdocs.org/sdr/JGVR20200303001.md): Not Reported · corroded · Mar 3, 2020 · N315QS · Cessna 680A · Fuselage Miscellaneous Structure
  > REPAIRED SPOTS OF CORROSION ON LH AND RH SIDES OF FORWARD DROPPED AISLE PER AEROSPACE QRD ERO-965791, TITLED "FUSELAGE REPAIR", DATED 27 FEB 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED FEBRUARY 27, 2020.
- [SDR JGVR20180110001](https://openairdocs.org/sdr/JGVR20180110001.md): Door · corroded · Jan 10, 2018 · N315QS · Cessna 680CE · Emergency Exits
  > EMERGENCY EXIT DOOR CORRODED BEYOND ECONOMIC REPAIR, REPLACED THE DOOR.
- [SDR JGVR20180109001](https://openairdocs.org/sdr/JGVR20180109001.md): Rib · corroded · Jan 9, 2018 · N315QS · Cessna 680CE · Wing, Rib/Bulkhead
  > REPAIRED AREAS OF CORROSION ON LOWER FLANGE OF WING RIB P/N 6922037-20, AT WING STATION 18.50 IN RT MLG WELL PER ENGINEERING MEMO DQ10680M1, DATED JANUARY 5, 2018.
- [SDR JGVR20170915001](https://openairdocs.org/sdr/JGVR20170915001.md): Structure · corroded · Sep 15, 2017 · N315QS · Cessna 680CE · Emergency Exits
  > EMERGENCY EXIT HAS CORROSION AROUND MULTIPLE NUT PLATES UNDER CONTOUR RING. BLENDED AREAS. PERFORMED EDDY CURRENT INSPECTION ON BLENDED AREAS. NO CRACKS OR CORROSION INDICATIONS NOTED. PERFORMED ULTRASONIC THICKNESS INSPECTION ON BLENDED AREAS. PREPPED, T
- [SDR DXTAT2PL6D0059SG2](https://openairdocs.org/sdr/DXTAT2PL6D0059SG2.md): Uplock Switch · out of adjust · Jul 24, 2017 · N315QS · Cessna 680SOV · Landing Gear Position and Warning
  > DURING TAKEOFF, THE GEAR HANDLE WAS PLACED IN THE FULL UP POSITION. ALL GREEN GEAR INDICATIONS EXTINGUISHED BUT THE RED UNLOCK LIGHT REMAINED ILLUMINATED. CHECKLIST PROCEDURES WERE PERFORMED AND ALL GEAR EXTENDED AND LOCKED DOWN. PERFORMED LANDING GEAR SWINGS
- [SDR DXTA2017033106391](https://openairdocs.org/sdr/DXTA2017033106391.md): Apu · coked · Mar 31, 2017 · N315QS · Cessna 680CE · APU Core Engine
  > WHEN HEAT CAME ON AT CRUISE ALTITUDE, A VERY STRONG BURNED OIL ODOR COMES OUT OF THE VENTS. HAD TO TURN THE HEAT DOWN TO AN UNCOMFORTABLY COOLER TEMPERATURE TO REDUCE THE ODOR. TROUBLESHOT THE OIL ODOR, REMOVED THE INLET TO THE APU AND BORESCOPING THE INTAKE A
- [SDR CWQR20131002041](https://openairdocs.org/sdr/CWQR20131002041.md): Tube · cracked · Sep 25, 2013 · N315QS · Cessna 680CE · APU Bleed Air System
  > DURING SCHEDULED INSPECTION, WE FOUND APU BLEED AIR TUBE ASSY CRACKED AT THE APU COMPARTMENT ATTACH FLANGE. THE FLANGE WAS CRACKED 2 TO 3" WHERE THE FLANGE IS WELDED TO THE TUBE ASSY.
- [SDR DXTA2012043004966](https://openairdocs.org/sdr/DXTA2012043004966.md): Hose · damaged · Apr 27, 2012 · N315QS · Cessna 680CE · Hydraulic System, Main
  > DEPARTED, MOVED GEAR HANDLE TO UP, NOSE GEAR FAILED TO RETRACT FOLLOWED BY BOTH A HYD PRESSURE LOW LT AND HYD VOLUMN LOW AMBER CAS MESSAGES. RETURNED TO DEPARTURE WITH 3 GREEN INDICATIONS AND LANDED UNEVENTFULL. HYD FLUID CAME OUT OF NOSE GEAR AREA AND ON R
- [SDR 2011FA0000341](https://openairdocs.org/sdr/2011FA0000341.md): Tube · cracked · May 16, 2011 · N315QS · Cessna 680CE · Pneumatic Distribution System
  > FOUND SERVICE AIR TUBE ASSY CRACKED IN BEND RADIUS THAT LEADS TO THE RUDDER ACTUATOR IN THE TAIL
- [SDR DXTA2009090803773](https://openairdocs.org/sdr/DXTA2009090803773.md): Engine · vibration · Sep 7, 2009 · N315QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > RED ENGINE VIBRATION R CAS MSG POSTED REPEATEDLY FOR A FEW SECONDS EACH TIME AND THEN DISAPPEARED ( N1 96.3, N2 95.4, FL 360, SAT -52*C, RAT -25*C, ISA +3) CRUISE PWR WAS SET. NO VIBRATION WAS EVER EXPERENCED. REPLACED ENGINE HARNESS WIRE PINS AND SOCKET
- [SDR DXTA2008122303425](https://openairdocs.org/sdr/DXTA2008122303425.md): Tire · failed · Dec 21, 2008 · N315QS · Cessna 680CE · Wheel/Ski/Float
  > BOTH RIGHT MAIN TIRES BLEW ON LANDING. LEFT INBOARD MAIN TIRE FLAT. LEFT OUTBOARD MAIN TIRE FLAT. RIGHT MAIN GEAR DOOR DAMAGED ON LANDING.
- [SDR DXTA20082907](https://openairdocs.org/sdr/DXTA20082907.md): Unknown · unknown · Feb 1, 2008 · N315QS · Cessna 560CESSNA · Landing Gear System
  > AFTER DEPARTING, A CONTAMINATING RUNWAY GEAR UNLOCKED LIGHT, ILLUMINATED. CLEANED GEAR AND FLAP WELLS, INSPECTED, AND OPERATED SYSTEMS NUMEROUS TIMES WITH NO DEFECTS NOTED.

## 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 = 'N315QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N315QS/reports

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