Aircraft Description
N6748V is a 1980 Beech 58TC, a twin-engine reciprocating (piston) aircraft registered to Cannon Oil & Gas Well Services INC in Rock Springs, WY. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on March 19, 1980. The registration certificate was issued on September 24, 2007. The registration is set to expire on April 30, 2028. Powered by a Cont Motor TSIO-520 SER engine producing 300 horsepower, N6748V is. The aircraft's Mode S transponder code is A8EE18 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N6748V was last updated on May 5, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Beechcraft Baron 58 became one of general aviation's most successful light twin-engine aircraft, establishing itself as the preferred choice for owner-operated business aviation. First flown on June 23, 1969, it was a low-wing twin-engine monoplane powered by two Continental IO-520 piston engines, each producing 285 horsepower, with seating for four to six passengers. Spanning 37 feet 10 inches with an overall length of 29 feet 10 inches, the aircraft achieved a cruising speed of 200 miles per hour and a range exceeding 1,000 miles. Originally manufactured by Beech Aircraft Corporation, production continued for 34 years until 2004. AviatorDB tracks 18,376 Beech aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is BE58.
AviatorDB has found no NTSB accident or incident reports involving N6748V. 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 |
|---|---|---|---|---|
| Oct 11, 2021 | CEN22FA011 | Destroyed | Fatal | The maintenance personnel’s failure to properly tighten the turbocharger oil line and the right engine propeller governor, which resulted in a loss of engine power. Contributing to the accident was the loss of airplane control following the loss of engine power. |
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