No fatalities

1983-02-15: De Havilland DHC-6 Twin Otter (N361V) — Sierra Pacific Airlines - SPA — Hailey-Friedman Memorial, United States of America

Hailey-Friedman Memorial, United States of AmericaLanding (descent or approach)

On February 15, 1983, a De Havilland DHC-6 Twin Otter (registration N361V) operated by Sierra Pacific Airlines - SPA was involved in an aviation accident near Hailey-Friedman Memorial, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The in-flight loss of elevator control following separation of the control rod from the torque tube at a connection where the company's maintenance department had used a non-standard, unsecured bolt, which the company's inspection department had failed to… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781220744Data APIEditorial standards

On February 15, 1983, a Sierra Pacific Airlines DHC-6 crashed during approach to Hailey, Idaho, after losing elevator control. One passenger suffered minor injuries; others were seriously injured.

Accident Overview

On February 15, 1983, at approximately 1100 Mountain Standard Time, a Sierra Pacific Airlines DHC-6 twin-engine aircraft, operating as Transwestern Flight 868, crashed during its final approach to runway 31 at Friedman Memorial Airport in Hailey, Idaho. The accident occurred 1.7 miles south of the airport. The aircraft was destroyed by impact forces, though no fire ensued.

Flight Details

Flight 868 was a regularly scheduled commuter passenger flight from Boise to Hailey, Idaho. On board were two flightcrew members and six passengers. Following the crash, one passenger escaped with minor injuries, while the other seven occupants sustained serious injuries.

Sequence of Events

While approximately 800 feet above the small town of Bellevue, about 2 miles south of the airport, the captain reduced power to configure the aircraft for its final approach. Immediately thereafter, the captain realized that elevator control had been lost. The aircraft nosed over and descended steeply. The captain attempted to control the pitch by adding power, and the aircraft began to recover. However, it crash landed on a highway in a slight nose-down attitude with the right wing slightly lowered. After touching down, the aircraft veered off the highway, struck a 4-foot-high snowbank, and broke apart.

Probable Cause

The official probable cause was the in-flight loss of elevator control following separation of the control rod from the torque tube at a connection where the company's maintenance department had used a non-standard, unsecured bolt, which the company's inspection department had failed to detect. Contributing to the accident was the company's failure to maintain the separation of maintenance and inspection functions required by the maintenance program approved by the Federal Aviation Administration, and the failure of the FAA to detect the company's deviation from approved maintenance procedures during surveillance inspection.