# Service difficulty reports: N389QS

A list on [N389QS](https://openairdocs.org/aircraft/N389QS.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 · 58 reports

- [SDR DXTA2026081709313](https://openairdocs.org/sdr/DXTA2026081709313.md): Engine · malfunctioned · Aug 13, 2026 · N389QS · Cessna 680SOV · Engine (Turbine/Turboprop)
  > ON OUR DESCENT OUT OF FL390 WHILE DECREASING POWER, GOT A VIBRATION OUT OF RT ENG, FOLLOWED BY RT ENG ROLLING BACK. SHORTLY AFTER, RECEIVED AN ENG SHUTDOWN R CYAN MESSAGE. AFTER ABOUT 5 - 10 SECS, RT ENGINE STARTED RELIGHTING ITSELF, & STABILIZED TO NORMAL S
- [SDR DXTA2026080409113](https://openairdocs.org/sdr/DXTA2026080409113.md): Uplock Switch · out of adjust · Aug 2, 2026 · N389QS · Cessna 680SOV · Landing Gear Position and Warning
  > ON TAKEOFF THE NOSE GEAR CAME UP WITH A LOUD BANG. IT WAS BOTH AUDIBLE AND FELT THROUGH THE COCKPIT FLOOR. IT SEEMED TO RETRACT SLIGHTLY SLOWER THAN NORMAL. ALL THE LIGHTS WERE OUT. IT EXTENDED NORMALLY. I¿M N POSTFLIGHT I NOTICED ONE OF THE HYDRAULIC LIN
- [SDR DXTA2026062208503](https://openairdocs.org/sdr/DXTA2026062208503.md): Solenoid · faulted · Jun 18, 2026 · N389QS · Cessna 680SOV · Engine (Turbine/Turboprop)
  > ON THE INITIAL DESCENT (FL430). WE FELT A LARGE VIBRATION FOLLOWED BY INDICATIONS OF THE THE RIGHT ENGINE ROLLING BACK. ENGINE SHUTDOWN RIGHT CYAN CAS DISPLAYED. AFTER 5-10 SECONDS, WE AGAIN FELT A VIBRATION/SURGE FOLLOWED BY INDICATION OF THE ENGINE RELIGHT
- [SDR DXTA2026022306949](https://openairdocs.org/sdr/DXTA2026022306949.md): Sign · inoperative · Feb 19, 2026 · N389QS · Cessna 680SOV · Emergency Lighting
  > 33-50-01 EMERGENCY CABIN LIGHTING REPEAT WRITE-UP. FLASHING EVERY 15 SECONDS. REMOVED MED AFT EXIT SIGN MARKER LIGHT ASSEMBLY PN 9919055-2 SN 07C197A. INSTALLED NEW LIGHT PN 9919055-2 SN 19L561A. PERFORMED OPS TEST OF EMER LIGHTS AND IT CHECKS GOOD. POWERED
- [SDR DXTA2026021706910](https://openairdocs.org/sdr/DXTA2026021706910.md): Switch · faulty · Feb 15, 2026 · N389QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHT SWITCH IN ARM POSITION, APU RUNNING AND EMERGENCY LIGHTS FLASH ON OFF ABOUT EVERY 15 SECONDS. CORRECTIVE ACTION: REMOVED AND REPLACED THE RELAY KC006 OPS CHECK GOOD FOR RELAY OPERATION AND ELIMINATED FLICKER. WORK PERFORMED IAW CE-680 MM 33-50-
- [SDR DXTA2026012106599](https://openairdocs.org/sdr/DXTA2026012106599.md): Relay · faulted · Jan 19, 2026 · N389QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHT SYS FAILED PREFLIGHT CHK. WITH SWITCH IN ARM, NO LIGHTS ILLUMINATED. EMERG LIGHT SWITCH ON, CABIN DOOR LIGHTS FAILED, AS LIGHT OVER GALLEY WORK AREA FAILED. WHILE MOVING EMERG LIGHT SWITCH, LIGHTS OCCASIONALLY FLICKER VERY BRIEFLY THEN GO OU
- [SDR DXTA2026010806429](https://openairdocs.org/sdr/DXTA2026010806429.md): Light · malfunctioned · Jan 4, 2026 · N389QS · Cessna 680SOV · Emergency Lighting
  > WITH EMER LIGHTS IN THE ARM POSITION-NO LIGHTS ILLUMINATE. HOWEVER, EVERY 30 SECONDS OR SO, ALL OF THE EMERGENCY LIGHTS FLASH TEMPORARILY (SEE ATTACHED VIDEO). GAINED ACCESS TO PILOT CONTROL EMERGENCY LIGHTS RELAY (KC005) PN: M83536/15-022L NSN THEN INSTALLE
- [SDR DXTA2025123106347](https://openairdocs.org/sdr/DXTA2025123106347.md): Battery Pack · inoperative · Dec 29, 2025 · N389QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHT ABOUT MED INOP. ALSO FORWARD FACING EMERGENCY LIGHT ON LEFT SIDE IS FLICKERING. PLEASE SEE PHOTO/ VIDEO CORRECTIVE ACTION: REMOVED #1 E-BATT PN 6430028-1 SN F24-11024 AND INSTALLED A NEW BATT PN 6430028-1 SN K2511703. REMOVED #4 E-BATT PN 64300
- [SDR DXTA2025111105626](https://openairdocs.org/sdr/DXTA2025111105626.md): Battery Pack · failed · Nov 9, 2025 · N389QS · Cessna 680SOV · Emergency Lighting
  > MAIN DOOR EMERGENCY EXIT LIGHT AND BOTH EXIT LIGHTS BESIDE MAIN CABIN DOOR APPEAR INOP. THEY DID NOT COME ON WITH EMER LIGHT CHECK OR WITH SWITCH SELECTED ON AFTER RUNNING APU FOR THE PREFLIGHT CHECKS. COMPLETED VISUAL INSPECTION OF EMERGENCY BATTERY POWER SUP
- [SDR JGVR20250625006](https://openairdocs.org/sdr/JGVR20250625006.md): Spar · corroded · Jun 25, 2025 · N389QS · Cessna 680CE · Wing Spar
  > REPAIRED CORROSION ON THE RH WING AFT WING SPAR WEB LOCATED AT THE INBOARD AND OUTBOARD HYDRAULIC CARRY-THROUGH FITTINGS BY R&R FITTINGS, BLENDING CORRODED AREAS, PERFORMING NDT, AND REPORTING OR REPAIR DISPOSITION. REPAIRED AREA PER NETJETS REQUEST FOR TECHNI
- [SDR JGVR20250625005](https://openairdocs.org/sdr/JGVR20250625005.md): Spar · corroded · Jun 25, 2025 · N389QS · Cessna 680CE · Wing Spar
  > MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED INSIDE RH GEARWELL BAY 720DR ON AFT SPAR WEB AND MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED INSIDE LH GEARWELL BAY 730DL ON AFT SPAR WEB. PERFORMED NDT AND REPORTING OR REPAIR DISPOSITION. REPAIRED AREA PE
- [SDR JGVR20250625004](https://openairdocs.org/sdr/JGVR20250625004.md): Spar · corroded · Jun 25, 2025 · N389QS · Cessna 680CE · Wing Spar
  > REPAIRED CORROSION ON THE LH WING AFT WING SPAR WEB LOCATED AT THE #4 SPOILER HYDRAULIC CARRY-THROUGH FITTINGS AND THE RH WING AFT WING SPAR WEB AT THE #9 SPOILER HYDRAULIC CARRY-THROUGH FITTINGS, BY R&R THE FITTINGS, BLENDING CORRODED AREAS, PERFORMING NDT, A
- [SDR JGVR20250625003](https://openairdocs.org/sdr/JGVR20250625003.md): Skin · corroded · Jun 25, 2025 · N389QS · Cessna 680CE · Ailerons
  > REPAIRED CORROSION ON THE RH AILERON LOWER SKIN BY BLENDING, PERFORMING NDT, AND REPORTING OR REPAIR DISPOSITION. REPAIRED AREA NETJETS REQUEST FOR TECHNICAL SERVICES BY CLEANING, TREATING AND PRIMING REPAIR AREA, FABRICATING AND INSTALLING REPAIR DOUBLER.
- [SDR DXTA2025052003552](https://openairdocs.org/sdr/DXTA2025052003552.md): Screw · loose · May 18, 2025 · N389QS · Cessna 680SOV · Wing Main, Frame Structure
  > THE AIRCRAFT WAS ON A FERRY LEG FROM KSWO TO KDAL AND WAS FLOWN AT 17000, ON AN INITIAL SIGHTING OF A THUNDERSTORM WE TURNED WEST FROM A SOUTH WEST ARRIVAL HEADING AND DESCENDED FROM 17000 TO 9000 AND REDUCED AIRSPEED THE AIRCRAFT WAS IN A CLEAN CONFIGURATION
- [SDR DXTA2025041403014](https://openairdocs.org/sdr/DXTA2025041403014.md): Light · no discrepancy · Apr 9, 2025 · N389QS · Cessna 680SOV · Emergency Lighting
  > CABIN EMERG LIGHT: MAIN DOOR EXIT EMER LIGHT OFF WITH SWITCH IN ON POSITION. CORRECTIVE ACTION: OPERATIONAL CHECK OF MAIN DOOR EXIT EMER LIGHT NORMAL IAW CE-680 AMM 33-50-10.
- [SDR DXTA2025040302906](https://openairdocs.org/sdr/DXTA2025040302906.md): Light · no discrepancy · Apr 1, 2025 · N389QS · Cessna 680SOV · Emergency Lighting
  > WITH APU RUNNING ON GROUND AFTER FLIGHT EMERGENCY LIGHTS IN CABIN AND OVER WING FLICKER OR GO OUT AND THEN COME BACK ON. COMPLIED WITH OPERATIONAL CHECKS OF THE EMERGENCY LIGHTING SYSTEM FOR 10 MINUTES. ATTEMPTED TO DUPLICATE ITEM WITH BATTERIES, APU, AND EX
- [SDR DXTA2025030302547](https://openairdocs.org/sdr/DXTA2025030302547.md): Battery Pack · defective · Feb 28, 2025 · N389QS · Cessna 680SOV · Emergency Lighting
  > EMERG LIGHT SWITCH: WITH THE EMER LTS SWITCH IN THE ON POSITION, ALL EMER LIGHTS, WITH THE EXEPTION OF THE GALLEY WORK LIGHT AND THE MAIN DOOR EXIT SIGN ILLUMINATE. WHEN THE EMER LTS SWITCH IS PLACED IN THE ARM POSITION AND THE PAX SAFETY BUTTON IS PUSHED ON,
- [SDR DXTA2025022702487](https://openairdocs.org/sdr/DXTA2025022702487.md): Battery Pack · inoperative · Feb 23, 2025 · N389QS · Cessna 680SOV · Emergency Lighting
  > EMERG LIGHT SWITCH: EMERGENCY LIGHTS DO NOT WORK IN ARM POSITION, BUT DO ILLUMINATE IN THE ON POSITION. MAIN EXIT EMERGENCY LIGHTING DOES NOT WORK IN EITHER POSITION. CORRECTIVE ACTION; REPLACED #3 BATTERY PACK, BLOWN FUSE IN #2 BATTERY PACK AND INERTIA SWITCH
- [SDR DXTA2025012001998](https://openairdocs.org/sdr/DXTA2025012001998.md): Fuse · blown · Jan 16, 2025 · N389QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHTING: WHEN THE EMER LIGHT SWITCH IS PLACED IN THE ARMED POSITION AND THE PAX SAFETY SWITCH IS ON, ALL EMER LIGHTS REMAIN OFF AND NO AUDIBLE CHIME WITH OR WITHOUT DC POWER APPLIED. WHEN THE SWITCH IS MOVED TO THE ON POSITION, THE EMER LIGHTS ILLU
- [SDR DXTA2024122701683](https://openairdocs.org/sdr/DXTA2024122701683.md): Battery Pack · inoperative · Dec 24, 2024 · N389QS · Cessna 680SOV · Emergency Lighting
  > PAX SAFETY BUTTON SELECTED ON DURING DECENT, THE EMERGENCY LIGHTS DID NOT COME ON. RETESTED LIGHTS ON THE GROUND AND ONLY 1 EMERGENCY LIGHT NEXT TO THE LAV ILLUMINATES. ALL OTHER EMERG LIGHTS REMAIN OFF. REPLACED BATTERY PACK AND OPS CHECK GOOD IAW AMM 33-50
- [SDR DXTA2024112001190](https://openairdocs.org/sdr/DXTA2024112001190.md): Sign · inoperative · Nov 18, 2024 · N389QS · Cessna 680SOV · Emergency Lighting
  > EMERG EXIT SIGN/LIGHT: THE RED EXIT SIGN ON THE VERTICAL POST FORWARD OF THE MAIN ENTRY DOOR DOES NOT ILLUMINATE WHILE TESTING THE EMERGENCY LIGHTS. VERIFIED DISCREPANCY. REMOVED FWD MED INTERIOR UPHOLSTERY. INSPECTED WIRING AND SECURITY OF CONNECTION. NO DEFE
- [SDR DXTA2024112001167](https://openairdocs.org/sdr/DXTA2024112001167.md): Tensioner · loose · Nov 16, 2024 · N389QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN DOOR: MAIN DOOR HAS NO BALENCE TENSION GOING UP OR DOWN. OPENS-FALLS DOWN. HAVE TO USE FORCE TO GET UP. OPENED DOOR, VERIFIED DISCREPANCY CONDITIONS. REMOVED CABIN DOOR REEL COVERS, VERIFIED TENSIONS TO BE LOW. AFTER MULTIPLE ATTEMPTS, ADJUSTED CABLE TE
- [SDR 2024F00261](https://openairdocs.org/sdr/2024F00261.md): Skin · corroded · Oct 25, 2024 · N389QS · Cessna 680A · Fuselage Main, Plate/Skin
  > REPAIRED CORROSION OF TAILCONE L/H, R/H, AND MIDDLE LOWER SKIN ASSEMBLIES UNDER AFT CHIN FAIRING PER AQRD ERO-981949 REV. IR TITLED "N389QS AFT TAILCONE SKIN CORROSION REPAIR" DATED OCT 24, 2024. SUPPORTED BY FAA FORM 8110-3 DATED 10/24/2024.
- [SDR DXTA2024093000704](https://openairdocs.org/sdr/DXTA2024093000704.md): Fuse · blown · Sep 29, 2024 · N389QS · Cessna 680SOV · Emergency Lighting
  > SEVERAL CABIN EMERGENCY LIGHTS FAILED PREFLIGHT EMERGENCY LIGHT TEST. MISSING ALL MAIN ENTRY LIGHTS UPPER AND LOWER, FORWARD READING LIGHTS AND HALF OF THE LEFT FORWARD FLOOR LIGHT. RAN APU TO COMPLETE THE REST OF PREFLIGHT. AFTER SHUT DOWN TESTED AGAIN AND
- [SDR DXTA2024092600653](https://openairdocs.org/sdr/DXTA2024092600653.md): Counterweight · out of adjust · Sep 24, 2024 · N389QS · Cessna 680SOV · Passenger/Crew Doors
  > MAIN CABIN DOOR COUNTERWEIGHT NEEDS ADJUSTMENT - UNABLE TO CRACK DOOR WITHOUT IT FALLING OPEN. REMOVED DEFECTIVE FWD COUNTER BALANCE SPRING PN 6911319-202 NSN AND INSTALLED A NEW COUNTERBALANCE SPRING. ALSO REPLACED LUBRICATED SPRING AFT POSITION PN 6911319-
- [SDR DXTA2024062012088](https://openairdocs.org/sdr/DXTA2024062012088.md): Battery · defective · Jun 18, 2024 · N389QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY EXIT LIGHTS OVER EMERGENCY EXIT AND ON BULKHEAD SEAT BEHIND SEAT 9 FAIL PREFLIGHT TEST. MUST REPEAT RECHARGE PROCEDURE TO MAINTAIN CHARGE. REMOVED EMERGENCY LIGHTING BATTERY #4 P/N: CBS28-1 S/N: 008896 AND INSTALLED CUSTOMER SUPPLIED REPAIRED EMERGE
- [SDR DXTA2024061112021](https://openairdocs.org/sdr/DXTA2024061112021.md): Roller · out of adjust · Jun 10, 2024 · N389QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN ENTRY DOOR HANDLE EXTREMELY HARD TO OPEN. THE MAIN ENTRY DOOR HANDLE IS BINDING AND EXTREMELY HARD TO GET OPEN AND CLOSED. IT FEELS LIKE THE MECHANISM IN THE DOOR IS BINDING AS IT GOES OVER CENTER. RESOLUTION: FOUND THE FORWARD AND AFT MIDDLE LATCH ROLLE
- [SDR DXTA2024061012006](https://openairdocs.org/sdr/DXTA2024061012006.md): Door · out of adjust · Jun 9, 2024 · N389QS · Cessna 680A · Passenger/Crew Doors
  > OPENING DOOR FIRST THING IN THE MORNING. AFTER UNLOCKING HANDLE IT WAS EXTREMELY DIFFICULT TO OPEN THE HANDLE. THEN TO OPEN THE DOOR IT REQUIRED AN EXTREME AMOUNT FORCE TO PULL THE ACTUAL DOOR OPEN. THE DOOR OPENED ABOUT A FOOT AND STUCK. I CLOSED THE DOOR, AG
- [SDR DXTA2024040811438](https://openairdocs.org/sdr/DXTA2024040811438.md): Seal · leaking · Apr 7, 2024 · N389QS · Cessna 680CE · Passenger/Crew Doors
  > WHEN CLIMBING OUT BETWEEN APPROX 8000FT AND 11500FT THERE IS A LOUD WHISTLING SOUND COMING FROM THE MAIN CABIN DOOR. IT THEN GOES COMPLETELY AWAY AFTER HITTING 11,500FT. REMOVED MAIN CABIN DOOR PRIMARY DOOR SEAL AND REPLACED WITH CUSTOMER PROVIDED MAIN CABIN
- [SDR 2024F00084](https://openairdocs.org/sdr/2024F00084.md): Spar Splice · cracked · Mar 20, 2024 · N389QS · Cessna 680CE · Wing Spar
  > CRACK INDICATIONS, CENTER WING, CENTER SPAR SPLICE, WS 18 TO WS 37. ACCOMPLISHED ENGINEERING FIELD REPAIR FR-680-0149-12602 REV A. CRACK INDICATIONS, CENTER WING, CENTER SPAR SPLICE, WS 18 TO WS 37.
- [SDR 20240320083](https://openairdocs.org/sdr/20240320083.md): Trunnion · corroded · Mar 20, 2024 · N389QS · Cessna 680CE · Wing, Landing Gear Attach Fittings
  > CORROSION, RH MLG, TRUNNION, TRAILING LINK ATTACH LUGS. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0149-12564 REV A DATED 25 OCT 2023 AND FAA FORM 8100-9 DATED 25 OCT 2023; FIELD REPAIR - CORROSION, RH MLG, TRUNNION, TRAILING LINK ATTACH LUGS.
- [SDR 2023FA0000219](https://openairdocs.org/sdr/2023FA0000219.md): Unknown · unknown · Apr 18, 2023 · N389QS · Cessna 680A · Fuselage Structure (General)
  > LIGHTNING STRIKE BURN, FUSELAGE AND PYLON, SKINS, MULTIPLE LOCATIONS. REPORT NUMBER FR-680-0149-11733 REV - DATED 31 MARCH 2023 WITH FAA FORM 8100-9 DATED 7 APRIL 2023.
- [SDR 2023FA0000218](https://openairdocs.org/sdr/2023FA0000218.md): Unknown · unknown · Apr 18, 2023 · N389QS · Cessna 680A · Fuselage Structure (General)
  > LIGHTNING STRIKE BURN, FUSELAGE AND PYLON, SKINS, MULTIPLE LOCATIONS. REPORT NUMBER FR-680-0149-11733 REV - DATED 31 MARCH 2023 WITH FAA FORM 8100-9 DATED 7 APRIL 2023.
- [SDR DXTA2022090669500](https://openairdocs.org/sdr/DXTA2022090669500.md): None · defective · Sep 2, 2022 · N389QS · Cessna 120 · Air Conditioning System
  > COCKPIT ODOR: DURING EACH DESCENT WHEN THE THROTTLES/POWER WERE REDUCED THE CREW NOTICED A HOT OIL SMELL. THE SMELL WAS THE STRONGEST WHEN THE THROTTLES WERE AT IDLE. ENGINE OIL LEVELS ARE NORMAL.// CORRECTIVE ACTION// REMOVED AND REPLACED CONDENSER BAG. PERF
- [SDR DXTA2022032859050](https://openairdocs.org/sdr/DXTA2022032859050.md): Battery · faulted · Mar 28, 2022 · N389QS · Cessna 680CE · Battery/Charger System
  > BATTERY O?TEMP R CAS MESSAGE ILLUMINATED IN FLIGHT. COMPLETED QRH PROCEDURES AND DIVERTED ASAP. MAXIMUM TEMPERATURE SEEN WAS 79. ON FINAL, CAS MESSAGE BECAME INTERMITTENT GOING ON AND OFF. AFTER LANDING, NO SMOKE OR FUMES WERE OBSERVED AND BATTERY WAS COOL T
- [SDR DXTA2022012055440](https://openairdocs.org/sdr/DXTA2022012055440.md): Coalescer Bag · dirty · Jan 19, 2022 · N389QS · Cessna 680CE · Humidity Control System
  > ODORS IN COCKPIT / CABIN: ACM HAS A MOLDY/OILY/DIRTY SOCK SMELL WHEN RUNNING FROM EITHER THE APU OR ENGINES. RAN APU AND CHECKED FOR SMELL, NOTED A DIRTY, MUSTY SMELL COMING FROM THE AIR SYSTEM. CHECKED WATER SEP SOCK AND NOTED IT VERY DIRTY. DID NOT NOTE ANY
- [SDR DXTA2022010354700](https://openairdocs.org/sdr/DXTA2022010354700.md): Not Reported · not reported · Jan 2, 2022 · N389QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR EXTERNAL ENTRY HANDLE IS JAMMED AND WILL NOT OPEN WITHOUT EXCESSIVE MANEUVERING / FORCE APPLIED. // SIGNOFF// INSPECTED THE MAIN CABIN DOOR AND DETERMINED THAT THE OUTSIDE HANDLE HAD TO BE ADJUSTED. ADJUSTED THE MAIN CABIN DOOR OUTSI
- [SDR DXTA2021120152820](https://openairdocs.org/sdr/DXTA2021120152820.md): None · none · Nov 30, 2021 · N389QS · Cessna 680CE · Emergency Lighting
  > SEVERAL EMER LIGHT STUCK ON. // SIGNOFF // FOUND EMERGENCY LIGHTING BATTERY PACK #4 INERTIA SWITCH TRIPPED. RESET SWITCH AND EMERGENCY LIGHTS OP'S CHECKED GOOD. WORK PERFORMED PER CE680 M/M 33-50-10.
- [SDR DXTA2021110851480](https://openairdocs.org/sdr/DXTA2021110851480.md): Strut · unknown · Nov 6, 2021 · N389QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR TELESCOPING ROD: FORWARD ROD DISCONNECTED FROM FORWARD DOOR FRAME. ***CORRECTIVE ACTION*** REMOVED AND REPLACED FWD SUPPORT STRUT ASSEMBLY, SNAP RING AND KEYWAY. OPS CHECKS GOOD. REF CE-680 AMM 52-10-30
- [SDR DXTA2021031739590](https://openairdocs.org/sdr/DXTA2021031739590.md): Spring · defective · Mar 16, 2021 · N389QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR: DURING NORMAL OPERATIONS, HEARD AN UNUSUAL SNAP SOUND WHILE OPENING THE DOOR, BUT DOOR OPERATION WAS NORMAL. DURING PREFLIGHT THIS MORNING A BROKEN SPRING WAS DISCOVERED ON THE LEDGE OF THE DOOR WELL BEHIND THE MAIN AIRSTAIR DOOR.///SIGN-OFF///INSTA
- [SDR JGVR20201208001](https://openairdocs.org/sdr/JGVR20201208001.md): Spar · corroded · Dec 8, 2020 · N389QS · Cessna 680A · Vertical Stabilizer, Spar/Rib
  > 2 AREAS OF CONFIRMED CORROSION ON VERTICAL STAB SPAR RT AFT SPAR CLIP. MECHANICALLY AND HAND SANDED 1 AREA OF CORROSION LOCATED ON VERTICAL STAB RT AFT SPAR CLIP ON UPPER END AT 1ST RIVET AND 1 AREA OF CORROSION LOCATED 3RD RIVET BELOW UPPER RUDDER HINGE ON R
- [SDR 2020F00048](https://openairdocs.org/sdr/2020F00048.md): Skin · damaged · Nov 18, 2019 · N389QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > RIGHT WING ROOT SKIN DAMAGE (MIS-DRILLED HOLE). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ23664M1 DATED NOV. 11, 2019; 680-0149 (N389QS) RIGHT WING ROOT SKIN DAMAGE (MIS-DRILLED HOLE).
- [SDR JGVR20181219001](https://openairdocs.org/sdr/JGVR20181219001.md): Panel · corroded · Dec 19, 2018 · N389QS · Cessna 680SOV · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION AROUND NLG SQUAT SWITCH WIRE HARNESS CARRY THROUGH ON LT SIDE OF NOSE WHEEL WELL APPROX 1 O'CLOCK AREA.
- [SDR JGVR20180727003](https://openairdocs.org/sdr/JGVR20180727003.md): Firewall · cracked · Jul 27, 2018 · N389QS · Cessna 680CE · APU Cowling/Containment
  > REPAIRED TWO CRACKS IN THE APU FIREWALL BY STOP DRILLING INSTALLING DOUBLER PER AQRD ENGINEERING ORDER.
- [SDR JGVR20180727002](https://openairdocs.org/sdr/JGVR20180727002.md): Attach Angle · corroded · Jul 27, 2018 · N389QS · Cessna 680CE · APU Cowling/Containment
  > REPLACED EXISTING CORRODED APU TAILCONE FAIRING ATTACH ANGLE WITH NEW RT P/N 6912630-68 AND LT ANGLE P/N 6912630-67 REFERENCING SRM 51-40-03 AND SPM 20-40-20.
- [SDR JGVR20180727001](https://openairdocs.org/sdr/JGVR20180727001.md): Skin · corroded · Jul 27, 2018 · N389QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > FOUND CORROSION AROUND AIRCRAFT OEM DATA TAG, REMOVED DATA TAG, MECHANICALLY BLENDED CORRODED AREA, PERFORMED NDT AND REPORTED RESULTS FOR DISPOSITION. CLEANED, TREATED, PRIMED AND PAINT AREA IAW REPAIR MEMO. REINSTALLED EXISTING AIRCRAFT DATA TAG.
- [SDR 2017F00088](https://openairdocs.org/sdr/2017F00088.md): Spar Cap · corroded · Apr 12, 2017 · N389QS · Cessna 680SOV · Vertical Stabilizer, Spar/Rib
  > CORROSION ON VERTICAL AFT SPAR CAPS.
- [SDR DXTA2016072706272](https://openairdocs.org/sdr/DXTA2016072706272.md): Wire · chafed · Jul 27, 2016 · N389QS · Cessna 680CE · Fire Protection System Wiring
  > INFLIGHT ENGINE FIRE DETECTOR L CAS MESSAGE DISPLAYED. ALSO NOTED THE CIRCUIT BREAKER TRIPPED. PUSHED IN CIRCUIT BREAKER POWERED UP ACFT. CIRCUIT BREAKER POPPED. TROUBLESHOT DOWN TO A CHAFED WIRE ON THE ENGINE WIRE HARNESS. CUTOUT BAD SECTION OF WIRE INST
- [SDR DXTA2014031105683](https://openairdocs.org/sdr/DXTA2014031105683.md): Structure · corroded · Mar 7, 2014 · N389QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > CORROSION FOUND IN LT WW DURING INSPECTION. REPAIRED CORROSION DAMAGE IAW REPAIR DEFINITION S-680-0149 05RD.
- [SDR DXTA2014020565640](https://openairdocs.org/sdr/DXTA2014020565640.md): Brake · frozen · Feb 5, 2014 · N389QS · Cessna 680CE · Brake
  > UPON INITIAL LANDING TOUCHDOWN, LT MAIN WHEEL BRAKES WERE FROZEN. RESULTED IN BOTH LT MAIN BLOWN TIRES. INSPECTED EXTERIOR OF ACFT & FOUND NO FURTHER DAMAGE. ACCOMPLISHED MAIN GEAR TIRE BURST CHECK IAW CE-680 AMM 5-50-00. NO DEFECTS NOTED. REMOVED AND REPL

Next page: https://openairdocs.org/aircraft/N389QS/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 = 'N389QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N389QS/reports

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