Our steering control unit controls of the nose landing gear. It receives crew commands from the cockpit, both from tillers and from the rudder pedals. It monitors the position of the landing gear and signals from aircraft systems so that interlocks can be implemented if required.
Compact, lightweight and reliable
Up to Design Assurance Level A - hardware and software
ARINC 2MCU construction
Control Lane architecture to suit any customer requirement
Fully automatic Built-in-Test capability to monitor the health of its own circuits
Convection cooled - forced air cooling is not required
Configurable to perform additional functions such as backup hydraulic control and brake temperature monitoring
Power supply: 28VDC
Power consumption: 20W
Software: DO-178 Level A
Hardware: DO-254 Level A
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