# Service difficulty reports: N313QS

A list on [N313QS](https://openairdocs.org/aircraft/N313QS.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 · 54 reports

- [SDR JGVR20260516201](https://openairdocs.org/sdr/JGVR20260516201.md): Skin · corroded · May 16, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > BLENDED MULTIPLE AREAS OF CORROSION ON THE UPPER AND LOWER SKINS OF THE HORIZONTAL STABILIZER, NEAR LT AND RT TIP CAP, LH AND RH IB ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED, AND TOPCOATED AREAS.
- [SDR JGVR20260515204](https://openairdocs.org/sdr/JGVR20260515204.md): Skin · corroded · May 15, 2026 · N313QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > MECHANICALLY REMOVED 1 AREA OF CORROSION ON THE UPPER AFT CORNER OF THE CUT OUT OF THE E-EXIT ON FUSELAGE SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20260515203](https://openairdocs.org/sdr/JGVR20260515203.md): Spar · corroded · May 15, 2026 · N313QS · Cessna 680CE · Wing Spar
  > MECHANICALLY REMOVED CORROSION LOCATED ON RH WING AFT SPAR, AFT FACE OF SPAR WEB BELOW SPOILER PANEL #9 AROUND PRESSURE AND RETURN HYDRAULIC LINE CARRY THROUGH FITTINGS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER
- [SDR JGVR20260515202](https://openairdocs.org/sdr/JGVR20260515202.md): Spar Cap · corroded · May 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Spar/Rib
  > MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED INSIDE LH HORIZONTAL STAB ELEVATOR COVE, LOWER SPAR CLIP BETWEEN INBOARD AND MIDDLE ELEVATOR HINGE ATTACHMENTS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS
- [SDR JGVR20260515001](https://openairdocs.org/sdr/JGVR20260515001.md): Skin · corroded · May 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > MECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICA
- [SDR JGVR20260515201](https://openairdocs.org/sdr/JGVR20260515201.md): Skin · corroded · May 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > MECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICA
- [SDR 2025FA0000779](https://openairdocs.org/sdr/2025FA0000779.md): Wing Root · corroded · Nov 21, 2025 · N313QS · Cessna 680CE · Fuselage, Wing Attach Fittings
  > CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.
- [SDR 2025FA0000771](https://openairdocs.org/sdr/2025FA0000771.md): Wing Root · corroded · Nov 19, 2025 · N313QS · Cessna 680CE · Wing, Fuselage Attach Fittings
  > CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.
- [SDR 2025FA0000740](https://openairdocs.org/sdr/2025FA0000740.md): Skin · corroded · Nov 4, 2025 · N313QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCATED ON AFT FUSELAGE AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATE PLATE. PERFORMED ULTRASONIC REMAI
- [SDR 2025FA0000739](https://openairdocs.org/sdr/2025FA0000739.md): Skin · corroded · Nov 4, 2025 · N313QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCATED ON AFT FUSELAGE AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATE PLATE. PERFORMED ULTRASONIC REMAI
- [SDR DXTA2025060603759](https://openairdocs.org/sdr/DXTA2025060603759.md): Battery Pack · inoperative · Jun 3, 2025 · N313QS · Cessna 680SOV · Emergency Lighting
  > LIGHTS CONNECTED TO THEIR RESPECTIVE EMERGENCY LIGHTING BATTERY PACK FAILED TO OPERATE AFTER TWO 30 MINUTE CHARGING SESSIONS. THE TWO LOWER SIDES OF MAIN CABIN DOOR FRAME, ONE ABOVE EMERGENCY EXIT, ONE ON BULKHEAD BEHIND SEAT 9. CORRECTIVE ACTION: REMOVED AND
- [SDR 2024FA0000757](https://openairdocs.org/sdr/2024FA0000757.md): Skin · corroded · Oct 7, 2024 · N313QS · Cessna 680A · Vertical Stabilizer, Plate/Skin
  > REPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER SKINS LOCATED NEAR THE UPPER EDGE AND ONE NEAR THE FORWARD EDGE BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DEPOSITION, CLEANING, TREATING, PRIMING AND FABRICATING AND INSTALLING REPAIR DOUBLERS IAW AERO
- [SDR DXTA2024090300378](https://openairdocs.org/sdr/DXTA2024090300378.md): Fuse · defective · Aug 29, 2024 · N313QS · Cessna 680SOV · Emergency Lighting
  > EMERG EXIT SIGN/LIGHT: THE AFT LAV EMERGENCY EXIT SIGN IS INOP. THE AFT DIVIDER OVERHEAD EMERGENCY EXIT SIGN IS INOP. CORRECTIVE ACTION: CHECKED THE EMERGENCY POWER SUPPLY BATTERY #4 FUSE AND FOUND IT BURNT. PERFORMED WIRING CHECK AND FOUND WIRES GOING TO THE
- [SDR DXTA2024062512164](https://openairdocs.org/sdr/DXTA2024062512164.md): Fadec · faulted · Jun 25, 2024 · N313QS · Cessna 680CE · Fuel Controlling System
  > DURING DESCENT FROM FL350 WITH ANTI-ICE ON THE ENGINE CONTROL FAULT R AMBER CAS MESSAGE ILLUMINATED. FAULT MESSAGE WAS RESET AFTER PUSHING THE FADEC RESET. REMOVED PN HG1153CA04, SN 08053096 DUE TO "RH ENG CONTROL FAULT" CAS MESSAGE. INSTALLED A REPAIRED UN
- [SDR DXTA2023082894000](https://openairdocs.org/sdr/DXTA2023082894000.md): Fuse · blown · Aug 27, 2023 · N313QS · Cessna 680CE · Emergency Lighting
  > ON PREFLIGHT, ALL EMERGENCY LIGHTS INTERIOR AND EXTERIOR DO NOT ILLUMINATE WITH THE EMER LTS SELECTED ON. IN ARM, AFT EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. MET WITH CREW AND VERIFIED DISCREPANCY. GAINED ACCESS TO #4 EMER LIGHT POWER SUPPLY AND INSPECTED CO
- [SDR JGVR20230720001](https://openairdocs.org/sdr/JGVR20230720001.md): Unknown · unknown · Jul 20, 2023 · N313QS · Cessna 680CE · Horizontal Stabilizer Structure
  > REPAIRED CRACKED INBOARD END RIB OF THE RH HORIZONTAL STABILIZER, LOWER FLANGE AT RBL 8.8, PER REPAIR -2 OF TEXTRON REPAIR DEFINITION S-680-ATA55/08RD REVISION – BY NDT MAPPING CRACK, TRIMMING CRACKED AREA, FABRICATING AND INSTALLING REPAIR PIECES.
- [SDR DXTA2022112374570](https://openairdocs.org/sdr/DXTA2022112374570.md): Coalescer Bag · dirty · Nov 22, 2022 · N313QS · Cessna 680CE · Air Distribution System
  > DEPARTED APF, APU OFF FOR TAKEOFF. LEVELED OFF AT 2000 FT PER CLEARANCE & NOTICED A HOT BURNING OIL ODOR, REDUCED POWER AT 2,000 FT TO KEEP A SLOW AIRSPEED, ODOR BEGAN TO EASE. VISUAL INSP SHOWED NO OIL ON ENG COWLINGS OR UNDER APU. OIL LEVELS CHECKED G
- [SDR DXTA2022062764570](https://openairdocs.org/sdr/DXTA2022062764570.md): Acm · defective · Jun 24, 2022 · N313QS · Cessna 680A · APU Cowling/Containment
  > APU BLEED AIR: COULD NOT CONTROL CABIN TEMP BELOW 80 DEGREES. STARTED APU AND SELECTED BLEED AIR ON. ODOR OF BURNT OIL ENTERED CABIN AND THEN BLEED SELECTED OFF. ON GROUND BEFORE FLIGHT THERE WAS NO ODOR W BLEED AIR ON. APU WAS STARTED AFTER SLOWING AI
- [SDR DXTA2022011755260](https://openairdocs.org/sdr/DXTA2022011755260.md): Battery Pack · inoperative · Jan 15, 2022 · N313QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTING: WHEN DOING THE EMERGENCY LIGHT CHECK, THE ONLY LIGHTS WORKING ARE THE EXIT LIGHT OVER THE MAIN CABIN DOOR, THE OVERHEAD LIGHT BETWEEN SEATS 3 AND 5 AND THE OVERHEAD LIGHT OVER SEAT 9. THE DOORFRAME EXIT SIGNS, THE AISLE LIGHTING, THE DIVI
- [SDR DXTA2021123154490](https://openairdocs.org/sdr/DXTA2021123154490.md): Unknown · unknown · Dec 30, 2021 · N313QS · Gulstm 680 · Emergency Lighting
  > CABIN EMERG LIGHT: RIGHT SIDE CABIN EMERGENCY LIGHTS INOP. LEFT SIDE OPERATES NORMALLY. // SIGNOFF// RAN APU FOR 1 HOUR TO CHARGE THE EMERGENCY BATTERIES. PREFORMED OPS CHECK OF THE EMERGENCY LIGHTS AND NO DEFECTS FOUND JAW SOVEREIGN 680 AMM 33-50-00
- [SDR DXTA2021121553510](https://openairdocs.org/sdr/DXTA2021121553510.md): Controller · defective · Dec 13, 2021 · N313QS · Cessna 680CE · Brake Anti-Skid Section
  > ANTISKID FAIL AMBER CAS: ON CLIMB OUT WE HAD A FLICKERING AMBER ANTISKID FAIL CAS MESSAGE. THE CHECKLIST HAD US TURN IT OFF SINCE THE MESSAGE WOULD NOT CLEAR. WE LANDED IN THE OFF POSITION. // SIGNOFF // REMOVED THE ANTI-SKID CONTROLLER AND INSTALLED SERVICEAB
- [SDR JGVR20210319003](https://openairdocs.org/sdr/JGVR20210319003.md): Skin · corroded · Mar 19, 2021 · N313QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED CORRODED AREAS OF THE LOWER SURFACE OF THE RH LOWER WING SKIN, BELOW THE AFT SPAR CAP NEAR THE MAIN LANDING GEAR WHEEL WELL AREA, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS AS REQUIRED, TREATED, PRIMED, AND TOP COATED
- [SDR DXTA022220213833](https://openairdocs.org/sdr/DXTA022220213833.md): Wheel · iced · Feb 18, 2021 · N313QS · Cessna 680CE · Wheel/Ski/Float
  > RIGHT INBOARD MLG TIRE: BRAKE FROZEN. TIRE DAMAGED. WE FOUND THAT THERE WAS ICE BUILD-UP 0F THE RT INBOARD BRAKE. AFTER REMOVING THE ICE WE WERE ABLE TO TURN THE WHEEL AND WE CONFIRMED THAT THE TIRE WILL NEED TO BE REPLACED. WE REMOVED THE MLG WHEEL ASSY RE
- [SDR DXTA021920213833](https://openairdocs.org/sdr/DXTA021920213833.md): Brake · frozen · Feb 18, 2021 · N313QS · Cessna 680CE · Landing Gear Brake System
  > RIGHT INBOARD MLG TIRE: BRAKE FROZEN. TIRE DAMAGED.
- [SDR JGVR202002192001](https://openairdocs.org/sdr/JGVR202002192001.md): Spar · corroded · Feb 20, 2020 · N313QS · Cessna 680A · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB HAS 1 AREA OF VERIFIED CORROSION ON LH SPAR CLIP BELOW UPPER RUDDER HINGE. FOUND DURING 6 MONTH INSPECTION. REMOVED LEVEL 1 CORROSION FROM VERTICAL STAB LH SPAR CLIP BELOW UPPER RUDDER HINGE IAW CESSNA 680 SRM 51-70-02. FOUND BLENDED AREA TO BE B
- [SDR DXTA2019111403074](https://openairdocs.org/sdr/DXTA2019111403074.md): Strut · stuck · Nov 13, 2019 · N313QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > ALL LANDING GEAR RETRACTION DID NOT RETRACT - WHEN NOSEWHEEL CAME OFF THE GROUND ON TAKEOFF, THE MASTER WARNING LIGHT ILLUMINATED. THE GEAR HANDLE WOULD NOT MOVE AND "WOW MISCOMPARE" AMBER CAS MESSAGE DISPLAYED. "CORRECTIVE ACTION" TROUBLESHOT LANDING GEAR SYS
- [SDR DXTA2018030800694](https://openairdocs.org/sdr/DXTA2018030800694.md): Compressor · stalled · Mar 8, 2018 · N313QS · Cessna 680CE · Turbine Engine Compressor Section
  > DURING CLIMB OUT, AT APPROXIMATELY FL 350 IN MCT THRUST, THERE WERE SEVERAL ENGINE COMPRESSOR STALLS ON THE RT ENGINE. DURING THE STALLS THE ITT EXCEEDED 900. THE STALLS WERE SEVERE ENOUGH TO CAUSE THE AIRPLANE TO YAW. THE STALLS WENT AWAY WHEN POWER WAS REDUC
- [SDR DXTA2018010400434](https://openairdocs.org/sdr/DXTA2018010400434.md): Unknown · smoke · Jan 2, 2018 · N313QS · Cessna 680SOV · Air Distribution System
  > SHORTLY AFTER STARTING THE APU AND SELECTING BLEED ON, A GRAYISH SMOKE COULD BE SMELLED AND SEEN THROUGHOUT THE CABIN AND COCKPIT. SMOKE DISSIPATED AFTER APU SHUT DOWN.
- [SDR DXTAT2PL6D005MFJN](https://openairdocs.org/sdr/DXTAT2PL6D005MFJN.md): Bleed Valve · defective · Dec 27, 2017 · N313QS · Cessna 680CE · Compressor Bleed Valve
  > AT CRUISE FL340, THE AIRPLANE MADE A LOUD POP, THEN A BANG, FOLLOWED BY A VIBRATION, YAW, AND ITT OVERTEMP/ N1 OVERSPEED ON THE RIGHT ENGINE. BOTH POWER LEVERS REDUCED IMMEDIATELY. BOTH ENGINE PARAMETERS INDICATED NORMAL RANGES. FLIGHT RETURNED TO DEPARTURE A
- [SDR JGVR20170823001](https://openairdocs.org/sdr/JGVR20170823001.md): Door · corroded · Aug 23, 2017 · N313QS · Cessna 680CE · Emergency Exits
  > EMERGENCY EXIT DOOR SKIN HAS SEVERAL AREAS OF CORROSION AROUND PERIPHERY NEAR COMPOSITE RING. FOUND DURING PAINT PROCESS. REMOVED SEAL AND COMPOSITE RINGS AND BLENDED CORROSION. CORROSION FOUND TO BE BEYOND LIMITS. REMOVED THE EMERGENCY EXIT DOOR, AND INSTA
- [SDR 2017F00165](https://openairdocs.org/sdr/2017F00165.md): Fairing · damaged · Jul 13, 2017 · N313QS · Cessna 680CE · Aerodynamic Fairings
  > FAIRING DAMAGE.
- [SDR 2017F00156](https://openairdocs.org/sdr/2017F00156.md): Skin · corroded · Jul 12, 2017 · N313QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER LEFT AND RIGHT SKIN DAMAGE.
- [SDR 2017F00151](https://openairdocs.org/sdr/2017F00151.md): Skin · corroded · Jul 7, 2017 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > HORIZONTAL STABILIZER LEFT AND RIGHT UPPER AND LOWER SKIN DAMAGE.
- [SDR 2017F00149](https://openairdocs.org/sdr/2017F00149.md): Spar · damaged · Jul 6, 2017 · N313QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > VERTICAL FIN REAR SPAR DAMAGED.
- [SDR 2017F00147](https://openairdocs.org/sdr/2017F00147.md): Bulkhead · damaged · Jul 6, 2017 · N313QS · Cessna 680CE · Nacelle/Pylon, Bulkhead/Firewall
  > BULKHEAD BOND ASSY. DAMAGED, DOUBLER CRACKED, NICKED AND DEBONDED.
- [SDR 2017F00146](https://openairdocs.org/sdr/2017F00146.md): Hinge Bracket · corroded · Jul 6, 2017 · N313QS · Cessna 680CE · Rudder Structure
  > RUDDER HINGE BRACKET CORRODED.
- [SDR 2017F00145](https://openairdocs.org/sdr/2017F00145.md): Access Panel · delaminated · Jul 6, 2017 · N313QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB LEADING EDGE UPPER LEFT EDGE DELAMINATED.
- [SDR 2017F00144](https://openairdocs.org/sdr/2017F00144.md): Skin · corroded · Jul 6, 2017 · N313QS · Cessna 680CE · Elevator, Plate/Skin
  > LEFT ELEVATOR SKIN CORRODED.
- [SDR DXTR2016031003](https://openairdocs.org/sdr/DXTR2016031003.md): Skin · corroded · Mar 4, 2016 · N313QS · Cessna 680SOV · Fuselage Main, Plate/Skin
  > CORROSION FOUND AT DISCRETE LOCATIONS ON THE STR AND TAILCONE SKINS. REPAIRED IAW STRUCTURES REPORT S-680-0140/04RD.
- [SDR DXTR2016031002](https://openairdocs.org/sdr/DXTR2016031002.md): Skin · corroded · Mar 4, 2016 · N313QS · Cessna 680SOV · Vertical Stabilizer, Plate/Skin
  > CORROSION FOUND AT MULTIPLE SITES ON THE LT & RT VERTICAL STABILIZER SKINS. REPAIRED IAW STRUCTURES REPORT NR: S-680-014/05RD.
- [SDR DXTR2016031001](https://openairdocs.org/sdr/DXTR2016031001.md): Skin · corroded · Mar 4, 2016 · N313QS · Cessna 680SOV · Wing, Plate/Skin
  > CORROSION DAMAGE FOUND ON LT UPPER WING SKIN. REPAIRED IAW STRUCTURES REPORT NR: S-680-0140/06RD.
- [SDR DXTA2014080605845](https://openairdocs.org/sdr/DXTA2014080605845.md): Control Handle · faulty · Jul 4, 2014 · N313QS · Cessna 680CE · Landing Gear Selector
  > GEAR WOULD NOT RETRACT, GEAR HANDLE COULD NOT BE MOVED. AFTER ACFT WAS JACKED BROUGHT UP CDMS TO LANDING GEAR PAGE. WITH NO HYD TRIED TO PULL GEAR HANDLE BUT HANDLE WOULD NOT PULL FROM DOWN POSITION. VIEWED CDMS & CORRECT COMMANDS WHERE PRESENT POWER & GND
- [SDR DXTA2014080605844](https://openairdocs.org/sdr/DXTA2014080605844.md): Control Handle · faulty · Jul 2, 2014 · N313QS · Cessna 680CE · Landing Gear Selector
  > GEAR WOULD NOT RETRACT, GEAR HANDLE COULD NOT BE MOVED. REMOVED GEAR HANDLE & BENCH CHECKED SOLENOID OPERATION. APPLIED POWER & GND, HANDLE REMAINS LOCKED DOWN. INTERMITTENTLY HANDLE WILL UNLOCK. SOLENOID COIL HAS EXCESSIVE RESISTANCE. GEAR HANDLE ASSEMBL
- [SDR CWQR20131203049](https://openairdocs.org/sdr/CWQR20131203049.md): Filter Element · mismanufactured · Dec 3, 2013 · N313QS · Cessna 680CE · Hydraulic Filter, Main
  > DURING A SCHEDULED INSPECTION WE TRIED TO INSTALL A NEW FILTER ELEMENT. THE ELEMENT WOULD NOT SIT INTO THE BOTTOM OF THE FILTER HOUSING BOWL. THE FILTER WAS REJECTED & RED TAGGED BY THE TECHNICIAN & RETURNED TO THE MATERIALS DEPARTMENT. WE HAD IN THE PAST R
- [SDR DXTA2013111205562](https://openairdocs.org/sdr/DXTA2013111205562.md): Engine · malfunctioned · Nov 11, 2013 · N313QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > APPROXIMATELY 20 MIN INTO FLIGHT AT FL430, CREW NOTICED A HOT SMELL. 5 MINUTES LATER A WHITE GRAY SMOKE ENTERED THE COCKPIT & CABIN. THE PRESS SOURCE SELECT KNOB WAS SELECTED TO L IAW ENVIRONMENTAL SMOKE CHECKLIST. SMOKE DISSIPATED DURING DESCENT & LANDING
- [SDR DXTA2013100705531](https://openairdocs.org/sdr/DXTA2013100705531.md): Engine · odor · Oct 7, 2013 · N313QS · Cessna 680CE · Engine (Turbine/Turboprop)
  > SMOKE IN CABIN AT FL 430. DURING CLIMBOUT ABOUT 14,000 APU SYS FAIL ANNUNCIATOR CAME ON AND APU SHUTDOWN. APU GEN HAD BEEN OFF, BUT BLEED AIR ON. APPROX 30 MINUTES LATER, LEVEL AT FL 430 ADVISED OF A LITTLE SMOKY IN CABIN. FINE GREY ENVIRONMENTAL SMOKE/HAZE
- [SDR DXTA2013053105404](https://openairdocs.org/sdr/DXTA2013053105404.md): Bearing · dirty · May 30, 2013 · N313QS · Cessna 680CE · Wheel/Ski/Float
  > NOSE GEAR MADE LOUD BANGING NOISE UPON GEAR RETRACTION, SHOOK GLARE SHIELD. NOSE STRUT WITHIN LIMITS RETRACTION GUIDES SEEM TO ALIGNED CORRECTLY. CYCLED GEAR, UNABLE TO DUPLICATE. CHECKED SERVICE OF NOSE STRUT FOUND LOWER CHAMBER TO BE LOWER AT 15 PSI.
- [SDR DXTA2013051305392](https://openairdocs.org/sdr/DXTA2013051305392.md): Coalescer Bag · dirty · May 12, 2013 · N313QS · Cessna 680CE · Humidity Control System
  > GETTING AN INTERMITTENT ACRID "DIRTY SOCK" ODOR IN CABIN DURING FLIGHT WITH APU OFF. R & R THE WATER SEPARATOR COALESCER IAW MM 21-21-03, 21-50-00. THE OPS AND LEAK CHECKS ARE SATISFACTORY. THERE WAS NO EVIDENCE OR ANY OIL IN THE WATER SEPARATOR.
- [SDR DXTA2011092304734](https://openairdocs.org/sdr/DXTA2011092304734.md): Ecu · failed · Sep 22, 2011 · N313QS · Cessna 680CE · Cabin Cooling System
  > UPON CLIMBING TO CRUISE ALTITUDE, BRIEF ODOR OF "HEAT" WAS NOTED IN THE COCKPIT. FOLLOWED LATER BY THE PASSENGERS WHO ALERTED THE CREW TO WHITE SMOKE COMING FROM BACK OF THE CABIN. A DIVERSION WAS DECLARED AND UPON REDUCTION OF POWER, SMOKE SOMEWHAT ABBATED
- [SDR 2011FA0000090](https://openairdocs.org/sdr/2011FA0000090.md): Connector · damaged · Jan 11, 2011 · N313QS · Cessna 680CE · Fuel System Wiring
  > WHILE PERFORMING THE 2B INTERNAL WING INSP, FOUND THAT THE LT AND RT ELECTRICAL CONNECTOR BLANKING PINS WERE FALLING OUT BECOMING FOD IN THE CTR FUEL TANK. CONNECOTRS ARE LOCATED IN FUEL ACCESS PANELS 175AB AND 176AB, ON THE FWD WALL.

Next page: https://openairdocs.org/aircraft/N313QS/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 = 'N313QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N313QS/reports

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