An apparatus for testing an aircraft Elevator Feel Computer (EFC), comprising:
- a test box including a housing having a base and a first cover attached to the base;
- an interface panel mounted on the base to define a base enclosure;
- an electrical power supply interface including a power on-off switch and an electrical connector for connecting the apparatus to an electrical power cable;
- a pressurized air delivery subsystem including:
- an air pump disposed entirely within the base enclosure;
- a regulated air port in selectable fluid communication with the air pump, the regulated air port disposed through the interface panel;
- a pressure regulator to adjustably regulate an air pressure delivered through the regulated air port, the pressure regulator including a pressure regulator knob, located on the interface panel, for adjusting the air pressure delivered through the regulated air port;
- a pump power switch disposed on the interface panel to selectably close an electrical power circuit that delivers electrical power to the air pump and to indicate whether or not the electrical power circuit is energized;
- a shut off valve having a shut off valve knob disposed on the interface panel wherein the shut off valve is to selectably block the pressurized air from being delivered from the air pump to the regulated air port;
- and
- a pressure relief valve disposed on the interface panel, the pressure relief valve to selectably exhaust pressurized air in a pneumatic circuit within the base enclosure, the pneumatic circuit connected to the regulated air port;
- a two-channel pneumatic pressure measurement subsystem including:
- a first air inlet connector disposed on the interface panel, the first air inlet connector to connect to a first visco drain in fluid communication with the first pitot probe;
- a first pneumatic circuit to fluidically connect the first air inlet connector to a first pitot pressure gage to indicate a first pneumatic pressure in the first pneumatic circuit;
- a second air inlet connector disposed on the interface panel, the second air inlet connector to connect to a second visco drain in fluid communication with a second pitot probe;
- and
- a second pneumatic circuit to fluidically connect the second air inlet connector to a second pitot pressure gage to indicate a second pneumatic pressure in the second pneumatic circuit;
- a two-channel hydraulic pressure measurement subsystem including:
- a first electrical connector disposed on the interface panel, the first electrical connector to connect to a first hydraulic transmitter;
- a first electrical circuit defined within the base enclosure to electrically connect the first electrical connector to a first hydraulic pressure display to indicate a first hydraulic pressure;
- a second electrical connector disposed on the interface panel, the second electrical connector to connect to a second hydraulic transmitter;
- and
- a second electrical circuit to electrically connect the second electrical connector to a second hydraulic pressure display to indicate a second hydraulic pressure.