Aircraft Description
N9531Y is a Beech P35, a single-engine reciprocating (piston) aircraft registered to White Bill E in Estacada, OR. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on July 17, 1962. The registration certificate was issued on September 15, 2018. The registration is set to expire on September 30, 2028. Powered by a Cont Motor I0-470 SERIES engine producing 260 horsepower, N9531Y is. The aircraft's Mode S transponder code is AD425E (hex), used for ADS-B identification and flight tracking. The FAA registry record for N9531Y was last updated on June 10, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Beechcraft Model 35 Bonanza revolutionized personal aviation as the first modern all-metal general aviation aircraft, introducing features that became industry standards. First flown on December 22, 1945, it was a low-wing single-engine monoplane that seated four to six occupants with its distinctive V-tail configuration. Measuring 26 feet long with a 33-foot wingspan, the aircraft achieved cruise speeds up to 200 knots during its production run. Manufactured by Beech Aircraft Corporation from 1947 to 1982, over 10,000 Model 35 variants were produced. AviatorDB tracks 18,376 Beech aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is BE35.
AviatorDB has found no NTSB accident or incident reports involving N9531Y. 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 |
|---|---|---|---|---|
| Aug 18, 1995 | SEA95LA186 | Substantial | None | seizure of the #4 connecting rod bearing due to overtemperature resulting in the separation of the connecting rod and total loss of engine power. A factor contributing to the accident was the lack of suitable terrain for a forced landing. |
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