Aircraft Description
N22932 is a 1946 Grumman G-21A, a twin-engine reciprocating (piston) aircraft registered to Runyon Aviation LLC in Fort Worth, TX. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on July 17, 1978. The registration certificate was issued on October 9, 2025. The registration is set to expire on October 31, 2032. Powered by a P&w R-985 SERIES engine producing 450 horsepower, N22932 is. The aircraft's Mode S transponder code is A2054C (hex), used for ADS-B identification and flight tracking. The FAA registry record for N22932 was last updated on October 9, 2025. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Grumman Aircraft (later Northrop Grumman) was a major American aircraft manufacturer known for naval fighters in World War II and the Apollo Lunar Module. In general aviation, the Grumman American AA-5 and Tiger series remain popular sport aircraft. AviatorDB tracks 473 Grumman aircraft currently registered in the FAA database, including the G-21A model.
AviatorDB has found no NTSB accident or incident reports involving N22932. 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 (3)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Apr 5, 2004 | ANC04LA038 | Substantial | None | The inadvertent ground loop/swerve by the second pilot during the landing roll, and the first (check) pilot's inadequate supervision of the second pilot, which resulted in a loss of control and substantial damage to the airplane. Factors associated with the accident are the second pilot's improper upgrade/transition training by the company check airman, the second pilot's lack of experience in the accident type airplane, the operator's lack of surveillance of the training process, and a crosswind. |
| Apr 15, 1998 | ANC98LA038 | Substantial | None | The pilot-in-command's failure to identify the swells prior to landing. A factor was the water swells. |
| Jan 7, 1993 | ANC93IA026 | MINR | None | THE INCIDENT WAS CAUSED BY THE PILOTS IMPROPER COMPENSATION FOR THE WINDS. FACTORS WERE THE MICROBURST, THE ROUGH WATER, AND THE PILOT'S INADEQUATE EVALUATION OF THE WEATHER CONDITIONS. |
The inadvertent ground loop/swerve by the second pilot during the landing roll, and the first (check) pilot's inadequate supervision of the second pilot, which resulted in a loss of control and substantial damage to the airplane. Factors associated with the accident are the second pilot's improper upgrade/transition training by the company check airman, the second pilot's lack of experience in the accident type airplane, the operator's lack of surveillance of the training process, and a crosswind.
The pilot-in-command's failure to identify the swells prior to landing. A factor was the water swells.
THE INCIDENT WAS CAUSED BY THE PILOTS IMPROPER COMPENSATION FOR THE WINDS. FACTORS WERE THE MICROBURST, THE ROUGH WATER, AND THE PILOT'S INADEQUATE EVALUATION OF THE WEATHER CONDITIONS.
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