Single-engine aircraft crash during oil exploration mission

No fatalities • Tadebyayakha, Russia • Takeoff (climb)

A single-engine aircraft carrying 22 passengers and crew crashed in a snow-covered field after failing to maintain altitude following takeoff.

What happened

During an expedition focused on oil exploration, a single-engine aircraft was operating with a total of 22 people on board, including two pilots and 20 scientists and geologists. Shortly after departing, the aircraft struggled to establish sufficient climb performance. The plane subsequently entered a stall and descended into a field covered in snow.

Despite the impact, all 22 occupants were successfully rescued from the wreckage. While there were no fatalities, the aircraft sustained damage that rendered it a total loss.

Findings

Investigations into the accident revealed critical weight and balance discrepancies. The aircraft was operating significantly over its maximum allowable limits, with the total weight recorded at 831 kilos above the maximum takeoff weight. Additionally, the center of gravity was positioned 6.8% behind the permitted aft limit, which contributed to the loss of control.

Probable cause

The accident was caused by the aircraft being operated significantly above its maximum takeoff weight and with an improper center of gravity.

Frequently asked questions

What happened in the 1985-05-21 Antonov AN-2 accident near Tadebyayakha, Russia?

A single-engine aircraft carrying 22 passengers and crew crashed in a snow-covered field after failing to maintain altitude following takeoff.

Were there any fatalities in the 1985-05-21 Antonov AN-2 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1985-05-21 involved a Antonov AN-2, registration CCCP-04326, operated by Aeroflot - Russian International Airlines, at Tadebyayakha, Russia.

What was the probable cause of the accident?

The accident was caused by the aircraft being operated significantly above its maximum takeoff weight and with an improper center of gravity.

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