N675QS2019 Textron Aviation INC 680A
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply15 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Co-owners
- Certificate issued
- Mar 3, 2026
- Expires
- Mar 31, 2033
- Airworthiness
- Standard · Transport
- Airworthiness date
- Aug 25, 2019
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
- 2019
- Serial number
- 680A0212
- 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
- A8EFBA
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 (15)
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.
- Doors · door · lack of lubeJul 14, 2026
THE MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO LATCH. DURING SEVERAL CLOSURES, THE RESISTANCE VARIED, BUT WHEN IT DID HANG UP, THE INSIDE HANDLE WAS ABOUT IN THE MIDDLE OF THE THROW. CLEANED AND LUBRICATED DOOR STOP. PREFORMED SATISFACTORY OPS CHECK IAW CE 680A AMM / 52-10-00 NO FURTHER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · pin · lack of lubeMay 20, 2026
MAIN CABIN DOOR HANDLE DIFFICULT TO FULLY ENGAGE IN LOCKED POSITION WHEN CLOSING DOOR FROM EITHER INSIDE OR OUTSIDE. HANDLE TRAVELS FREELY WHEN DOOR IS OPEN. OPERATED DOOR/DOOR HANDLE MULTIPLE TIMES FROM BOTH INSIDE AND OUTSIDE WITH DOOR IN THE OPEN AND CLOSED POSITIONS. DOOR/DOOR HANDLE OPERATES…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · module · defectiveJan 31, 2026
FLAP FAIL AND CAS MESSAGE APPEARED FOR EVERY FLAP SETTING SELECTED. RESET REQUIRED AND QRH RUN FOR EACH FAILURE (FLAPS 1, FLAPS 2, FLAPS FULL SELECTIONS). CORRECTIVE ACTION: DURING ARES DOWNLOAD ANALYSTS DISCOVERED THE GIA#1 FAILED ANDGENERATED ALL ASSOCIATED REMOVED SUSPECT BAD GIA#1 P/N…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Autoflight · module · defectiveJan 31, 2026
ON CLIMB OUT FULL NOSE DOWN TRIM REQUIRED. AUTOPILOT KICKED OFF. DECISION MADE TO SLOW THE AIRCRAFT BELOW 200 KTS TO MAINTAIN CONTROL AND LESSEN CONTROL INPUTS. LANDED AIRCRAFT UNDER MAX WEIGHT. CORRECTIVE ACTION: DURING ARES DOWNLOAD ANALYSTS DISCOVERED THE GIA#1 FAILED ANDGENERATED ALL…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · unknown · odorDec 6, 2025
WITH THE APU ON & BLEED AIR SELECTED ON, SMELL AN ELECTRICAL BURNING. TRACKED ODOR BACK TO LT SIDE OVERHEAD HEAT DUCT. WHEN TOUCHED, METAL TRACK WHERE THE HEATER DUCT IS THAT HOUSES AN OVERHEAD LIGHT STRIP, TOO HOT TO TOUCH & HAS A BURNING ODOR. HEAT IS TRANSFERRING TO ROOF LINER. ODOR IS MORE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · fitting · corrodedNov 11, 2025
AFTER REMOVAL OF NLG ACTUATOR FOUND CORROSION ON THE AFT FITTING ASSEMBLY. REMOVED CORRODED NLG ACTUATOR FITTING AND REPLACED WITH NEW CUSTOMER SUPPLIED NLG FITTING IAW TEXTRON STANDARD REPAIR SR-680A-ATA53-33739 REV. A STANDARD REPAIR - NLG ACTUATOR FITTING REPLACEMENT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedNov 10, 2025
FOUND 43 AREAS OF CORROSION UNDER AFT BELLY PANEL 316CBC. MECHANICALLY REMOVED CORROSION WHERE 36 NUTPLATES WERE REMOVED AND 4 ADDITIONAL AREAS IN BAY 316CBC IAW SRM 51-70-03. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-03 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · tunnel wall · corrodedNov 7, 2025
REPAIRED LEVEL 2 CORROSION ON LH AND RH NLG TUNNEL SKINS PER AQRD ERO-986034 REV.IR, TITLED "N675QS NLG TUNNEL CORROSION" DATED 28OCT25. SUPPORTED BY FAA FORM 8110-3 DATED 10/28/2025.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bushing · damagedApr 27, 2025
MAIN DOOR: TO OPEN MAIN CABIN DOOR A PUSH IS REQUIRED FROM THE INSIDE TO GET THE DOOR TO OPEN. CORRECTIVE ACTION: ACCOMPLISHED FF-1 INFORMATION RECEIVED FROM NETJETS- MED FWD HINGE ADJUSTMENT BUSHING BOLT ARE SEIZED SO THE DOOR CANNOT BE ADJUSTED. REMOVED L/H FWD CLOSET. REMOVED FORWARD HINGE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · latch · out of rigOct 10, 2024
MAIN DOOR: MAIN CABIN DOOR IS VERY HARD TO OPEN FROM THE OUTSIDE OF THE AIRCRAFT. REPEAT WRITE UP. CORRECTIVE ACTION: RIGGED CED LATCH/LOCK SYSTEM IN REF TO CE680A AMM 52-10-04. RIG CHECK GOOD, OPS CHECK OF CED OPENING FROM OUTSIDE GOOD WITH NO BINDING NOTED AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 15 reports.
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