FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to sea planes. Proposed device comprises searchlight mounted on the bar, translational electric mechanism and wiring of circuit that controls flaps opening/closing and searchlight extension/retraction connected therewith. Electric mechanism housings can be disconnected from wiring elements in case the latter fail. Said housings have yokes with openings rigidly secured thereon. Said yokes allow fastening said housing to bracket arranged on airframe, in the case of flaps opening/closing electric mechanism, or to said bracket secured onto searchlight bar in retracted position, in the case of searchlight extension/retraction mechanism.
EFFECT: simplified repair and design.
3 dwg
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