# Service difficulty reports: N372QS A list on [N372QS](https://openairdocs.org/aircraft/N372QS.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2026060808336](https://openairdocs.org/sdr/DXTA2026060808336.md): Trim System · inoperative · Jun 4, 2026 · N372QS · Cessna 680SOV · Autopilot System > ON DEPARTURE WE RECEIVED AP FAIL A CAS MESSAGE. REENGAGED AP AND RECEIVED AP FAIL B CAS MESSAGE ALSO. WE FOUND THE PRIMARY STAB TRIM TO BE INOPERATIVE WITH NO PRIMARY STAB TRIM FAIL CAS MESSAGE. WE USED SECONDARY TRIM AND LANDED WITHOUT ISSUE. REMOVED ELEVATO - [SDR DXTA2025120205930](https://openairdocs.org/sdr/DXTA2025120205930.md): Brake Sys · malfunctioned · Dec 1, 2025 · N372QS · Cessna 680SOV · Landing Gear Brake System > AFTER PARKING AND SETTING THE BRAKE THE RIGHT BRAKE CALIPER WAS SMOKING WITH BRAKES SET AND RELEASED. PERFORMED GVI OF BOTH RT MLG BRAKES AND WHEEL ASSEMBLIES WITH NO LEAKS OR DEFECTS NOTED. SET BRAKES AND LET SIT FOR 30 MINUTES WITH NO DEFECTS AND PUMPED BR - [SDR DXTA2025111005614](https://openairdocs.org/sdr/DXTA2025111005614.md): Cable · out of adjust · Nov 7, 2025 · N372QS · Cessna 680SOV · Passenger/Crew Doors > MAIN DOOR DOES NOT GO DOWN ALL THE WAY. IT STAYS UP ABOUT AN INCH AND WHEN THE PASSENGERS STEP ON IT, IT DROPS THAT INCH UNTIL THE ARMS ARE FULLY EXTENDED. CABLE TENSION NEED TO BE ADJUSTED ACCOMPLISHED THE CABLE TENSION, INSPECTED FOUND CABLE TO MUCH TENSIO - [SDR 2025F00219](https://openairdocs.org/sdr/2025F00219.md): Skin · gouged · Sep 11, 2025 · N372QS · Cessna 680A · Wing, Plate/Skin > MECHANICALLY BLENDED HIGH SPOTS ON A GOUGE ON THE RH WING LEADING EDGE APPROXIMATELY 3.25 INCHES OTBD OF THE START OF THE LEADING EDGE. POLISHED AND RETURNED AREA TO ORIGINAL SURFACE FINISH IAW CESSNA 680 SPM 51-70-02 AND NETJETS ENGINEERING RFTS-114953 REV. 0 - [SDR DXTA2025082904755](https://openairdocs.org/sdr/DXTA2025082904755.md): Pushrod · out of adjust · Aug 28, 2025 · N372QS · Cessna 680SOV · Passenger/Crew Doors > UPON OPENING DOOR WE HEARD A LOUD GRINDING/BINDING NOISE ON DOOR DOWNWARD DESCENT, DOOR IS DIFFICULT TO LOCK DOWN AND REQUIRES EXCESSIVE FORCE TO LIFT HANDLE OVER DETENT TO CLOSE. VERIFIED. T/S DOOR AND FOUND CLOSING HANDLE PUSHROD TO BE OUT OF ADJUSTMENT. - [SDR DXTA2025080104399](https://openairdocs.org/sdr/DXTA2025080104399.md): Throttle · unknown · Jul 29, 2025 · N372QS · Cessna 680SOV · Power Lever > WHILE IN A DESCENT FROM FL 410 TO FL 340 ZERO, WITH THE THRUST LEVERS AT IDLE, THERE WAS A VIBRATION FROM THE RIGHT ENGINE AND THE ENGINE SHUTDOWN R CYAN MESSAGE ILLUMINATED. MOVED THE RIGHT THROTTLE OUT OF IDLE AND THE ENGINE SHUTDOWN R CYAN MESSAGE EXTINGUI - [SDR DXTA2025060203674](https://openairdocs.org/sdr/DXTA2025060203674.md): Compressor · stalled · May 28, 2025 · N372QS · Cessna 680SOV · Turbine Engine Compressor Section > REPEAT WRITE UP. BEGAN DESCENT FROM 43,000FT. THROTTLE WAS AT OR NEAR IDLE. AT 43,000FT WE FELT A COMPRESSOR STALL WHILE OBSERVING A RIGHT ENGINE ROLL BACK FOLLOWED BY A BLUE CAS MESSAGE ENG SHUTDOWN R. WITHIN 5-10 SECONDS THE ENGINE AUTOMATICALLY RESTARTED. E - [SDR DXTA2025050203276](https://openairdocs.org/sdr/DXTA2025050203276.md): Control Valve · faulted · Apr 29, 2025 · N372QS · Cessna 680SOV · Aircraft Fuel System > RIGHT ENGINE ENGINE COMPRESSOR STALL: AT APPROX. 42000FT IN THE DECENT, A COMPRESSOR STALL WAS FELT FOR ABOUT 5-10 SECONDS, AIRCRAFT VIBRATION WAS FELT AND LOUD BANGING NOISE WAS HEARD. THE R ENGINE SHUTDOWN BLUE ADVISORY MESSAGE WAS ALSO DISPLAYED WITH N1, N2 - [SDR DXTA2025010901874](https://openairdocs.org/sdr/DXTA2025010901874.md): Handle · detached · Jan 7, 2025 · N372QS · Cessna 680SOV · Passenger/Crew Doors > MAIN ENTRY DOOR INTERIOR GRAB HANDLE CAME OFF WHILE CLOSING DOOR. ATTACHING HARDWARE IS BROKEN OFF ALONG WITH PART OF THE STEP STRUCTURE AND IS INSIDE THE DOOR NOW. SEE ATTACHED PHOTOS. CORRECTIVE ACTION: REATTACHED HANDLE STAND OFFS. INSTALLED NEW STEP ASSEM - [SDR JGVR20230416001](https://openairdocs.org/sdr/JGVR20230416001.md): Spar Cap · corroded · Apr 16, 2024 · N372QS · Cessna 680CE · Wing Spar > R&R FASTENERS, BLENDED CORRODED AREAS OF THE AFT WING SPAR LOWER CAP LOCATED IN THE LH MAIN LANDING GEAR WHEEL WELL, PERFORMED NDT, REPORTED FOR RESULTS REPAIR DISPOSITION. RE-INSTALLED EXISTING HI-LOK'S WITH NEW COLLARS. APPLIED ALODINE, PRIMER, TOPCOAT AND C - [SDR DXTA2024010810555](https://openairdocs.org/sdr/DXTA2024010810555.md): Unknown · unknown · Jan 8, 2024 · N372QS · Cessna 680CE · Passenger/Crew Doors > THE MAIN CABIN DOOR HAND RAIL REQUIRES EXCESSIVE FORCE TO LOCK THE STEPS IN PLACE. ONCE LOCKED IN PLACE, HAND RAIL AGAIN NEEDS EXCESSIVE FORCE TO BE ABLE TO RAISE THE DOOR. FEELS LIKE SOMETHING WILL BREAK IF TENSION DOES NOT GET ADJUSTED. ADJUSTED CLOSING HA - [SDR DXTA2022091270120](https://openairdocs.org/sdr/DXTA2022091270120.md): Unknown · unknown · Sep 10, 2023 · N372QS · Cessna 680CE · Nose/Tail Landing Gear > UPON TAKE OFF, RETRACTED MLG, ALL 3 RETRACTED, THE MLG UNLOCK LIGHT DID NOT EXTINGUSH. COMPELETED UNLOCK QRH CHECKLIST, NLG DID NOT EXTEND. COMPLETED MLG WILL NOT EXTEND QRH CHECKLIST, UNSUCCESSFUL. PROCEDED TO LAND WITH NLG IN UP POSITION. PERFORMED GEAR - [SDR DXTA2022071165740](https://openairdocs.org/sdr/DXTA2022071165740.md): Line · leaking · Jul 11, 2022 · N372QS · Cessna 680CE · Hydraulic System, Main > A FEW SECONDS AFTER ROTATION AND LANDING GEAR RETRACTION WE RECEIVED A ?HYDRAULIC VOLUME LOW? AND ?HYDRAULIC PRESSURE LOW L-R? AMBER EICAS MESSAGES AND A RED LANDING GEAR ?UNLK? LIGHT WITH A RH MLG GREEN LIGHT ON THE GEAR INDICATORS. WE REQUESTED TO STAY AT 50 - [SDR DXTA2021100549950](https://openairdocs.org/sdr/DXTA2021100549950.md): Battery · defective · Oct 4, 2021 · N372QS · Cessna 680CE · Emergency Lighting > CABIN EMERG LIGHT: CABIN INTERIOR EMERGENCY LIGHT OVER WORK TABLE DOES NOT ILLUMINATE DURING EMERGENCY LIGHT CHECK. THE LIGHT DOES ILLUMINATE WITH MAIN DC POWER. (PRE FLIGHT) // SIGNOFF // PERFORMED EMER UGHTING OPS CHECK, DOME UGHT OVER WORK TABLE DID NOT IL - [SDR DXTA2021072945990](https://openairdocs.org/sdr/DXTA2021072945990.md): Spring · low tension · Jul 28, 2021 · N372QS · Cessna 680A · Passenger/Crew Doors > MAIN CABIN DOOR NOT PROPERLY COUNTER WEIGHTED. DOOR FALLS ALL THE WAY OPEN WHEN NOT COMPLETELY CLOSED. DOOR IS HARD TO BRING UP TO CLOSE FROM INSIDE CABIN. // SIGNOFF// GAINED ACCESS TO COUNTER BALANCE ASSEMBLY AND FOUND THE FWD SPRING UNDER TENSIONED. ADJUST - [SDR DXTA2021070644610](https://openairdocs.org/sdr/DXTA2021070644610.md): Counterweight · out of adjust · Jul 2, 2021 · N372QS · Cessna 680A · Passenger/Crew Doors > MAIN DOOR: MAIN CABIN DOOR COUNTERWEIGHT NEEDS ADJUSTMENT. DOOR WILL NOT STAY CRACKED AND FALLS 1 QUARTER TRAVEL. PREFORMED OPS CHECK WITH NO DEFECTS NOTED AND OPS CHECH GOOD ALL WORKCDONE IAW CE-680 AMM: 52-10-00 - [SDR JGVR20210212002](https://openairdocs.org/sdr/JGVR20210212002.md): Spar · corroded · Feb 12, 2021 · N372QS · Cessna 680A · Wing Spar > 4 AREAS OF VERIFIED CORROSION ON LH AFT SPAR IN MLG WELL. BLENDED 4 AREA OF CORROSION IN LH GEAR WELL, AFT LOWER SPAR. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED FINDINGS AND FOUND AREA TO BE BEYOND LIMITS. REPAIRED AREA OF LEVEL 2 CORRO - [SDR JGVR202102001](https://openairdocs.org/sdr/JGVR202102001.md): Spar · corroded · Feb 12, 2021 · N372QS · Cessna 680A · Wing Spar > 7 AREAS OF VERIFIED CORROSION ON RH AFT SPAR IN MLG WELL. BLENDED 7 AREA OF CORROSION IN RH GEAR WELL, AFT LOWER SPAR. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED FINDINGS AND FOUND AREA TO BE BEYOND LIMITS. REPAIRED AREA OF LEVEL 2 CORRO - [SDR DXTA2020111504356](https://openairdocs.org/sdr/DXTA2020111504356.md): Charger · failed · Nov 15, 2020 · N372QS · Cessna 680A · Emergency Lighting > EMERGENCY LIGHTING CONSISTING OF AFT OVER WING LIGHT, EXIT SIGN ON BULKHEAD SEAT NINE, EXIT SIGN OVERLAP, SEAT LAV OVERHEAD LIGHT ALL INOPERABLE WITH THE EMERGENCY SWITCH IN ARM AND MAIN BATTERIES OFF. ALSO WITH SWITCH IN ON POSITION AND MAIN BATTERIES OFF NO - [SDR EBVR20200915001](https://openairdocs.org/sdr/EBVR20200915001.md): Structure · corroded · Sep 15, 2020 · N372QS · Cessna 680A · Fuselage Main, Structure > FOUND DURING CABIN INTERNAL ZONAL INSPECTION, FOUND SEVERAL SPOTS OF CORROSION ON STRUCTURE UNDER THE CENTER DROP AISLE PANELS. PERFORMED AQRD REPAIR ERO-966932 REVISION A DATED SEP 10 2020 AT FUSELAGE FLOOR F.S. 157. - [SDR JGVR20190829001](https://openairdocs.org/sdr/JGVR20190829001.md): Control Valve · loose · Aug 29, 2019 · N372QS · Cessna 680CE · Cabin Temperature Control System > CABIN AND COCKPIT TEMPERATURE CONTROL VALVE INTERNAL AND EXTERNAL COMPONENTS ARE VERY LOOSE AND MOVING DURING VALVE OPERATION. FOUND WHILE PERFORMING TASK 21-61-00-7100 COCKPIT AND CABIN MANUAL TEMPERATURE CONTROL OPERATIONAL CHECK. PART NUMBERS OF THE CABIN - [SDR DXTA2019050702358](https://openairdocs.org/sdr/DXTA2019050702358.md): Power Supply · malfunctioned · May 6, 2019 · N372QS · Cessna 680CE · Attitude and Direction Data System > MAU 1 FAIL AMBER CAS ILLUMINATED - MAU 1 FAIL AMBER CAS MESSAGE ILLUMINATED IN FLIGHT A FL400 DURING CRUISE. ****CORRECTIVE ACTION**** REPLACED POWER SUPPLY MODULE ASSY. - [SDR JGVR201609220001](https://openairdocs.org/sdr/JGVR201609220001.md): Hinge · corroded · Sep 22, 2016 · N372QS · Cessna 680CE · Fuselage, Door Hinge > CORROSION DISCOVERED ON AFT BAGGAGE DOOR HINGES. REMOVED CORROSION VIA MECHANICAL MEANS. RECOMMEND REDUCING THE INSPECTION INTERVAL OR USING AN IMPROVED PRIMER IN THAT AREA. - [SDR DXTA2010031504031](https://openairdocs.org/sdr/DXTA2010031504031.md): Brake Assy · weak · Mar 13, 2010 · N372QS · Cessna 680CE · Landing Gear Brake System > BRAKES WEAKER THAN NORMAL AT HIGH SPEEDS. SEEMS MAX BRAKING NOT AVAILBLE WHEN APPLYING MAX BRAKE PEDAL PRESSURE. BRAKING ACTION NORMAL AT TAXI SPEEDS. INSPECTED BRAKES FOR WEAR & LEAKS - OK. PERFORMED FUNCITONAL CHECK OF POWER BRAKE SYS FOUND LT BRAKE PRESSUR - [SDR DXTA2009010303457](https://openairdocs.org/sdr/DXTA2009010303457.md): Seal · worn · Jan 3, 2009 · N372QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle > AFTER DEPARTURE GEAR HANDLE PLACED IN UP POSITION. NOSE GEAR RETRACTED NORMALLY " LIGHT OUT ". UNLOCK RED LIGHT REMAINED ILLUMINATED AS MAIN LT AND RT GEAR CYCLED UP AND DOWN APPROX 3 TIMES WHEN MAIN GEAR CYCLED DOWN " GREEN ' DOWN LOCK LIGHT. INSPECTED AND - [SDR DXTA2009010503457](https://openairdocs.org/sdr/DXTA2009010503457.md): Landing Gear · malfunctioned · Jan 3, 2009 · N372QS · Cessna 680CE · Landing Gear Retraction/Extension System > GEAR HANDLE PLACED IN UP POSITION, MAIN LT AND RT GEAR CYCLED UP AND DOWN APPRX 3 TIMES. - [SDR DXTA2008121503403](https://openairdocs.org/sdr/DXTA2008121503403.md): Autopilot Sys · unknown · Dec 15, 2008 · N372QS · Cessna 680CE · Autopilot System > AFTER DEPARTING, THE AP FAIL B MESSAGE FLICKERED THEN ILLUMINATED SOLID. TROUBLESHOT AUTOPILOT SYS USING DIAGNOSTIC MX SYS. NO FAULTS FOUND SYSTEM CHECKS GOOD IAW MM 45-40-00. - [SDR DXTA2008121603403](https://openairdocs.org/sdr/DXTA2008121603403.md): Autopilot Sys · malfunctioned · Dec 15, 2008 · N372QS · Cessna 680CE · Autopilot System > AFTER DEPARTING CMH THE AP FAIL B MSG FLICKERED THEN ILLUMINATED SOLID. ## 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 = 'N372QS' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N372QS/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.