Aircraft Description
N415JB is a 1999 Aviat Aircraft INC A-1A, a single-engine reciprocating (piston) aircraft registered to Brewer Allen E in Madison, MS. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on December 7, 1999. The registration certificate was issued on February 22, 2005. The registration is set to expire on July 31, 2029. Powered by a Lycoming O&VO-360 SER engine producing 180 horsepower, N415JB is. The aircraft's Mode S transponder code is A4E77D (hex), used for ADS-B identification and flight tracking. N415JB was last tracked by AviatorDB at coordinates 32.3159, -90.1945 on February 22, 2026. The FAA registry record for N415JB was last updated on August 18, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Aviat A-1 Husky is a high-wing utility aircraft that modernized bush flying through advanced short takeoff and landing capabilities. First flown in 1986, it was a high-wing single-engine monoplane powered by a 180-horsepower Lycoming O-360 engine that could seat two occupants. With a top speed of 145 mph and a stall speed of just 53 mph, it was manufactured by Christen Industries and later Aviat Aircraft. AviatorDB tracks 971 Aviat Aircraft INC aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is HUSK.
AviatorDB has found no NTSB accident or incident reports involving N415JB. 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 |
|---|---|---|---|---|
| Jan 11, 2003 | ATL03LA035 | Substantial | None | The pilot's failure to maintain directional control during landing roll which resulted in a loss of control and collision with a ditch. A factor was separation of the spring clip from the landing gear steering system. |
| Jul 6, 2000 | MIA00LA216 | Substantial | None | The pilot's failure to maintain directional control of the airplane during landing flare into a crosswind, resulting in a runway excursion off the runway edge and collision of the wingtip with the terrain. |
The pilot's failure to maintain directional control during landing roll which resulted in a loss of control and collision with a ditch. A factor was separation of the spring clip from the landing gear steering system.
The pilot's failure to maintain directional control of the airplane during landing flare into a crosswind, resulting in a runway excursion off the runway edge and collision of the wingtip with the terrain.
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