N8262 - 2013 Charles D Walker Walker Curtiss JN4D Aircraft Registration
SA042013 CHARLES D WALKER WALKER CURTISS JN4D
Aircraft Description
N8262 is a 2013 Charles D Walker WALKER CURTISS JN4D, a single-engine reciprocating (piston) aircraft registered to Freestar Fiancial Credit Union in Mount Clemens, MI. This aircraft holds a experimental airworthiness certificate issued by the Federal Aviation Administration on August 6, 2013. The registration certificate was issued on February 14, 2024. The registration is set to expire on February 28, 2031. Powered by a Gm ECO TEC 2.4L engine producing 182 horsepower, N8262 is. The aircraft's Mode S transponder code is AB49C3 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N8262 was last updated on February 14, 2024. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Charles D Walker is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 1 Charles D Walker aircraft currently registered in the FAA database, including the WALKER CURTISS JN4D model.
AviatorDB has found no NTSB accident or incident reports involving N8262. 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 |
|---|---|---|---|---|
| May 15, 2023 | ERA23LA231 | Substantial | None | The separation of an electrical wire that powered the ignition module, rendering the ignition system inoperative, and resulting in the total loss of engine power. |
| Aug 12, 2017 | GAA17CA488 | Substantial | Minor | The pilot’s exceedance of the biplane’s critical angle of attack during initial climb, which resulted in an aerodynamic stall and collision with trees. |
The separation of an electrical wire that powered the ignition module, rendering the ignition system inoperative, and resulting in the total loss of engine power.
The pilot’s exceedance of the biplane’s critical angle of attack during initial climb, which resulted in an aerodynamic stall and collision with trees.
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