FIELD: transport.
SUBSTANCE: invention relates to aircraft landing systems. Tie-down hook consists of the power cylindrical case accommodating the cylinder with piston displacing therein and provided with rod. Rod extends beyond said cylinder. Free end of said rod comprises hook head to be engaged with the grating. Said head has pins to be retained in the latter. Said power cylinder is connected with pressurised medium source via control elements. Medium source includes cartridge with consumed gas.
EFFECT: decreased dimensions.
12 cl, 5 dwg
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