Accident description
Last updated: 24 July 2014
Status:
Date:Friday 14 January 1966
Type:Tupolev 134
Operator:Tupolev Design Bureau
Registration: CCCP-45076
C/n / msn: 0001
First flight: 1964
Engines: 2 Soloviev D-20
Crew:Fatalities: / Occupants:
Passengers:Fatalities: / Occupants:
Total:Fatalities: 8 / Occupants: 8
Airplane damage: Damaged beyond repair
Location:near Chkalovsky (   Russia) show on map
Phase: En route (ENR)
Nature:Test
Departure airport:?
Destination airport:?
Narrative:
CCCP-45076, the second Tupolev 134 prototype crashed whilst on trials with the NII VVS.
During a test flight the pilot had turned the rudder some twenty-five degrees without reducing speed. The aircraft turned sharply, entered a dive and crashed.


Classification:
Loss of control

Sources:
» Soviet Transports
» Tupolev: The Man and His Aircraft / Andrei Kandalov, Paul Duffy , 1996 (ISBN 1560918993)


Follow-up / safety actions
After the accident the Tupolev added a limiter on the rudder control. At speed, the maximum rudder deflection was now five degrees.

Photos

photo of Tupolev 134 CCCP-45076
photo of Tupolev 134 CCCP-45076
photo of Tupolev 134 CCCP-45076
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This information is not presented as the Flight Safety Foundation or the Aviation Safety Networkĺs opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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