8 fatalities

2009-12-13: Technoavia SM-92 Turbo Finist (RA-0257G) — Chelavia — Kalachevo, Russia

Kalachevo, RussiaTakeoff (climb)

On December 13, 2009, a Technoavia SM-92 Turbo Finist (registration RA-0257G) operated by Chelavia was involved in an aviation accident near Kalachevo, Russia during takeoff. 8 people were killed. Investigators recorded the probable cause as: The aircraft entered a stall during the initial climb due to exceeding maximum takeoff weight and failing to maintain proper climb speeds. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781196376Data APIEditorial standards
Aircraft registered RA-0257G
Aircraft registered RA-0257G. Photo: SkyBon / Public domain, via Wikimedia Commons

A single-engine aircraft crashed shortly after takeoff from Kalachevo Airport, resulting in the deaths of all eight people on board.

What happened

On a flight operating out of Kalachevo Airport, located approximately 24 km south of Chelyabinsk, a single-engine aircraft was performing routine skydiving missions. During the initial climb phase, while the plane had reached an altitude of roughly 100 meters, it experienced a stall. The aircraft subsequently crashed into a field covered in snow, situated about 1.5 km north of the airport runway.

The impact resulted in the total destruction of the single-engine aircraft. There were no survivors among the 8 fatalities recorded during the incident.

Findings

Investigations into the crash identified several contributing elements that led to the loss of control. The primary cause was a stall occurring during the climb, which was driven by multiple operational failures:

  • The crew failed to adhere to established climb procedures regarding airspeed.
  • The aircraft's performance capabilities were insufficient because it was being utilized for skydiving operations despite not being configured for that specific mission profile.
  • The aircraft was operating at a total weight that exceeded its maximum takeoff weight (MTOW).
  • There was an absence of an onboard warning system to alert the pilot to an impending stall.
  • The stall occurred at such a low altitude that the pilot had no opportunity to execute recovery maneuvers.

Probable cause

The aircraft entered a stall during the initial climb due to exceeding maximum takeoff weight and failing to maintain proper climb speeds.