- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0246
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 10, 2020
- Certificate issued
- July 23, 2026
- Expires
- July 31, 2033
- Mode S code
- A80677
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2018 | 1 |
|---|---|
| 2023 | 1 |
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N616QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Textron 680A aircraft
FAA incident reports
No FAA accident or incident reports matched to N616QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Textron 680A aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026010206357Actuator · faultyPITCH TRIM JAM DURING TAKE-OFF. PRIMARY PITCH TRIM WOULD NOT ACTUATE NOSE DOWN WHILE BEING PRESSED CONSTANTLY FOR AT LEAST 5-6 SECONDS AFTER TAKE-OFF. A LOUD CLUNK/THUD NOISE WAS HEARD. SECONDARY TRIM WAS SELECTED AND USED TO REGAIN PITCH CONTROL. AN IMMEDIATESDR DXTA2025031702700Warning Message · false activationCABIN DOOR OPEN AMBER CAS: AFTER CLOSING DOOR, AMBER CAS MESSAGES "CHECK DOORS" AND "CABIN DOOR OPEN" DISPLAYED. RAN THE QRH CHECKLIST AND CAS MESSAGE CLEARED. THIS OCCURRED TWICE DURING THE DAY CORRECTIVE ACTION; COMPLETED THE CABIN DOOR - ADJUSTMENT/TEST MULSDR DXTA2023101998320Pcb · malfunctionedDOOR DOES NOT LOCK AFTER CLOSING & HANDLE MOVED DOWN. DOOR OPEN LIGHT ON DOOR ILLUMINATED. CAS MESSAGES CABIN DOOR OPEN & CHECK DOORS OPEN ARE ILLUMNATED. C/W OPS CHECK OF MCD & OPS CHECK FAILD. C/W TROUBLESHOOTING RECOMMENDATIONS. WENT INTO ARES FILE, & ISDR DXTA2023040783840Unknown · unknownAISLE LIGHT AT SEAT 10, AND ALL THREE EXIT LIGHTS AT THE MAIN EXIT REMAIN ILLUMINATED WITH EMERGENCY LIGHT SWITCH OFF AND BATTERY SWITCHES OFF. RESET INERTIA SWITCH,AS PER CE-680A AMM 33-50-11, CHARGE EMERGENCY BATTERY'S, PERFORMED OPS CHECK, OPS CHECK GOOD ISDR DXTA2023040783820Unknown · unknownAISLE LIGHT AT SEAT 10, AND ALL THREE EXIT LIGHTS AT THE MAIN EXIT REMAIN ILLUMINATED WITH EMERGENCY LIGHT SWITCH OFF AND BATTERY SWITCHES OFF. RESET INERTIA SWITCH,AS PER CE-680A AMM 33-50-11, CHARGE EMERGENCY BATTERY'S, PERFORMED OPS CHECK, OPS CHECK GOOD ISDR DXTA2022060863550Proximity Switch · defectiveCABIN DOOR OPEN AMBER CAS: CABIN DOOR OPEN CAS MESSAGE WILL NOT EXTHINGISH. RAN CHECKLIST STILL ILLUMINATED. ON SITE NETJETS MAINTENANCE CONFIRMED AN ISSUE WITH DOOR INDICATOR. // SIGNOFF// REMOVED BAD PROX SWITCH CORD SET P/N RKV4T·2/S90 AND REPLACED WITH A NSDR DXTA2022052762810Structure · out of positionMAIN DOOR: REPEAT WRITE UP. LOUD DOOR SQUEAL BEGINS AT 12000 FT AND BEGINS TO SUBSIDE AT APPROX 18000 FT. NO SPIKE IN CABIN PRESSURE WAS NOTICED AND HAD NORMAL RATE OF CLIMB APPROX 2500 FT PER MIN. C/W VISUAL INSPECION OF DOOR INNR SEAL. NO DEFECTS NOTED. INSSDR DXTA2022040759860None · damagedGEAR POSITION & WARNING: GEAR EXTENSION SPEED EXCEEDED DURING EMERGENCY DESCENT // SIGNOFF// COMPLIED WITH NLG STRUT EXTENSION INSPECTION IAW CE-680A MM 12·10-52. FOUND STRUT AT 9.95' / 0.122 OUT OF TOLERANCE CREATING UPLOCK TO BE IN UNSAFE CONDITION. LIMITS ASDR DXTA2022040759850None · noneNLG: DURING CRUISE FLIGHT AT FL400 WE OBSERVED A NOSE GEAR MISCOMPARE MESSAGE ON THE CAS. WE FOLLOWED THE CHECK LIST AND DETERMINED THE GEAR WAS UP AND LOCKED. WE CONTACTED THE FODM AND DETERMINED IT WAS SAFE TO CONTINUE. APPROXIMATELY 30 MINUTES LATER WE HADSDR DXTA2022033159430Switch · defectiveNLG: AT 37000, GEAR DIASGREE N CAS ILLUMINATED. FOLLOWED BY NOSE GEAR AMBER INDICATION LIGHT. BANGING NOISE HEARD FROM NOSE GEAR AREA. SPEED SLOWED TO 190 KNOTS. DESCENDED TO 17000, GEAR EXTENDED. NOSE GEAR EXTENDED PROPERLY WITH GEAR DOWN GREEN INDICATIOSDR DXTA2021091348660Lock · out of adjustMAIN DOOR HANDLE: WITH DOOR IN FULLY UP POSITION, DOOR HANDLE WILL NOT ROTATE TO CLOSE AND LATCH THE DOOR. THE HANDLE WILL NOT MOVE AT ALL. NO CHECK DOORS CAS. ONLY CABIN DOOR OPEN CAS. PROCEDURE N1 CABIN DOOR OPEN CHECKLIST STEP 4 - LIGHTS DO NOT FLASH. FOSDR DXTA2021091048600Handle · bindingMAIN CABIN DOOR WILL NOT CLOSE. DOOR HANDLE IS LOCKED IN OPEN POSITION AND WILL NOT MOVE. FOUND CABIN DOOR LATOT/LOCK OUT OF ADJUSTMENT. PERFORMED CABIN DOOR LATCH/LOCK SYSTEM ADJUSTMENT/TEST. OPERATIONAL CHECKS SATISFACTORY NO DISCREPANCIES NOTED AT THIS TIMSDR DXTA2021031939650Screw · looseMAIN DOOR: A LOUD SQUEAL IS HEARD DURING DESCENT BETWEEN 18-14,000FT. "CORRECTIVE ACTION" PRESSURIZED AIRCRAFT UP TO 3.7 PSI AND DID NOT HEAR HEAR ANY SQUEALING NOISES GOING UP. ON THE WAY DOWN WE HEARD THE SQUEALING NOISE START AT 2.2 PSI. FOUND AREA AT THE M
Reports on N616QS not matched to an aircraft · 11
They name N616QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2015122306142Horn · failedON TAKEOFF EXPERIENCED VIBRATION THAT WAS PRESENT IN BOTH YOKE & PEDALS. SEEMED TO INTENSIFY WITH INCREASED POWER & PITCH. CONTINUED THRU FL 230 BEFORE DECIDING TO DIVERT. DID NOT SEEM TO BE AS PRONOUNCED IN DESCENT. REMOVED RUDDER HORN ASSEMBLY. INSPECTSDR DXTA2012090605116Structure · corrodedCORROSION ON LT AND RT STRAKE ASSY. REPAIRED CORROSION ON LT AND RT VENTRAL STRAKE. MAJOR REPAIR.SDR DXTA2012090605115Attach Bracket · damagedRT WING INBD AILERON HINGE ATTACH BRACKET HAS 2.2500" BOLTS ON FWD SIDE INVESTIGATED RT WING INBD AILERON HINGE WITH .2500" BOLTS (AN4-7A, EXISTING) IN FWD HOLES. FOUND HOLES HAD BEEN PREVIOUSLY OVERSIZED. OVERSIZED HOLES ARE FOUND TO BE ACCEPTABLE IAW ENGIN
STCs that may be installed · 16
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 680A
STC ST04765NYUnprepared (Grass/Sod) Runway OperationsSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12344IBReplacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher