N629QS2021 Textron Aviation INC 680A
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply10 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Co-owners
- Certificate issued
- Jul 23, 2026
- Expires
- Jul 31, 2033
- Airworthiness
- Standard · Transport
- Airworthiness date
- May 12, 2021
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Textron Aviation INC
- Model
- 680A
- Year
- 2021
- Serial number
- 680A0269
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A8391B
Engine
- Make and model
- P&W Canada Pw306d1
- Type
- Turbo-fan
- Power
- 5,907 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2026 – nowCo-ownerscurrent
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (1)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-07-13 | Landing Gear | May 15, 2018 | Airframe (680A)Serial numbers per UTC Service Bulletins 2-1706-1-32-1 Rev 1 and 2-1675-32-2 Rev 1 (brake assembly serial numbers). Only with: Equipped with brake assembly P/N 2-1706-1 (Model 510) or P/N 2-1675-1 (Models 680/680A) with serial number listed in table 1 of the applicable UTC service bulletin. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (10)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Landing gear · landing gear · malfunctionedOct 1, 2026
DURING CLIMB, PASSING FL370, FELT WHAT APPEARED TO BE A GEAR-RELATED BUMP. SHORTLY THEREAFTER, AN AMBER GEAR DISAGREE CAS MESSAGE WAS DISPLAYED, ACCOMPANIED BY AN AMBER DASHED NOSE GEAR INDICATION. COMPLIED WITH GEAR BUMP TROUBLESHOOTING IAW AMM 32-00-00. SENT THE MEASUREMENTS AND PRESSURES TO…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · inhibitor · corrodedJun 2, 2026
(LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION) INTERNAL CORROSION AFTER NDT NO CRACKS CLEANED AND APPLIED CORRISION INHIBITOR IAW SPM 51-30-10 THE LH TRAILING LINK PN#7441030-5 SN#3015789 WAS FOUND TO BE GOOD IN SERVICEABLE CONDITION
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · inhibitor · corrodedJun 2, 2026
SL680A-32-11 (LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION) - INTERNAL CORROSION. AFTER NDT NO CRACKS FOUND. CLEANED AND APPLIED CORRISION INHIBITOR IAW SPM 51-30-10 THE RH TRAILING LINK PN#7441030-5 SN# 30194768 WAS FOUND TO BE GOOD IN SERVICEABLE CONDITION
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Air conditioning and pressurization · filter · odorMar 5, 2025
COCKPIT ODOR: WHILE PROGRAMMING THE AIRCRAFT FOR OUR NEXT FLIGHT, WE NOTICED A DISTINCT ODOR IN THE COCKPIT; POSSIBLY ELECTRICAL IN NATURE. WE NOTICED A SLIGHT HAZE IN THE COCKPIT. WE POWERED DOWN THE AIRCRAFT UPON DISCOVERY. APU POWER, BLEED AIR, AND INTERIOR HAVE ALL BEEN POWERED ON FOR 30…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · strut · faultedFeb 28, 2024
DURING CLIMB THROUGH 180, A CHIRPING NOISE HEARD FROM CABIN. STOPPED AFTER ABOUT 2 MINS. ON ARRIVAL, MAIN DOOR WAS DIFFICULT TO UNLOCK. MOVEMENT OF LOCKING HANDLE PRODUCES A GRINDING NOISE FROM INSIDE. TROUBLESHOT AND FOUND THE SOURCE OF THE GRINDING NOISE IS THE MED SUPPORT STRUT, ATTEMPTED TO…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · connector · disconnectedFeb 10, 2024
EXIT LIGHT JUST BELOW TOILET LID INOP. TROUBLESHOOTING FOUND LIGHT ASSEMBLY CONNECTION LOOSE ON THE THE LAV LOWER PANEL EXIT SIGN LIGHT CONNECTOR, SECURED CONNECTION PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · unknown · unknownNov 22, 2023
RIGHT MLG LANDING GEAR EXTENSION: AFTER EXTENDING THE GEAR ON APPROACH, WE INITIALLY GOT A THREE-GREEN INDICATION, BUT AFTER ABOUT 30 SECONDS THE GEAR DISAGREE R CAS CAME ON. WE DIVERTED, SAME THING HAPPENED WHEN EXTENDING THE GEAR AT THE DIVERSION AIRPORT. WE BLEW THE GEAR DOWN AND LANDED WITHOUT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · unknown · unknownOct 2, 2023
LAV EMERG LIGHT: EMERGENCY LIGHT UNDER LAV. IS OUT. REMOVED EMER LIGHT UNDER LAV. PERFORMED DVI OF WIRING, PINS, AND CONNECTOR FOR ANY DEFECTS. NOTED BUILD UP OF SURFACE CORROSION AND DEBRIS COATING CONNECTOR AND PINS. REMOVED SURFACE CORROSION AND CLEANED CONNECTOR AS REQUIRED. REINSTALLED EMER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · unknown · unknownMay 5, 2023
WOW MISCOMPARE AMBER CAS: AT CRUISE ALTITDUE (41,000) GOT AN AMBER WOW MISCOMPARE AND THE LDG 2 GEAR CONT 2 CIRCUIT BREAKER POPPED. GEAR DID NOT EXTEND UNDER NORMAL PROCEDURE. RAN CHECKLIST TO EXTEND GEAR. REMOVED RH LANDING GEAR WOW PCB ASSEMBLY P/N 6768156-5 S/N 0956 DUE TO WOW MISCOMPARE CAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · aileron · vibrationDec 2, 2022
SIGNIFICANT AIRFRAME VIBRATION IN LEVEL FLIGHT AND ACCELERATING AT 12000'. VIBRATION CAME ON AT BETWEEN 270-290 KNOTS. FELT A LIGHT RUMBLE IN THE YOLK AT 210 KNOTS. REMOVED RT AILERON PANEL. INSTALLED A SERVICEABLE RT AILERON PANEL ASSEMBLY. WORK PERFORMED IAW AMM 57-60-05, POST-MAINTENANCE CHECKS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026