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Status:
Datum:dinsdag 21 december 1976
Type:Silhouette image of generic AN22 model; specific model in this crash may look slightly different
Antonov An-22A
Luchtvaartmaatschappij:Soviet Air Force
Registratie: CCCP-09318
Constructienummer: 03340501
Bouwjaar: 1973
Motoren: 4 Kuznetsov NK-12MA
Bemanning:slachtoffers: 7 / inzittenden: 7
Passagiers:slachtoffers: 0 / inzittenden: 0
Totaal:slachtoffers: 7 / inzittenden: 7
Schade: Vernield
Gevolgen: Written off (damaged beyond repair)
Plaats:nabij Seshcha (   Rusland)
Fase: Manoeuvreren (MNV)
Soort vlucht:Test
Vliegveld van vertrek:Seshcha-Br'ansk AFB, Rusland
Vliegveld van aankomst:Seshcha-Br'ansk AFB, Rusland
Beschrijving:
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.

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


Veiligheidsmaatregelen
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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