Tbilisi - Omsk - Irkutsk - Komsomolsk-on-Amur

Following a wrong approach configuration, the twin engine aircraft passed over the runway threshold at a height of 20 meters. At a distance of 300 meters from the runway end, the flight engineer (who was acting as a copilot on this flight) reduced power on both engines above idle. The captain took over control, increased engine power at maximum and initiated a go-around procedure when the left engine autofeathered. At a speed of 170 km/h, the aircraft banked left to an angle of 70° then stalled and crashed 1,526 meters past the runway end. Seven occupants were injured while two others, including one pilot, were killed.

Flight / Schedule

Tbilisi - Omsk - Irkutsk - Komsomolsk-on-Amur

Aircraft

Antonov AN-8

Registration

CCCP-13330

MSN

133430

Year of Manufacture

1961

Date

May 16, 1991 at 12:00 AM

Type

CRASH

Flight Type

Cargo

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Irkutsk-2 (Northwest/Vostochny) Irkutsk oblast

Region

Asia • Russia

Crash Cause

Human factor

Narrative Report

On May 16, 1991 at 12:00 AM, Tbilisi - Omsk - Irkutsk - Komsomolsk-on-Amur experienced a crash involving Antonov AN-8, operated by MAP - Ministerstvo Aviatsionnoi Promyshlennosti - Minaviaprom, with the event recorded near Irkutsk-2 (Northwest/Vostochny) Irkutsk oblast.

The flight was categorized as cargo and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

9 people were known to be on board, 2 fatalities were recorded, 7 survivors were identified or estimated. This corresponds to an estimated fatality rate of 22.2%.

Crew on board: 6, crew fatalities: 1, passengers on board: 3, passenger fatalities: 1, other fatalities: 0.

The listed crash cause is human factor. Following a wrong approach configuration, the twin engine aircraft passed over the runway threshold at a height of 20 meters. At a distance of 300 meters from the runway end, the flight engineer (who was acting as a copilot on this flight) reduced power on both engines above idle. The captain took over control, increased engine power at maximum and initiated a go-around procedure when the left engine autofeathered. At a speed of 170 km/h, the aircraft banked left to an angle of 70° then stalled and crashed 1,526 meters past the runway end. Seven occupants were injured while two others, including one pilot, were killed.

Aircraft reference details include registration CCCP-13330, MSN 133430, year of manufacture 1961.

Fatalities

Total

2

Crew

1

Passengers

1

Other

0

Crash Summary

Following a wrong approach configuration, the twin engine aircraft passed over the runway threshold at a height of 20 meters. At a distance of 300 meters from the runway end, the flight engineer (who was acting as a copilot on this flight) reduced power on both engines above idle. The captain took over control, increased engine power at maximum and initiated a go-around procedure when the left engine autofeathered. At a speed of 170 km/h, the aircraft banked left to an angle of 70° then stalled and crashed 1,526 meters past the runway end. Seven occupants were injured while two others, including one pilot, were killed.

Cause: Human factor

Occupants & Outcome

Crew On Board

6

Passengers On Board

3

Estimated Survivors

7

Fatality Rate

22.2%

Known people on board: 9

Operational Details

Schedule / Flight

Tbilisi - Omsk - Irkutsk - Komsomolsk-on-Amur

Flight Type

Cargo

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

Asia • Russia

Aircraft Details

Aircraft

Antonov AN-8

Registration

CCCP-13330

MSN

133430

Year of Manufacture

1961