N4654F1966 Cessna P206A
This N-number isn't registered right now. Below is its last known registration, canceled Jan 2, 2020.
Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply1 service difficulty report
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 19, 2026- Last registered owner
- Individual owner
- City, state
- Bulverde, TX
- Certificate issued
- Jul 1, 2019
- Canceled
- Jan 2, 2020
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 26, 1966
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
- P206A
- Year
- 1966
- Serial number
- P206-0254
- 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
- A5AF18
Engine
- Make and model
- Cont Motor Io 520 Series
- Type
- Reciprocating
- Power
- 285 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2019 – 2020Individual ownerBulverde, TX
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (2)
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 (P206A) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)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. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
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.
- Navigation · casting · creepSep 18, 1996
THIS ALTIMETER WAS RECEIVED IN A PARTICULARLY HAZARDOUS CONDITOIN. ALL THREE END SHAKES ON THE CRITICAL ROTATING SHAFTS WERE UNDER THE MINIMUM TOLERANCE. THEY MEASURED .0000 INCH, .0006 INCH, AND .0008 INCH. THE HAIR SPRING WHEEL SHAFT IS THE ONE THAT MEASURED .0000 INCH. THE FACTORY RAN COLD…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026