Aircraft Description
N210WS is a 1969 Cessna 210J, a single-engine reciprocating (piston) aircraft registered to Olin David G in Jupiter, FL. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on April 10, 1969. The registration certificate was issued on February 17, 2017. The registration is set to expire on February 28, 2027. Powered by a Cont Motor IO 520 SERIES engine producing 285 horsepower, N210WS is. The aircraft's Mode S transponder code is A1BB87 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N210WS was last updated on January 22, 2023. 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 N210WS. 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 (1)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Sep 5, 2013 | ERA13LA398 | Substantial | None | The failure of the landing gear hydraulic power pack system to provide sufficient pressure to lock the main landing gear in the down position. Contributing to the accident was the improper maintenance and inspection of the landing gear system, the pilot’s continued operation of the airplane with a known mechanical problem with the landing gear system, and the pilot’s failure to visually verify that the landing gear were down. |
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