FIELD: transport machine building.
SUBSTANCE: control mechanism of the flap of the retractable landing gear of the aircraft comprises a chassis flap, a supporting bracket and a chassis flap control assembly. Bracket is attached to chassis flap and to aircraft structure. Control unit of chassis flap is connected with supporting flap by bracket. Control unit of chassis flap comprises located above the center line spring assembly, which facilitates rotation of bracket and flap of chassis, which it supports. Proposed aircraft comprises fuselage, chassis recesses in fuselage lower part, retractable landing gear assemblies, chassis flap assemblies and chassis flap control mechanism. Retractable landing gear assemblies are installed in retractable landing gear recesses. Units of landing gear chassis are connected with chassis niches and are made with possibility of movement between closed and open positions.
EFFECT: possibility to open chassis flap in emergency situation.
10 cl, 5 dwg
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