Aircraft Description
N7736K is a 1979 Cessna P210N, a single-engine reciprocating (piston) aircraft registered to Valiair Lc Trustee in Ogden, UT. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on December 5, 1979. The registration certificate was issued on July 26, 2024. The registration is set to expire on July 31, 2031. Powered by a Cont Motor TSIO-520 SER engine producing 300 horsepower, N7736K is. The aircraft's Mode S transponder code is AA7760 (hex), used for ADS-B identification and flight tracking. N7736K was last tracked by AviatorDB at coordinates 25.9895, -111.3484 on June 29, 2025. The FAA registry record for N7736K was last updated on July 26, 2024. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna 210 Centurion, a high-performance single-engine aircraft that dominated the retractable-gear general aviation market for over two decades, first flew on January 22, 1957. This low-wing monoplane could carry up to six passengers and featured innovative retractable landing gear with fuel-injected Continental engines producing 260-310 horsepower. With cruise speeds reaching 200 knots and a service ceiling above 20,000 feet, the 210 bridged the performance gap between fixed-gear singles and twin-engine aircraft. Cessna Aircraft Company produced 9,304 examples between 1960 and 1986. AviatorDB tracks 80,556 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C210.
AviatorDB has found no NTSB accident or incident reports involving N7736K. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Mar 18, 2021 | ERA21LA159 | Substantial | None | The failure of the alternator control unit housing plug connection, which resulted in insufficient battery power to fully extend the landing gear. Contributing to the accident was the pilot’s decision to not use the emergency gear extension handle to secure the gear prior to landing. |
| Jul 20, 2004 | DEN04LA107 | Substantial | None | the failure of the engine's crankshaft due to the rotation of the engine's number two bearing, which resulted in the oil starvation of the crankshaft's number 2 main journal. Contributing factors include the engine's improper maintenance, and the in-flight collision with a fence post during a forced landing. |
The failure of the alternator control unit housing plug connection, which resulted in insufficient battery power to fully extend the landing gear. Contributing to the accident was the pilot’s decision to not use the emergency gear extension handle to secure the gear prior to landing.
the failure of the engine's crankshaft due to the rotation of the engine's number two bearing, which resulted in the oil starvation of the crankshaft's number 2 main journal. Contributing factors include the engine's improper maintenance, and the in-flight collision with a fence post during a forced landing.
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC