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Estado:
Fecha:martes 21 diciembre 1976
Tipo:Silhouette image of generic AN22 model; specific model in this crash may look slightly different
Antonov An-22A
Operador:Soviet Air Force
Registración: CCCP-09318
Numéro de série: 03340501
Año de Construcción: 1973
Motores: 4 Kuznetsov NK-12MA
Tripulación:Fatalidades: 7 / Ocupantes: 7
Pasajeros:Fatalidades: 0 / Ocupantes: 0
Total:Fatalidades: 7 / Ocupantes: 7
Daños en la Aeronave: Destruido
Consecuencias: Written off (damaged beyond repair)
Ubicación:cerca Seshcha (   Rusia)
Fase: Maniobras (MNV)
Naturaleza:Prueba
Aeropuerto de Salida:Seshcha-Br'ansk AFB, Rusia
Aeropuerto de Llegada:Seshcha-Br'ansk AFB, Rusia
Descripción:
During a test flight out of Br'ansk AFB, the Antonov made a turn with maximum rudder deflection. At an altitude of 6000 m the plane entered a slip. The captain manoeuvred the plane in an attempt not to lose height, but the Antonov attained a critical angle of attack. It entered a spin and broke up in the air.

Fuentes:
» Scramble 154, Scramble 286
» Soviet Transports
» vta81vtap.narod.ru
» airdisaster.ru


Subsiguiente / acciones de seguridad
Following this accident Antonov limited the rudder deflection angle on their An-22 and recommended that pilots not use the rudders during turns when ailerons could be sufficient.

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This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s 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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