No fatalities

23 Jun 2011: BEECH B36TC (N93PP) — Arizona Thunderbolts LLC — Akron, CO

Akron, CO, United States

On 23 Jun 2011, a BEECH B36TC (registration N93PP) operated by Arizona Thunderbolts LLC was involved in an aviation accident near Akron, CO. No fatalities were reported. Investigators recorded the probable cause as: The mixture control cable disconnected from the cable housing attach clamp, which resutlted in the pilot's inability to add power when needed. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On June 23, 2011, a Beech B36TC (N93PP) impacted terrain short of the runway at Colorado Plains Regional Airport, Colorado, after the engine failed to respond to power application during landing. The pilot and passenger sustained minor injuries; the aircraft was substantially damaged. Investigation revealed a disconnected mixture control cable.

Accident Overview

On June 23, 2011, at approximately 0915 mountain daylight time, a Beech B36TC aircraft, registration N93PP, impacted terrain short of the runway at Colorado Plains Regional Airport (AKO) in Akron, Colorado. The airplane was registered to and operated by Arizona Thunderbolts LLC of Phoenix, Arizona, under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed at the time, and no flight plan had been filed. The flight originated from Yuma (2V6), Colorado, at about 0900 and was en route to AKO.

Pilot Account and Damage

According to the pilot, he reduced power for landing because he was slightly high. When he added power to arrest the descent, the engine failed to respond. The airplane subsequently landed short of the runway. The impact drove the main landing gear through the right wing. The pilot and the passenger onboard sustained minor injuries, and the airplane was substantially damaged.

Post-Accident Examination

During a functional test of the engine, the engine was started using high boost prime. When low boost was selected, the engine quit. A second examination revealed that the mixture control cable was disconnected from the cable housing attach clamp. When the mixture control was moved inside the cockpit, the cable and housing moved together. The mixture control cable was reconnected and the engine was functionally tested again. The engine operated at all power settings, from idle to 2,800 rpm, and mixture adjustments were made with no anomalies noted.

Contributing factors

Inoperative