FIELD: ammunition.
SUBSTANCE: invention relates to aircraft ammunition, particularly to anti-submarine air bombs. In compliance with this invention, proposed method comprises disconnecting container with parachute system from the bomb bottom face sleeve. Temporary plug is fitted in the sleeve central orifice to lock inner carcass components. Outer bands and head plate are removed and inner carcass with explosive charge is withdrawn from the casing. Head sleeve is withdrawn from the carcass front part, while flange and disk are withdrawn from the carcass rear part. Now, the container is broken down, parachute system is detached therefrom and bomb assemblies and parts are separated in compliance with the material they made in.
EFFECT: lower costs and safe partial disassembly.
5 dwg, 1 ex
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