N7485Q1973 Cessna TU206F
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply4 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Co-owners
- City, state
- Hooksett, NH
- Certificate issued
- Sep 19, 2013
- Expires
- Sep 30, 2029
- Airworthiness
- Standard · Normal
- Airworthiness date
- Dec 18, 1973
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
- Cessna
- Model
- TU206F
- Year
- 1973
- Serial number
- U20602220
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AA1358
Engine
- Make and model
- Cont Motor Tsio-520 Ser
- Type
- Reciprocating
- Power
- 300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2013 – nowCo-ownersHooksett, NH · current
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 (3)
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 |
|---|---|---|---|
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (TU206F) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (TU206F)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (4)
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.
- Flight controls · control cable · corrodedMar 17, 1997
AIRCRAFT TOTAL TIME 3,075 HRS. AIRCRAFT BUILT AS LAND PLANE AND MODIFIED FOR FLOATS INSTALLATION IAW WIPAIRE STL SA1483GL. POH SUPPLEMENT REQUIRES 'OPERATION IN FRESH WATER ONLY' PLACARD DUE TO NO STAINLES STEEL CONTROL CABLES OR FUSELAGE INTERIOR PRIMER. CONTROL CABLES FOUND BADLY RUSTED IN BELLY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · structure · corrodedMar 17, 1997
AIRCRAFT TOTAL TIME 3,075 HRS. AIRCRAFT BUILT AS LAND PLANE AND MODIFIED FOR FLOATS INSTALLATION IAW WIPAIRE STL SA1483GL. POH SUPPLEMENT REQUIRES 'OPERATION IN FRESH WATER ONLY' PLACARD DUE TO NO STAINLES STEEL CONTROL CABLES OR FUSELAGE INTERIOR PRIMER. CONTROL CABLES FOUND BADLY RUSTED IN BELLY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · axle · corrodedMar 17, 1997
AIRCRAFT TOTAL TIME 3,075.0 HOURS. AIRCRAFT HAD BEEN CONVERTED TO SEAPLANE BY STC 1483GL IN 1991 AND OPERATED IN SALT WATER FOR 3 YEARS PRIOR TO ANNUAL INSPECTION IN 1997. ON DISASSEMBLY FOR MAINTENANCE AND INSPECTION, THE MLG AXLES WERE REMOVED FROM THE GEAR SWING-ARMS. AFTER ACCUMULATED GREASE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reportsShow fewer reports
- Landing gear · cylinder · crackedJul 1, 1996
HYDRAULIC LEAK. CRACK INSIDE OF HYDRAULIC CYLINDER. REPLACED PART WITH NEW. INSPECTED, FOUND CORROSION, POSSIBLY CAUSED BY GEAR INDICATOR LIGHT WIRES AND HYDRAULIC LINE BEING CLAMPED TO CYLINDER. A RUBBER/PLASTIC PAD HAD BEEN GLUED TO CYLINDER TO PREVENT CONTACT SO CORROSION OCCURRED AT PERIPHERY…
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