Aircraft Description
N804ST is a 1980 Cessna 501, a twin-engine turbo-fan aircraft registered to Ial Corp in Lewes, DE. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on May 19, 2005. The registration certificate was issued on June 22, 2017. The registration is set to expire on June 30, 2027. Powered by a Williams FJ 44 SERIES engine producing 1900 pounds of thrust, N804ST is. The aircraft's Mode S transponder code is AAF25B (hex), used for ADS-B identification and flight tracking. The FAA registry record for N804ST was last updated on February 11, 2025. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna Citation I/SP, the first business jet certified for single-pilot operation, created the entry-level light corporate jet market and became the foundation for the world's largest family of business jets. First flown in 1969 as the FanJet 500, it was a straight-wing twin-turbofan aircraft that could seat up to seven passengers plus one pilot. With a maximum range of 1,325 nautical miles and short-field capabilities including a 2,930-foot takeoff distance, the aircraft was manufactured by Cessna Aircraft Company in Wichita, Kansas. AviatorDB tracks 80,556 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C501.
AviatorDB has found no NTSB accident or incident reports involving N804ST. 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 |
|---|---|---|---|---|
| May 24, 2016 | CEN16LA197 | Substantial | Minor | The pilot's failure to use supplemental oxygen as required during high-altitude flight, which resulted in his loss of consciousness following a loss of cabin pressurization. Contributing to the accident was the separation of the air conditioning system's primary pressurization duct and the subsequent failure of the aft pressure bulkhead check valve flapper due to progressive weakening from age. |
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC