4 fatalities

Antonov An-2TP Crash After Takeoff from Naryan-Mar (RA-01460)

Naryan-Mar, RussiaTakeoff (climb)

On December 19, 2017, a PZL-Mielec AN-2 (registration RA-01460) operated by Naryan-Mar Air Enterprise - Naryan-Marskoe Aviapredpriatie was involved in an aviation accident near Naryan-Mar, Russia during takeoff. 4 people were killed. Investigators recorded the probable cause as: Loss of control during initial climb due to the combination of an excessive weight (the total weight of the aircraft was 42 kilos above MTOW) and a CofG that was too far aft, well above the permissible limit (32%). Poor flight preparation. 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 1781191610Data APIEditorial standards
Aircraft registered RA-01460
Aircraft registered RA-01460. Photo: Alan Wilson / CC BY-SA 2.0, via Wikimedia Commons

An Antonov An-2TP converted with a turbine engine crashed shortly after takeoff from Naryan-Mar Airport, resulting in four fatalities and multiple injuries. The probable cause was loss of control due to excessive weight and aft center of gravity.

Accident Details

On an unspecified date, an Antonov An-2TP (converted in 2014 with a Honeywell TPE331 turbine engine) operating as flight NYA9280 departed Naryan-Mar Airport on a scheduled service to Kharuta, Republic of Komi. The aircraft carried 11 passengers and two pilots. Shortly after takeoff, while climbing to a height of 30-40 metres, the aircraft entered an excessive nose-up attitude, then rolled to the right, stalled, and crashed in a snow-covered field.

Casualties

One passenger was killed in the initial impact. Twelve other occupants were injured. Later in the evening, two additional passengers died from their injuries, and a fourth passenger passed away on 10 January 2018.

Probable Cause

The official investigation determined that the probable cause was loss of control during initial climb due to a combination of excessive weight (the total weight of the aircraft was 42 kilograms above maximum takeoff weight) and a center of gravity that was too far aft, well above the permissible limit (32%). Poor flight preparation was also cited.