# Service difficulty reports: N341QS

A list on [N341QS](https://openairdocs.org/aircraft/N341QS.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 · 59 reports

- [SDR DXTA2026010506406](https://openairdocs.org/sdr/DXTA2026010506406.md): Wing · ground damage · Jan 2, 2026 · N341QS · Cessna 680SOV · Wing Main, Frame Structure
  > JUST AS WE GOT TO THE AIRPORT AND BEFORE WE GOT TO THE PLANE A EXECUJET VAN STRUCK THE LEFT WING OF N341QS AT 8:56. THE DAMAGE TO THE WING SEEMS MINIMAL BUT THE VAN HAS A BIG DENT. CORRECTIVE ACTION: GAINED ACCESS TO THE AIRCRAFT AND INSPECTED THE DAMAGED AREA
- [SDR DXTA2025120806024](https://openairdocs.org/sdr/DXTA2025120806024.md): Power Supply · inoperative · Dec 7, 2025 · N341QS · Cessna 680SOV · Emergency Lighting
  > DURING PREFLIGHT FOUND ALL BUT TWO EMERGENCY LIGHTS INOPERATIVE. THE ONLY TWO THAT WORK ARE THE CABIN FLOOR FWD LT & EXTERIOR LIGHT BY THE CABIN DOOR. REMOVED NR 1 EMERGENCY LIGHT POWER SUPPLY & REPLACED WITH NEW EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-10.
- [SDR 2025FA0000724](https://openairdocs.org/sdr/2025FA0000724.md): Spar Cap · corroded · Oct 18, 2025 · N341QS · Cessna 680CE · Wing Spar
  > CORROSION FOUND IN RT WHEEL WELL ON LOWER AFT SPAR CAP. ACCOMPLISHED FORM 8100-9, FIELD REPAIR FR-680-0225-15874 FIELD REPAIR-CORROSION, RT WING REAR SPAR CAP LOWER FORWARD ANGLE RWS 37.
- [SDR DXTA2025051403445](https://openairdocs.org/sdr/DXTA2025051403445.md): Door · malfunctioned · May 11, 2025 · N341QS · Cessna 680SOV · Passenger/Crew Doors
  > PRIMARY CABIN DOOR WOULD NOT OPEN AFTER LANDING. RED BUTTON WOULD NOT DEPRESS TO OPEN THE DOOR. ATTEMPTED TO HAVE GROUND CREW OPEN THE DOOR FROM THE OUTSIDE. THEY WERE UNABLE TO¿ AND THE SILVER HANDLE ON THE EXTERIOR PART THE DOOR JAMMED INWARD. ATTEMPTED TO
- [SDR DXTA2025041403069](https://openairdocs.org/sdr/DXTA2025041403069.md): Cabin Pressure · malfunctioned · Apr 12, 2025 · N341QS · Cessna 680SOV · Cabin Pressure Control System
  > OVERWEIGHT LANDING: LANDED AT APPROXIMATELY 28,100 POUNDS DUE TO PRESSURIZATION EMERGENCY WITH PASSENGERS. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSPECTION IAW CE-680 AMM 05-50-00. OPS CHECK GOOD.
- [SDR DXTA2025041403068](https://openairdocs.org/sdr/DXTA2025041403068.md): Coupling · out of position · Apr 12, 2025 · N341QS · Cessna 680SOV · Humidity Control System
  > CABIN PRESSURIZATION CONTROL: DURING CLIMBOUT, WE NOTICED A FLUTTERING/POPPING NOISE FROM ABOUT 1000 MSL TO ABOUT 2000 MSL. IT STOPPED. THEN WE NOTICED THAT THE CABIN WASNT PRESSURIZING AS QUICKLY AS NORMAL. CABIN ALTITUDE WAS ABOUT 4000 CLINBING THROUGH 14,00
- [SDR DXTA2025040102859](https://openairdocs.org/sdr/DXTA2025040102859.md): Control Valve · leaking · Mar 29, 2025 · N341QS · Cessna 680SOV · Main Landing Gear
  > AFTER A NORMAL LANDING IN HOU, A LINEMAN NOTICED OUR RIGHT MLG TRUCK SMOKING WITH A VERY DISTINCT CRACKLING SOUND (ALMOST THE SOUND OF A WOOD LOG BURNING IN A FIRE). THERE WAS ALSO THE SMELL OF BURNING HYDRAULIC FLUID. AFTER,PERFORMED DETAILED INSPECTION OF R
- [SDR 2025FA0000214](https://openairdocs.org/sdr/2025FA0000214.md): Spar · corroded · Mar 27, 2025 · N341QS · Cessna 680CE · Wing Spar
  > DURING WING AFT SPAR INSPECTION, FOUND CORROSION AROUND HYDRAULIC FITTINGS ON LH AFT SPAR. DURING BLENDING OF LH WING SPAR FOUND CORROSION UNDER ADDITIONAL FEED THROUGH. DURING ULTRASONIC THICKNESS INSPECTION OF A BLENDED AREA NEAR A FASTENER HOLE ON THE LH AF
- [SDR 2025FA0000213](https://openairdocs.org/sdr/2025FA0000213.md): Spar · corroded · Mar 27, 2025 · N341QS · Cessna 680CE · Wing Spar
  > DURING LH AND RH WING AFT SPAR INSPECTION FOUND CORROSION AROUND SPEED BRAKE HYDRAULIC FITTING AND SP HYDRAULIC FITTING ON RH WING. PERFORMED REPAIR TO RH WING SPAR WEB CORROSION. PER: NETJETS RFTS-112900 N341QS (680-0225) RH WING SPAR WEB CORROSION, REV.0 DAT
- [SDR 2025FA0000183](https://openairdocs.org/sdr/2025FA0000183.md): Spar Web · corroded · Mar 13, 2025 · N341QS · Cessna 680CE · Wing Spar
  > LH WING AFT SPAR WEB CORROSION.
- [SDR 2025FA0000182](https://openairdocs.org/sdr/2025FA0000182.md): Closeout Panel · corroded · Mar 13, 2025 · N341QS · Cessna 680CE · Passenger/Crew Doors
  > MED LOWER CLOSEOUT PANEL CORROSION AND GOUGING.
- [SDR 2025FA0000120](https://openairdocs.org/sdr/2025FA0000120.md): Tail Cone · corroded · Feb 19, 2025 · N341QS · Cessna 680CE · Aerodynamic Fairings
  > TAIL CONE HAS CORROSION SURROUNDING LOWER DATA PLATE.
- [SDR DXTA2024110401000](https://openairdocs.org/sdr/DXTA2024110401000.md): Shroud · damaged · Oct 30, 2024 · N341QS · Cessna 680SOV · Fuselage Miscellaneous Structure
  > ON TAKEOFF CLIMB OUT, APPROXIMATELY 500 FEET AGL A TURKEY VULTURE IMPACTED THE FRONT LEFT WINDSHIELD CRUSHING THE WINDSHIELD AIR VENT DUCTING. NO STRUCTURAL DAMAGE WAS OBSERVED ON THE LEFT CAPTAIN SIDE WINDSHIELD. AIRCRAFT ENTERED THE TRAFFIC PATTERN AND RETUR
- [SDR DXTA2024040211373](https://openairdocs.org/sdr/DXTA2024040211373.md): Cable · low tension · Mar 31, 2024 · N341QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR NOT BALANCED AND OPENS VERY VIOLENTLY. VERY HEAVY/DIFFICULT TO CLOSE. TECH PERFORMED THE COUNTERBALANCE ADJUSTMENT/TECH AND FOUND THE TENSION ON THE CABLES WERE CAUSING THE DOOR TO SLAM DOWN. TIGHTEN THE TENSION OF TME CABLES AND PE
- [SDR DXTA2024030811126](https://openairdocs.org/sdr/DXTA2024030811126.md): Spring · faulty · Mar 6, 2024 · N341QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR CABLE IS LOOSE INSIDE DOOR. CABLE IS ATTACHED, BUT SLACK. INSPECTED CABIN DOOR AND FOUND AFT DOOR COUNTERBALANCE SPRING BROKEN. REMOVED AND REPLACED CABIN DOOR AFT COUNTERBALANCE SPRING WITH A CUSTOMER SUPPLIED NEW PART. PERFORMED RIGGING PROCEDURE
- [SDR DXTA2024022811004](https://openairdocs.org/sdr/DXTA2024022811004.md): Spring · damaged · Feb 25, 2024 · N341QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR CABLE: LEFT SIDE MAIN CABIN DOOR COUNTER BALANCE CABLE WILL NOT RETRACT AND UNABLE CLOSE DOOR FROM INSIDE THE AIRCRAFT. REMOVED MAIN ENTRY DOOR STAIRS, FOUND FORWARD DOOR SPRING BROKEN, NO OTHER DAMAGE NOTED, PUT SPRING AND SOME SCREWS ON ORDER. (JP
- [SDR DXTA2023113010191](https://openairdocs.org/sdr/DXTA2023113010191.md): Hinge · damaged · Nov 30, 2023 · N341QS · Cessna 680SOV · Fuselage, Door Hinge
  > OPENING THE MAIN CABIN DOOR, AFTER LANDING, BITS OF THE MAIN HINGE BROKE OFF. TECHS WERE UNABLE TO REMOVE THE DAMAGED HINGE HALF AS THE HINGE PIN IS FULLY SEIZED. REMOVED SUPPORT BRACKET & INSTALLED NEW SUPPORT BRACKET REMOVED DAMAGED HINGE HALF & INSTALLED
- [SDR 2023FA0000698](https://openairdocs.org/sdr/2023FA0000698.md): Spar Cap · corroded · Oct 29, 2023 · N341QS · Cessna 680CE · Vertical Stabilizer
  > FIELD REPAIR - CORROSION, VERTICAL STABILIZER, AFT SPAR CAP VFS 174.85 - VFS 238.39. REPORT NO. FR-680-0225-12507 DATED OCTOBER 12, 2023 WITH FAA FORM 8100-9.
- [SDR DXTA2023062689410](https://openairdocs.org/sdr/DXTA2023062689410.md): Unknown · unknown · Jun 26, 2023 · N341QS · Cessna 680SOV · AC Generation System
  > AC GENERATION AND CONTROL: SLIGHT ELECTRICAL SMOKE ODOR BEFORE TAKEOFF, FADED WHEN FACING DOWN RUNWAY. DURING TROUBLESHOOTING OF THE RH WINDSHIELD HEAT INOP CAS MESSAGE. WHILE REMOVING RH WINDSHIELD HEAT CONTROLLER, NOTED STRONG ELECTRICAL BURNING SMELL FRO
- [SDR DXTA2023060587810](https://openairdocs.org/sdr/DXTA2023060587810.md): Unknown · unknown · Jun 5, 2023 · N341QS · Cessna 680SOV · Emergency Lighting
  > EMER LIGHTS FAIL PREFLIGHT CHECK. WITH BATTERIES OFF AND EMERGENCY LIGHT SWITCH IN ARM, ZERO EMERGENCY LIGHTS TURN ON. WITH THE EMERGENCY LIGHT SWITCH ON, ALL EMERGENCY LIGHTS ILLUMINATE EXCEPT THE OVERHEAD WORK LIGHT AND THE EMERGENCY EXIT LIGHT ABOVE MAIN CA
- [SDR DXTA2023052486950](https://openairdocs.org/sdr/DXTA2023052486950.md): Battery · defective · May 23, 2023 · N341QS · Cessna 680CE · Emergency Lighting
  > CABIN EMERG LIGHT: OVERHEAD CABIN EMERGENCY LIGHTS ON LEFT SIDE, AND MAIN CABIN DOOR EXTERIOR EMERGENCY LIGHT DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. VERIFIED DISCREPANCY. CHARGED BATTERIES FOR ONE HOUR. FOUND ALL OTHER LIGHTS WORKING CORRECTLY, INSPEC
- [SDR DXTA2023051285940](https://openairdocs.org/sdr/DXTA2023051285940.md): Unknown · unknown · May 11, 2023 · N341QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTING: WITH THE EMERGENCY LIGHTS IN THE ON POSITION OR THE PAX, SAFETY LIGHT SWITCH ON ALL INTERIOR EMERGENCY SIGNS AND PAX SAFETY LIGHTS FORWARD OF SEATS FIVE AND SIX ARE INOPERATIVE. ALL EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. INTERMITTENT CA
- [SDR DXTA2022111573970](https://openairdocs.org/sdr/DXTA2022111573970.md): G Switch · tripped · Nov 14, 2022 · N341QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTING: CABIN EMER LIGHTS ASSOCIATED WITH BATTERY PACK ONE FOR FORWARD PORTION OF CABIN, ILLUMINATED ON THEIR OWN DURING CRUISE. LIGHTS STAYED ON REGARDLESS OF EMER LIGHT SWITCH POSITION: ON ARM, OR OFF. LIGHTS STAYED ON AFTER ENGINE SHUT DOWN, BAT
- [SDR DXTA2022102672790](https://openairdocs.org/sdr/DXTA2022102672790.md): Battery Pack · inoperative · Oct 25, 2022 · N341QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTING: CABIN, EXTERIOR, AND LAV EMERGENCY LIGHTS FAIL TO ILLUMINATE DURING PREFLIGHT CHECKS. PERFORMED EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE REV. 2 DATED 200CT2022. OPS CHECK GOOD IAW CE-680 AMM 33-50-10.
- [SDR DXTA2021071345190](https://openairdocs.org/sdr/DXTA2021071345190.md): Apu · smoke · Jul 12, 2021 · N341QS · Cessna 680CE · Airborne Auxiliary Power Unit (APU) System
  > SMOKE AND AND ODOR IN THE CABIN. APU AND BLEED AIR WERE ON, ENGINES OFF. INSPECTED THE APU EXHAUST FINDING NO OIL OR VISUAL ABNORMALITIES. STARTED THE APU IAW THE POH, RAN THE APU FOR 30 MINUTES WITH THE APU BLEED SELECTED ON WITH NO SMOKE OR ODOR NOTED. S
- [SDR DXTA2021032439900](https://openairdocs.org/sdr/DXTA2021032439900.md): Warning Message · false activation · Mar 23, 2021 · N341QS · Cessna 680CE · Door Warning System
  > MAIN DOOR: AMBER CABIN DOOR OPEN CAS MESSAGE WILL NOT CLEAR. WE HAD PLANE PLANE GO DARK. WE OPENED AND CLOSED DOOR 6X TIMES IN A ROW TO RESET, NO LUCK PERFORMED OPS CHECK OF DOOR WARNING SYSTEM IAW CE-680 MM 52-70-00 SEVERAL TIMES, EICAS MESSAGE CLEARED EV
- [SDR EBVR20200807001](https://openairdocs.org/sdr/EBVR20200807001.md): Structure · corroded · Aug 7, 2020 · N341QS · Cessna 680SOV · Fuselage Main, Structure
  > CORROSION FOUND AROUND THREE LOCK FASTENERS IN CENTER AFT CABIN FLOOR JUST FWD OF OUTFLOW VALVES, FOUND SEVERAL SPOTS OF CORROSION ON STRUCTURE UNDER THE CENTER DROP AISLE PANELS. FINAL REPAIR ERO-966682 REV IR AND 8110-3. VERTICAL REAR SPAR INSPECTION FOUND
- [SDR DXTA2019031302157](https://openairdocs.org/sdr/DXTA2019031302157.md): Printed Ckt Board · faulty · Mar 13, 2019 · N341QS · Cessna 680CE · Landing Gear Position and Warning
  > ALL LANDING GEAR RETRACTION DID NOT RETRACT-GEAR WOULDNT RETRACT AFTER TAKEOFF. AMBER CAS WOW MIS-COMPARE CAME ON SHORTLY AFTER. **SUPPLEMENTAL INFORMATION - REMOVED & REPLACED LT AFT PCB NZ106 SQUAT SWITCH ASSEMBLY.
- [SDR DXTA2018071800266](https://openairdocs.org/sdr/DXTA2018071800266.md): Spar Cap · corroded · Jul 18, 2018 · N341QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB AFT SPAR CAP DAMAGE, CORROSION.
- [SDR DXTA2018053001017](https://openairdocs.org/sdr/DXTA2018053001017.md): Unknown · odor · May 30, 2018 · N341QS · Cessna 680SOV · Air Distribution System
  > BURNING SMELL IN COCKPIT.
- [SDR 2017F00002](https://openairdocs.org/sdr/2017F00002.md): Skin · damaged · Jan 10, 2017 · N341QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIR OF AFT CABIN LIGHTNING STRIKE DAMAGE, S-680-0225/10RD REV-. DATED DECEMBER 20, 2016 WITH FAA FORM 8100-9.
- [SDR 2017F00001](https://openairdocs.org/sdr/2017F00001.md): Skin · damaged · Jan 5, 2017 · N341QS · Cessna 680SOV · Fuselage Main, Plate/Skin
  > REPAIR OF AFT CABIN LIGHTNING STRIKE DAMAGE.
- [SDR DXTA2016020206174](https://openairdocs.org/sdr/DXTA2016020206174.md): Apu · leaking · Feb 1, 2016 · N341QS · Cessna 680CE · APU Core Engine
  > AFTER APU BLEED AIR SELECTED ON, THERE WAS AN ODOR & HAZY SMOKE IN THE COCKPIT & CABIN. WITH ENGS RUNNING & APU BLEED AIR OFF THE ODOR & SMOKE DISSIPATED. REMOVED STARTER & GENERATOR COOLING DUCT FOUND OIL SOAKED. APU IS LEAKING INTERNALLY. REMOVED APU, PN
- [SDR DXTA2015005006014](https://openairdocs.org/sdr/DXTA2015005006014.md): Coalescer Bag · dirty · May 1, 2015 · N341QS · Cessna 680CE · Humidity Control System
  > WHEN APU STARTED & BLEED AIR VALVES OPENED, SMOKE BEGAN TO POUR OUT OF VENTS. SMOKE DISSIPATED WHEN APU BLEEDS CLOSED. WHEN ENG STARTED, NO SMOKE WAS OBSERVED. R & R COALESCER SOCK & COMPLIED WITH ENVIRONMENTAL CONTROL SYS, ECS, DUCT BURN OUT FORM IAW TC-68
- [SDR DXTA2013080505467](https://openairdocs.org/sdr/DXTA2013080505467.md): Brake · weak · Aug 4, 2013 · N341QS · Cessna 680CE · Landing Gear Brake System
  > CO-PILOT`S LT BRAKE SPONGY. ON LANDING ROLLOUT, BRAKES WERE APPLIED EVENLY AND ACFT VEERED TO RT AND LT PEDAL FELT SPONGY. BLED LT INBD AND OTBD BRAKES IAW MM 32-42-01, NOTED AIR IN INBD BRAKE. OPS CHECKED GOOD.
- [SDR DXTA2013052005397](https://openairdocs.org/sdr/DXTA2013052005397.md): Oil System · overserviced · May 18, 2013 · N341QS · Cessna 680CE · APU Oil System
  > WITH THE APU ONLY RUNNING, BLEED AIR WAS SELECTED ON. SMOKE IMMEDIATELY STARTED TO POUR INTO BOTH CABIN AND COCKPIT. SHUTDOWN APU WITHIN 15 SECONDS AND A CONSIDERABLE HAZE OF SMOKE REMAINED HANGING IN AIR. LOCATED OIL COMING FROM AGB VENT LINES OUT EXHAUST.
- [SDR CWQR20130501032](https://openairdocs.org/sdr/CWQR20130501032.md): Nozzle · cracked · May 1, 2013 · N341QS · Cessna 680CE · Extinguishing System
  > DURING A SCHEDULED INSPECTION OF THE APU COMPARTMENT THE TECH FOUND THE FIRE EXTINGUISHING SYSTEM NOZZLE CRACKED 2.5" AT THE BULKHEAD MOUNTING FLANGE. THIS CONDITION AND PICTURES HAVE BEEN SENT TO UNDER SCR 657016.
- [SDR DXTA2013030805309](https://openairdocs.org/sdr/DXTA2013030805309.md): Squat Switch · out of adjust · Mar 7, 2013 · N341QS · Cessna 680CE · Landing Gear Position and Warning
  > DEPARTED, RECEIVED AN AMBER WOW MISCOMPARE MESSAGE. ON GEAR RETRACTION LANDING GEAR DID NOT RETRACT AND RED UNLOCK LIGHT ILLUMINATED. RETURNED LANDING HANDLE DOWN IAW (H-2) PROCEDURE. RED UNLOCK LIGHT WENT OUT AND 3 GREEN LIGHTS ON. NORMAL LANDING. AMBER W
- [SDR DXTA2012112105189](https://openairdocs.org/sdr/DXTA2012112105189.md): Bulb · inoperative · Nov 20, 2012 · N341QS · Cessna 680CE · Landing Gear Position and Warning
  > LANDING, HAD AN UNSAFE GEAR INDICATION (NO GREEN LIGHT ON LT MAIN) WE HAD GREEN LIGHTS FOR RT MAIN AND NOSE GEAR AND NO RED UNLOCK LIGHT. RAN GEAR WILL NOT EXTEND CHECKLIST. STILL NO GREEN. JIGGLED LT MAIN GEAR LIGHT AGAIN AND IT CAME ON. FOUND LT GEAR INDICA
- [SDR DXTA2012111305182](https://openairdocs.org/sdr/DXTA2012111305182.md): Coalescer Bag · odor · Nov 12, 2012 · N341QS · Cessna 680CE · Humidity Control System
  > ON ROTATION THROUGH FIRST POWER REDUCTION ABOUT 2 MINUTES AT HIGH BODY ANGLE, A STRONG OIL BURNING ODOR OCCURRED. WENT AWAY AT THAT TIME. DID NOT HAPPEN ON GROUND OR ANY OTHER TIME DURING FLIGHT. INSPECTED BOTH ENGINE EXHAUSTS AND APU EXHAUST AND FOUND NO
- [SDR DXTA2012081305091](https://openairdocs.org/sdr/DXTA2012081305091.md): Cowling · broken · Aug 10, 2012 · N341QS · Cessna 680CE · Engine Cowling System
  > 75 PERCENT OF BOTTOM HALF OF RT ENGINE COWLING IS MISSING. PERFORMED AIRCRAFT FOREIGN OBJECT DAMAGE INSPECTION IAW MM 5-50-00. NO FURTHER DAMAGE NOTED. PERFORMED ENGINE FOREIGN OBJECT DAMAGE INSPECTION IAW MM 05-50-00. NO DAMAGE NOTED. REMOVED REMNANTS OF THE
- [SDR DXTA2012081305092](https://openairdocs.org/sdr/DXTA2012081305092.md): Door · open · Aug 10, 2012 · N341QS · Cessna 680CE · Nacelle/Pylon, Main Frame
  > ON LT ENGINE, THE THREE SMALL LATCHED ON THE LOWER FRONT OF COWLING WERE FOUND UNLATCHED. ON THE LATCHED ON THE SIDE OF THE COWLING, LATCH 1 (FROM THE FRONT) WAS HANGING DOWN WITH THE TAB IN THE LATCHED POSITION. LATCH 2 THE HOOK WAS FOUND BEHIND THE LATCH BA
- [SDR DXTA2012011004843](https://openairdocs.org/sdr/DXTA2012011004843.md): Fuel Nozzle · clogged · Jan 10, 2012 · N341QS · Cessna 680CE · Fuel Injector Nozzle
  > AFTER TAKEOFF AT HIGH POWER SETTING AND RELATIVELY LOW AIRSPEED ON CLIMBOUT, A STRONG ODOR OF FUMES CAME INTO COCKPIT AND CABIN FOR ABOUT 10 MINS. THE APU WAS NOT RUNNING AND ALL ENGINE PARAMETERS WERE NORMAL. ODOR SEEMED TO DISSIPATE DURING CRUISE BUT RETURN
- [SDR DXTA2011111404787](https://openairdocs.org/sdr/DXTA2011111404787.md): Wire · chafed · Nov 13, 2011 · N341QS · Cessna 680CE · Electrical Power System Wiring
  > IN CRUISE AT FL230 A STRONG ELECTRICAL ODOR WAS DETECTED IN THE FWD CABIN AND COCKPIT. SECURED INTERIOR ELECTRICAL SWITCH AND ODOR DISSIPATED. FOUND THROTTLE QUADRANT PANEL WIRE CHAFED. REPAIRED PER WM 20-10-07. OPS CHECK GOOD.
- [SDR 2010F00025](https://openairdocs.org/sdr/2010F00025.md): Warning Light · illuminated · Feb 4, 2010 · N341QS · Cessna 680CE · Engine Indicating System
  > ENGINE CHIP DETECT ILLUMINATED IN FLIGHT, REMAINED ON FOR LAST 20 MINUTES OF FLIGHT.
- [SDR DXTA2009021203501](https://openairdocs.org/sdr/DXTA2009021203501.md): Switch · inoperative · Feb 11, 2009 · N341QS · Cessna 560CESSNA · Cabin Cooling System
  > AT FL410 FOR 2.5 TO 3 HOURS - AMBER CAS MSG ACM O'TEMP DISPLAYED & WITHIN 5 SEC AMBER EMERGENCY PRESSURIZATION DISPLAYED - PAX SAID SMOKE & FUMES IN CABIN. REQUESTED LOWER ALTITUDE & DESCENDING THROUGH FL390 BOTH CAS MSGS EXTINGUISHED - VERY LIGHT SMOKE. REP
- [SDR DXTA200702714](https://openairdocs.org/sdr/DXTA200702714.md): Engine · power loss · Dec 25, 2007 · N341QS · Cessna 560CESSNA · Engine Fuel and Control
  > ON TAKEOFF, UNABLE TO MAKE TAKEOFF, N1OF 95.5 PERCENT UNLESS THE POWER LEVER ON RT ENGINE WAS AT THE FIREWALL STOP. OPS CHECK GOOD ON ENGINE RUN. ALL NUMBERS WITHIN SPECS IAW MM 72-00-00. THROTTLE KNOB SPLIT WITHIN LIMITS.
- [SDR DXTA200702406](https://openairdocs.org/sdr/DXTA200702406.md): Valve · failed · Aug 15, 2007 · N341QS · Cessna 560CESSNA · Landing Gear Brake System
  > BRAKES FAILED ON LANDING. REMOVED AND REPLACED BRAKE BLEED VALVE WITH NEW, PERFORMED FUNCTIONAL CHECKED GOOD. I.A.W. 560 M/M 32-42-04. NO LEAKS NOTED P/N 77B62 REMOVED AND REPLACED ANTISKID SERVO VALVE WITH OVERHAULED ASSY. PERFORMED FUNCTIONAL CHECK, CHECKE
- [SDR DXTA200702162](https://openairdocs.org/sdr/DXTA200702162.md): Anti-Skid Sys · malfunctioned · Apr 29, 2007 · N341QS · Cessna 560CESSNA · Brake Anti-Skid Section
  > ANTI-SKID PULSES DURING NORMAL BRAKE USE. RETURNED TO DEPARTURE. [SUP 05-03-07] REMOVED & REPLACED A/S CONTROL BOX IAW CESSNA 560 M/M CHPT 32-42-00.
- [SDR DXTA200702152](https://openairdocs.org/sdr/DXTA200702152.md): Brake Assy · weak · Apr 27, 2007 · N341QS · Cessna 560CESSNA · Landing Gear Brake System
  > BRAKES ARE SPONGY AND SLOPPY FEELING DURING LANDING. RT SIDE PULSATED INTERMITTENTLY. [SUP 05-03-07] PERFORMED BRAKE & ANTI-SKID BLEEDING PROCEDURE 3 TIMES ON EACH WHEEL TO ENSURE REMOVAL OF ALL AIR FROM SYSTEM. LEAK CHECK GOOD. TAXIED AIRCRAFT FOR 20 MINUT

Next page: https://openairdocs.org/aircraft/N341QS/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 = 'N341QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N341QS/reports

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