FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft landing gear well control mechanism. Device comprises first retainer secured to landing gear well, second retainer secured to well to partially turn thereabout and to landing gear well flap. Note here that said first and second retainers are interconnected to turn simultaneously in opposite directions while turn of both said retainers opens or closes landing gear well.
EFFECT: simplified design.
19 cl, 7 dwg
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