Special Features:

Used to test aircraft hydraulic and pneumatic components such as engine-driven hydraulic pumps, electro-hydraulic flight control assemblies, hydraulic and pneumatic relief valves, hydraulic-pneumatic accumulators and other components

Properties:

A cabinetlike item usually with a front work area and consisting of the necessary instrumentation, mechanical and electrical facilities for component mounting. Designed to test efficiency of packaged hydraulic and pneumatic pressure and electric power generating equipment. Component under test is equipped with self contained power source. Excludes test stand, hydraulic system component; test stand, electric; and hydraulic system components.