Aircraft Description
N8200G is a 1971 Cessna 177RG, a single-engine reciprocating (piston) aircraft registered to Rj Vincent Enterprises LLC in Rancho Santa Fe, CA. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on March 29, 1971. The registration certificate was issued on March 7, 2024. The registration is set to expire on March 31, 2031. Powered by a Lycoming IO-360-A1B6 engine producing 200 horsepower, N8200G is. The aircraft's Mode S transponder code is AB333A (hex), used for ADS-B identification and flight tracking. N8200G was last tracked by AviatorDB at coordinates 32.8262, -116.9720 on July 28, 2025. The FAA registry record for N8200G was last updated on March 7, 2024. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna 177 Cardinal was an ambitious four-seat general aviation aircraft designed to replace the popular Cessna 172 Skyhawk with modern features including a cantilever wing and all-flying stabilator. First flown in 1967 and introduced in 1968, it was a high-wing single-engine monoplane that seated four occupants with improved visibility and comfort over its predecessor. Spanning over 35 feet with sleek aerodynamic lines, the Cardinal suffered from initial underpowering that hampered its commercial success. Manufactured by Cessna Aircraft Company from 1968 to 1978, approximately 4,295 units were produced across all variants. AviatorDB tracks 80,556 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C177.
AviatorDB has found no NTSB accident or incident reports involving N8200G. 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 31, 2002 | IAD02LA056 | Substantial | None | The separation of the engine induction alternate air door, which resulted in a loss of engine power. A factor was the non-compliance with the manufacturer's service letter. |
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