# Service difficulty reports: N323QS

A list on [N323QS](https://openairdocs.org/aircraft/N323QS.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 · 69 reports

- [SDR DXTA2026062308517](https://openairdocs.org/sdr/DXTA2026062308517.md): Engine · making metal · Jun 20, 2026 · N323QS · Cessna 680SOV · Engine (Turbine/Turboprop)
  > ENROUTE AT FL410, RT ENG OIL PRESSURE BEGAN SLOWLY DECAYING UNTIL OIL PRESSURE LOW RT CAS ILLUM, FOLLOWED BY A ENG VIBRATION RT CAS. SUBSEQUENTLY SHUT DOWN RT ENG IAW QRH & DIVERTED TO KAPA. CHIP DETECTOR. METAL, SLUDGE & COKE PRESENT. LP & HP ROTATE FREELY
- [SDR DXTA2026052608183](https://openairdocs.org/sdr/DXTA2026052608183.md): Brake · faulted · May 21, 2026 · N323QS · Cessna 680SOV · Landing Gear Brake System
  > AFTER TOUCHDOWN WHEN APPLYING BRAKES GRADUALLY BETWEEN 70 AND 80KTS THE LEFT MAIN BRAKE STARTS GRABBING AND SHIMMERING NOTICEABLY. WHEN BELOW ANTI SKID SPEED NO GRABBING NOR SHIMMERING IS OCCURRING. INSPECTED LT INBD AND OTBD BRAKE, WHEEL ASSEMBLIES AND SUR
- [SDR JGVR20250926001](https://openairdocs.org/sdr/JGVR20250926001.md): Skin · damaged · Sep 26, 2025 · N323QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > MECHANICALLY BLENDED 8 AREAS ON RT H-STAB LOWER SKIN ON THE AFT EDGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOP COATED AREAS PER NETJETS REQUEST FOR TECHNICAL DISPOSITION REPORT.
- [SDR DXTA2025062704035](https://openairdocs.org/sdr/DXTA2025062704035.md): Battery Pack · unserviceable · Jun 24, 2025 · N323QS · Cessna 680SOV · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS IN THE CABIN AND EXTERIOR NOT ILLUMINATING WHEN EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. RAN APU FOR 45 MINUTES TO CHARGE BATTERY PACKS, WITH NO SUCCESS. REMOVED # 1 EMERGENCY BATTERY, REMOVED #1 EMERGENCY BATTERY, INSTALLED REP
- [SDR DXTA2025040202863](https://openairdocs.org/sdr/DXTA2025040202863.md): Battery · inoperative · Mar 30, 2025 · N323QS · Cessna 680SOV · Emergency Lighting
  > FORWARD CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITION. AFT CABIN EMERGENCY LIGHTS DO ILLUMINATE. CORRECTIVE ACTION: TROUBLESHOT EMERGENCY LIGHTING SYSTEM AND VERIFIED THAT THE CABIN DOOR EXIT LIGHT AND FWD RH WORK SURFACE LIGHT W
- [SDR 2025F00077](https://openairdocs.org/sdr/2025F00077.md): Nut Plate · corroded · Mar 25, 2025 · N323QS · Cessna 680A · Passenger/Crew Doors
  > FOUND 8 NUTPLATES WITH CORROSION LOCATED INSIDE OF PANEL 154BC. NUT PLATES HOLD ON THE MED SPADE DOOR. REMOVED EXISTING MED SPADE DOOR AND 8 NUTPLATES FOR ACCESS. MECHANICALLY BLENDED AREAS OF CORROSION IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYON
- [SDR JGVR20250324001](https://openairdocs.org/sdr/JGVR20250324001.md): Skin · corroded · Mar 24, 2025 · N323QS · Cessna 680CE · Emergency Exits
  > FOUND THE EMERGENCY EXIT DOOR CORRODED OUTER SKIN ALONG CONTOUR RING EDGE AREA, REMOVED CONTOUR RINGS AND FOUND ADDITIONAL AREAS OF CORROSION. SENT DOOR OUT FOR REPAIRS. NOTE: EMERGENCY EXIT DOOR P/N 6911251-4.
- [SDR 2025F00075](https://openairdocs.org/sdr/2025F00075.md): Spar · corroded · Mar 21, 2025 · N323QS · Cessna 680A · Wing Spar
  > MECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED IN LH MLG WHEEL WELL, AFT SPAR, LOWER CLIP IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 EXCEEDING.002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLENDS IAW
- [SDR 2025F00073](https://openairdocs.org/sdr/2025F00073.md): Spar · corroded · Mar 21, 2025 · N323QS · Cessna 680A · Wing Spar
  > MECHANICALLY REMOVED 2 AREAS OF CORROSION FROM RH WING AFT SPAR, FWD FACE IN RH MLG WHEEL WELL. EVALUATED AND FOUND BLENDED AREAS WERE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02 EXCEEDING.002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLEN
- [SDR 2025F00072](https://openairdocs.org/sdr/2025F00072.md): Lug · corroded · Mar 21, 2025 · N323QS · Cessna 680A · Trailing Edge Flaps
  > REMOVED RH MIDDLE FLAP ASSEMBLY TO WORK CORROSION ON FWD, OUTBD LUG. MECHANICALLY REMOVED RH MIDDLE FLAP ROLLER, OUTBD LUG CORROSION, INBD SURFACE IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING.002" OF MATERI
- [SDR 2025F00074](https://openairdocs.org/sdr/2025F00074.md): Tail Cone · corroded · Mar 21, 2025 · N323QS · Cessna 680A · Aerodynamic Fairings
  > MECHANICALLY REMOVED 4 AREAS OF CORROSION LOCATED ON TAILCONE SERVICE DOOR FRAME ASSEMBLY WITH ADDITIONAL 4 AREAS OF CORROSION AFTER FRAME ASSEMBLY WAS REMOVED IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING.
- [SDR JGVR20250320007](https://openairdocs.org/sdr/JGVR20250320007.md): Skin · corroded · Mar 20, 2025 · N323QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > REPAIRED 2 AREAS OF CORROSION LOCATED ON LH HORIZONTAL STABILIZER UPPER SKIN FORWARD OF PANEL 351AC, BY BLENDING CORROSION, PERFORMING NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS ENGINEERING ORDER BY CLEANING, TREATING, AND PRIMING ARE
- [SDR JGVR20250320006](https://openairdocs.org/sdr/JGVR20250320006.md): Skin · corroded · Mar 20, 2025 · N323QS · Cessna 680CE · Wing, Plate/Skin
  > REPAIRED THE LH UPPER WING SKIN LOCATED UNDER AND ADJACENT TO THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING STRUCTURE) BY BLENDING CORROSION, PERFORMING NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER TEXTRON FIELD REPAIR BY CLEANING, TREATING, AND
- [SDR JGVR20250320005](https://openairdocs.org/sdr/JGVR20250320005.md): Stringer · corroded · Mar 20, 2025 · N323QS · Cessna 680CE · Fuselage Main, Longeron/Stringer
  > MECHANICALLY BLENDED CORROSION FROM CORROSION FROM CENTER STRINGER UNDER PANELS 154AC AND 154BC, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250320004](https://openairdocs.org/sdr/JGVR20250320004.md): Skin · corroded · Mar 20, 2025 · N323QS · Cessna 680CE · Wing, Plate/Skin
  > MECHANICALLY BLENDED CORROSION FROM LH OVER-WING FUEL ADAPTER LAND., PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250320003](https://openairdocs.org/sdr/JGVR20250320003.md): Skin · corroded · Mar 20, 2025 · N323QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > REMOVED NUT PLATES FROM PANELS LANDS TO ACCESS CORROSION AND MECHANICALLY REMOVED ALL AREAS OF CORROSION BEHIND VERTICAL STABILIZER PANELS 341ER, 341DR, 341CR, 341BR, AND 341AR, 341AL, 341BL, 341CL, AND 341DL, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION
- [SDR JGVR20250320002](https://openairdocs.org/sdr/JGVR20250320002.md): Skin · corroded · Mar 20, 2025 · N323QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > BLENDED AREAS OF CORROSION LOCATED ON UPPER EXTERIOR FUSELAGE SKIN IN ZONE 254, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250320001](https://openairdocs.org/sdr/JGVR20250320001.md): Skin · corroded · Mar 20, 2025 · N323QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > BLENDED 5 AREAS OF CORROSION LOCATED ON EXTERIOR FUSELAGE SKIN ALONG THE SEAM NEXT TO THE PILOT DV WINDOW IN ZONE 243 ALONG SEAM, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING,
- [SDR 2025F00059](https://openairdocs.org/sdr/2025F00059.md): Spar · corroded · Mar 13, 2025 · N323QS · Cessna 680A · Wing Spar
  > MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON RH GEARWELL AFT SPAR, FWD FACE, LOWER CLIP, INBD OF WS 37.00 IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 LIMITATIONS EXCEEDING.002" OF MATERIAL REMOVED FROM NOMINAL
- [SDR JGVR20250306003](https://openairdocs.org/sdr/JGVR20250306003.md): Lug · corroded · Mar 6, 2025 · N323QS · Cessna 680CE · Wing, Control Surface Attach Fittings
  > BLENDED CORRODED AREAS FROM THE OUTBOARD ROLLER LUG OF THE RH WING MIDDLE FLAP, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250306002](https://openairdocs.org/sdr/JGVR20250306002.md): Skin · corroded · Mar 6, 2025 · N323QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED CORRODED AREA ON THE RH UPPER WING SKIN, JUST AFT OF THE LEADING EDGE AND OUTBOARD OF THE WING WALK, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING
- [SDR JGVR20250306001](https://openairdocs.org/sdr/JGVR20250306001.md): Skin · corroded · Mar 6, 2025 · N323QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED 6 AREAS OF CORROSION ON THE RH LOWER OUTBOARD WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250303006](https://openairdocs.org/sdr/JGVR20250303006.md): Skin · corroded · Mar 3, 2025 · N323QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED 6 AREAS OF CORROSION ON LH UPPER WING (INBOARD WING) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250303005](https://openairdocs.org/sdr/JGVR20250303005.md): Skin · corroded · Mar 3, 2025 · N323QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED 15 AREAS OF CORROSION ON LH UPPER WING IN ZONES 551 AND 552 (OUTBOARD WING) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250303004](https://openairdocs.org/sdr/JGVR20250303004.md): Structure · corroded · Mar 3, 2025 · N323QS · Cessna 680CE · Wing Structure
  > BLENDED ONE AREA OF CORROSION FROM LH LOWER WING FORWARD OF THE AILERON, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250303003](https://openairdocs.org/sdr/JGVR20250303003.md): Structure · corroded · Mar 3, 2025 · N323QS · Cessna 680CE · Wing Structure
  > MECHANICALLY REMOVED CORROSION LOCATED AROUND LH OVERWING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER TEXTRON REPAIR MEMO BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR JGVR20250303002](https://openairdocs.org/sdr/JGVR20250303002.md): Rib · corroded · Mar 3, 2025 · N323QS · Cessna 680CE · Wing Structure
  > REMOVED EMERGENCY BRAKE LINES AND CARRY THROUGH FITTINGS FROM RH AND LH RIBS AT WS 37, BLENDED CORRODED AREAS, PERFORMED, NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIM
- [SDR JGVR20250303001](https://openairdocs.org/sdr/JGVR20250303001.md): Structure · corroded · Mar 3, 2025 · N323QS · Cessna 680CE · Wing Structure
  > MECHANICALLY REMOVED CORROSION LOCATED AROUND RH OVERWING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAID AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.
- [SDR DXTA2025010701863](https://openairdocs.org/sdr/DXTA2025010701863.md): Battery · no test · Jan 6, 2025 · N323QS · Cessna 680SOV · Emergency Lighting
  > FAILED TO TEST ON PREFLIGHT. LIGHTS DO NOT ILLUMINATE IN ARM POSITION. LIGHTS FUNCTION NORMALLY WHEN SELECTED ON. PERFORMED EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. OPS CHECK GOOD. IAW TC-FLT-33-1001.
- [SDR DXTA2024100100707](https://openairdocs.org/sdr/DXTA2024100100707.md): Precatch · out of rig · Sep 29, 2024 · N323QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR PRE CATCH NOT FLUSH WITH PANEL. ON LAST LEG DOOR WOULD NOT CATCH. CORRECTIVE ACTION: EVALUATED THE PRECHATCH SYSTE. SYSTEM IS COMPLETELY FUNCTIONAL 5/5 CHECKS SATISFACTORY. HANDLE DOES NOT SIT FLUSH AS REPORTED. FROM EVALUATION IT LOOKS AS IF THE H
- [SDR DXTA2024080600117](https://openairdocs.org/sdr/DXTA2024080600117.md): Door · excess play · Aug 6, 2024 · N323QS · Cessna 680SOV · Passenger/Crew Doors
  > THE MAIN CABIN DOOR HAS APPROXIMATELY TWO TO THREE INCHES OF PLAY IN IT WHEN IT IS FULLY DOWN AND LOCKED. FOUND THE OVER CENTER PUSHROD LOOSE. RESECURED THE PUSHROD AND OPERATED THE DOOR SEVERAL TIMES AND FOUND IT SATISFACTORY. WORK DONE IAW CE-680 AMM 51-1
- [SDR 2023FA0000598](https://openairdocs.org/sdr/2023FA0000598.md): Spar Cap · corroded · Oct 12, 2023 · N323QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > NJA CORROSION FOUND ON LEFT-AFT-VERTICAL-STAB SPAR CAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING MEMO DQ41418M1 DATED 10/5/2023.
- [SDR DXTA2023081492850](https://openairdocs.org/sdr/DXTA2023081492850.md): Unknown · unknown · Aug 11, 2023 · N323QS · Cessna 680CE · Airborne Auxiliary Power Unit (APU) System
  > APU (EXCEPT GENERATOR): IN FLIGHT AT 25,000FT WITH APU ON WITH MAX AIR SELECTED, A STRONG ODOR IN CABIN. TURNED APU OFF AND ODOR VERY SLOWLY DISSIPATED. ODOR DID NOT SMELL ELECTRICAL OR OILY. COMPUED WITH NJA TASK CARDS, THE COALESCER WAS A LLTTLE DIRTY •
- [SDR JGVR20210520006](https://openairdocs.org/sdr/JGVR20210520006.md): Spar · corroded · May 20, 2021 · N323QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > MECHANICALLY REMOVED CORROSION LOCATED ON VERTICAL STAB, AFT SPAR, LH SPAR CLIP JUST BELOW LOWER CROSS MEMBER. FOUND CORROSION EXCEEDING C680 SRM 51-70-02 LIMITATIONS AND SUBMITTED TO TEXTRON ENGINEERING FOR REPAIRS. REPAIRED CORROSION IAW TEXTRON ENGINEERING
- [SDR JGVR20210520005](https://openairdocs.org/sdr/JGVR20210520005.md): Skin · corroded · May 20, 2021 · N323QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > BLENDED 2 AREAS OF CORROSION ON UPPER AFT EDGE OF RH VERTICAL STAB SKIN. FOUND CORROSION REMOVED TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02. REPAIR CORROSION PER TEXTRON REPAIR MEMO DQ29966M1, SUBJECT "RIGHT-HAND VERTICAL STABILIZER SKIN CORROSION", DATED
- [SDR JGVR20210520004](https://openairdocs.org/sdr/JGVR20210520004.md): Skin · corroded · May 20, 2021 · N323QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > BLENDED CORROSION ON LOWER FUSELAGE SKIN AROUND TCAS ANTENNA CARRY THRU CONNECTORS. FOUND CORROSION TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02. REPAIRED CORROSION ON LOWER FUSELAGE SKIN AROUND TCAS ANTENNA CARRY THRU CONNECTOR PER TEXTRON REPAIR MEMO DQ 2
- [SDR JGVR20210520003](https://openairdocs.org/sdr/JGVR20210520003.md): Skin · corroded · May 20, 2021 · N323QS · Cessna 680CE · Wing, Plate/Skin
  > FOUND CORROSION GOING UNDER RH WING AFT DRAG ANGLE. FOUND ADDITIONAL 80 AREAS OF CORROSION UNDER DRAG ANGLE. MECHANICALLY REMOVED 94 AREAS OF CORROSION FROM RH WING AFT DRAG ANGLE AREA IAW CESSNA 680 SRM 51-70-02. EVALUATED REMAINING THICKNESS AND FOUND TO BE
- [SDR JGVR20210520002](https://openairdocs.org/sdr/JGVR20210520002.md): Spar · corroded · May 20, 2021 · N323QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > MECHANICALLY BLENDED CORROSION FROM RUDDER COVE ON VERTICAL STAB AFT SPAR RH CLIP IAW CESSNA 680 SRM 51-70-02. REFER TO SQK 103-2 OF THIS WO FOR NDT. EVALUATED REMAINING THICKNESS AND FOUND TO BE OUT OF LIMITS. SUBMITTED INFO TO ENGINEERING. COMPLIED WITH TEXT
- [SDR JGVR20210520001](https://openairdocs.org/sdr/JGVR20210520001.md): Torque Tube · cracked · May 20, 2021 · N323QS · Cessna 680CE · Rudder Structure
  > REMOVED CRACKED RUDDER TORQUE TUBE P/N UNKNOWN FROM RUDDER P/N 6933000-19 S/N 0134 AND INSTALLED NEW CUSTOMER SUPPLIED RUDDER TORQUE TUBE P/N 6933025-55 PER CESSNA 680 SRM 51-40-03, 51-40-06, 55-40-09, CSPM 20-40-20.
- [SDR JGVR20210113001](https://openairdocs.org/sdr/JGVR20210113001.md): Panel · corroded · Jan 13, 2021 · N323QS · Cessna 680A · Horizontal Stabilizer, Plate/Skin
  > BLENDED 1 AREA OF CORROSION ON TOP OF LT HORIZONTAL STAB JUST FORWARD OF WEDGE PANEL 351AC (INBOARD OF THE LT ELEVATOR) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED PER TEXTRON ENGINEERING MEMO.
- [SDR DXTA2020092004111](https://openairdocs.org/sdr/DXTA2020092004111.md): Spring · broken · Sep 20, 2020 · N323QS · Cessna 680A · Passenger/Crew Doors
  > MAIN CABIN DOOR HEAVY TO CLOSE. CABIN DOOR MAKES NUMEROUS CREAKING NOISES AS IT CLOSES. REMOVED AND REPLACED BOTH LUBRICATED SPRINGS DUE TO BROKEN AND CRACKED SPRINGS. RIGGED CABLE TENSIONS, OPERATIONS CHECK GOOD, DOOR CLOSES MUCH EASIER. ALL WORK DONE, IA
- [SDR DXTA2020081413965](https://openairdocs.org/sdr/DXTA2020081413965.md): Element · damaged · Aug 11, 2020 · N323QS · Cessna 680CE · Air Conditioning System
  > SHORT FINAL GOING TO EGE AIRPORT. APROX 8000 FT. EMERGENCY PRESS, ACM BLEED LEAK, BAGGAGE HEAT FAIL AND POSSIBLE ACM OVER TEMP MESSAGE COME ON AND WENT OUT. ELECTRICAL BURNING SMELL, WAS NOTICED SHORTLY AFTER. LANDED UN EVENTFULLY. RAN CHECK LIST FOR ACM B
- [SDR DXTA2020081213965](https://openairdocs.org/sdr/DXTA2020081213965.md): Warning System · multiple fail · Aug 11, 2020 · N323QS · Cessna 680CE · Central Warning
  > SHORT FINAL GOING TO AIRPORT. APROX 8000 FT. EMERGENCY PRESS, ACM BLEED LEAK, BAGGAGE HEAT FAIL AND POSSIBLE ACM OVER TEMP MESSAGE COME ON AND WENT OUT. ELECTRICAL BURNING SMELL, WAS NOTICED SHORTLY AFTER. LANDED UN EVENTFULLY. RAN CHECK LIST FOR ACM BLEED
- [SDR JGVR20200807003](https://openairdocs.org/sdr/JGVR20200807003.md): Hinge Bracket · corroded · Aug 7, 2020 · N323QS · Cessna 680CE · Rudder Structure
  > BLENDED CORRODED AREA ON THE LOWER HINGE BRACKET OF THE MIDDLE RUDDER HINGE ON THE VERTICAL STABILIZER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED CORRODED PART WITH NEW HINGE PLATE P/N 6931050-60 PER CESSNA 680 SRM 51-40-03, 51-40-06, 51-40-0
- [SDR JGVR20200807002](https://openairdocs.org/sdr/JGVR20200807002.md): Spar Cap · corroded · Aug 7, 2020 · N323QS · Cessna 680CE · Horizontal Stabilizer, Spar/Rib
  > BLENDED, PERFORMED NDT AND TREATED CORRODED AREAS ON THE LH HORIZONTAL STABILIZER SPAR CAP IAW REPAIR MEMO.
- [SDR JGVR202008070001](https://openairdocs.org/sdr/JGVR202008070001.md): Spar Cap · corroded · Aug 7, 2020 · N323QS · Cessna 680CE · Wing Spar
  > BLENDED, PERFORMED NDT AND TREATED CORRODED AREAS ON THE LT WING AFT SPAR LOWER CAP, LOCATED BEHIND ACCESS PANEL 730DL, IAW REPAIR MEMO.
- [SDR DXTA2019021200010](https://openairdocs.org/sdr/DXTA2019021200010.md): Drain · leaking · Feb 11, 2019 · N323QS · Cessna 680A · Hydraulic System, Main
  > 1) HYDRAULIC FLUID LEAK - COMPLETE LEFT AND RIGHT HYDRAULIC FLUID LOSS OCCURRED AFTER TAKEOFF WITH GEAR RETRACTED. POSTFLIGHT REVEALED HYDRAULIC FLUID COMING FROM RIGHT ENGINE DRAIN MAST. NO HYDRAULIC FLUID VISIBLE AROUND LEFT OR RIGHT MAIN LANDING GEAR. 2)
- [SDR DXTA2018080301257](https://openairdocs.org/sdr/DXTA2018080301257.md): Control Unit · malfunctioned · Aug 2, 2018 · N323QS · Cessna 680SOV · Landing Gear Steering System
  > RAISED LANDING GEAR AND THE NOSE GEAR DID NOT RETRACT, AS INDICATED BY A GREEN NOSE GEAR LIGHT, THE RED UNLOCK LIGHT, AND AERODYNAMIC NOISE WITH THE GEAR HANDLE SELECTED UP. WE CYCLED THE GEAR AND IT EXTENDED AND RETRACTED NORMALLY. GEAR EXTENSION FOR LANDING
- [SDR DXTA2018060801053](https://openairdocs.org/sdr/DXTA2018060801053.md): Shutoff Valve · failed · Jun 7, 2018 · N323QS · Cessna 680CE · Cabin Cooling System
  > CLIMBING THROUGH FL400, AN ODOR WAS NOTICED BY CREW, FOLLOWED BY VISUAL SMOKE IN BOTH THE CABIN AND COCKPIT. SHORTLY AFTER, TWO AMBER CAS MESSAGES FOR ACM OVERTEMP AND EMERGENCY PRESSURIZATION ILLUMINATED. EMERGENCY DESCENT WAS ACCOMPLISHED ALONG WITH COMPLIA
- [SDR DXTA2018022800072](https://openairdocs.org/sdr/DXTA2018022800072.md): Frame · cracked · Feb 28, 2018 · N323QS · Cessna 680SOV · Fuselage Main, Frame
  > NLG FRAME CRACK. ACCOMPLISHED ENGINEERING LETTER DQ11281M1 DATED FEB 23, 2018, 680-0134 NLG RIGHT SIDE FRAME (P/N 6713072-31) CRACK.

Next page: https://openairdocs.org/aircraft/N323QS/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 = 'N323QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N323QS/reports

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