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Crash of an Ilyushin II-114T in Moscow: 5 killed

Date & Time: Dec 5, 1999 at 0512 LT
Type of aircraft:
Operator:
Registration:
UK-91004
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Moscow - Tashkent
MSN:
10838 00305
YOM:
1998
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Aircraft flight hours:
240
Aircraft flight cycles:
123
Circumstances:
While taxiing at Moscow-Domodedovo Airport, the aircraft encountered strong crosswinds and the rudder got stuck in the full left position. The flight engineer suggested the captain to return to the apron to proceed to an inspection but the pilot prefered to takeoff. After liftoff from runway 32L, while climbing to a height of about 24 metres, the aircraft went out of control and crashed in a wooded area located 365 metres past the runway end. Two occupants were seriously injured and five others were killed.
Probable cause:
It was determined that the rudder was blocked in the full left position prior to takeoff, probably due to the strong crosswinds encountered during the taxi procedure.

Crash of an Ilyushin II-114 in Moscow: 7 killed

Date & Time: Jul 5, 1993
Type of aircraft:
Operator:
Registration:
RA-54001
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Moscow - Moscow
MSN:
01-03
YOM:
1989
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The aircraft was engaged in a local test flight, carrying nine engineers and pilots. Shortly after takeoff from Moscow-Zhukovsky Airport, while climbing to a height of 45 metres, the right propeller autofeathered. The aircraft started to roll left and right then reached a critical angle of attack. Out of control, it stalled and crashed 400 metres past the runway end, bursting into flames. Two people were seriously injured while seven others were killed. The aircraft was supposed to perform a series of five 7-minutes flights to test the noise from ground. At the time of the accident, the total weight of the aircraft was near the limit.
Probable cause:
It was determined that the right engine autofeathered immediately after lift-off due to an electronic malfunction.