Fatal aircraft accident during night cargo flight

2 fatalities • Soda Springs, United States of America • Flight

A cargo flight operating under VFR-on-top conditions crashed during a descent, resulting in the deaths of both crew members.

What happened

During a night cargo operation conducted under IFR conditions, the pilot requested and received clearance to descend from an altitude of 16,000 feet to fly via VFR-on-top procedures. At 21:06, the pilot confirmed awareness of the terrain along the flight path. Shortly thereafter, the aircraft performed a left turn of approximately 36 of degrees while descending through 13,800 feet, at which point radar contact was lost at 21:21:51 mdt. Air traffic controllers attempted to re-establish radio communication but were unsuccessful.

The wreckage was subsequently located roughly two miles southwest of the final radar position. The debris field spanned an area exceeding one mile. The accident resulted in two fatalities, as both pilots were killed in the crash.

Findings

Post-accident analysis determined that the left wing and the right horizontal stabilizer had separated from the airframe due to structural overload. Investigators found no evidence of pre-existing fatigue or mechanical malfunctions prior to the event. Environmental conditions at the time included moderate turbulence and towering cumulus clouds, with snow showers reported in nearby Pocatello, Idaho. The investigation concluded that the structural design stress limits of the aircraft were exceeded during the descent.

Probable cause

The aircraft's structural limits were exceeded by aerodynamic forces, leading to the separation of the wing and stabilizer.

Frequently asked questions

What happened in the 1988-04-08 Rockwell Grand Commander 680 accident near Soda Springs, United States of America?

A cargo flight operating under VFR-on-top conditions crashed during a descent, resulting in the deaths of both crew members.

Were there any fatalities in the 1988-04-08 Rockwell Grand Commander 680 accident?

The accident was fatal, resulting in 2 fatalities.

What aircraft was involved and where did it happen?

The accident on 1988-04-08 involved a Rockwell Grand Commander 680, registration N291NC, operated by Corporate Air - USA, at Soda Springs, United States of America.

What was the probable cause of the accident?

The aircraft's structural limits were exceeded by aerodynamic forces, leading to the separation of the wing and stabilizer.

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