our products

characteristics

OMA equips fighter and trainer aircraft with equipment designed and manufactured in-house for use on flight control systems:

• Air Brake Systems integrate a control valve package equipped with a servovalve, a swivel manifold, a hydraulic actuator, an internal LVDT and the appropriate piping. The system is developed to support the implementation of a dual redundant, closed loop, fly-by-wire architecture.
• Pilot Input Transducer able to provide the interface between aircraft control stick and pedal linkages and the Flight Control Computers, equipped with the anti-backlash feature, jam clearance torque system, four redundant independent, single channel, Rotary Variable Differential Transformer (RVDT).
• Engine Throttle Input Transducers able to provide the interface between the mechanical movement of the engine throttle and the electric output to the flight control computer to allow the pilot control on the engine thrust.