N3633S - 1986 Schweizer Aircraft CORP G-164B Aircraft Registration
G1641986 SCHWEIZER AIRCRAFT CORP G-164B
Aircraft Description
N3633S is a 1986 Schweizer Aircraft Corp G-164B, a single-engine reciprocating (piston) aircraft registered to Kingrey William Sampson III in Richmond, TX. This aircraft holds a restricted airworthiness certificate issued by the Federal Aviation Administration on March 25, 1986. The registration certificate was issued on September 4, 2014. The registration is set to expire on September 30, 2027. Powered by a P&w R1340 SERIES engine producing 600 horsepower, N3633S is. The aircraft's Mode S transponder code is A41A43 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N3633S was last updated on March 17, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Schweizer Aircraft Corp is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 65 Schweizer Aircraft Corp aircraft currently registered in the FAA database, including the G-164B model.
AviatorDB has found no NTSB accident or incident reports involving N3633S. 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 |
|---|---|---|---|---|
| Jun 29, 2013 | ERA13LA312 | Substantial | None | A failure of the right main landing gear wheel rim during the landing roll, resulting in a loss of control and a subsequent collapse of the right main landing gear. |
| Aug 26, 2008 | MIA08LA174 | Substantial | None | The mechanic’s failure to torque check the axle-to-spring gear attachment bolts per the manufacturer's Annual/100-Hour Airframe Inspection Checklist, resulting in fatigue failure of the bolts. |
A failure of the right main landing gear wheel rim during the landing roll, resulting in a loss of control and a subsequent collapse of the right main landing gear.
The mechanic’s failure to torque check the axle-to-spring gear attachment bolts per the manufacturer's Annual/100-Hour Airframe Inspection Checklist, resulting in fatigue failure of the bolts.
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