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ATA 32 landing gear control computers
ATA 32 Landing, braking and steering control systems
ATA 32 landing gear control computers
Fault detection BITE
Software download via Ethernet
The ATA 32 landing gear control units contribute to the optimum control of all landing gear parameters during taxiing, take-off and landing phases.
ATA 32 landing gear control computers
Fault detection BITE
Software download via Ethernet
Fully modular architecture
A level of redundancy adapted to your needs
Enhanced flight safety
High-performance landing gear command and control systems
Highly efficient, our command and control solutions ensure an optimum management of all the landing gear essential functions: braking parameter monitoring, landing gear extension and retraction kinematic control, nose wheel steering command. They also provide the crew with real-time information on a set of parameters, enhancing flight safety.
Modularity and versatility to all requirements
Our landing gear control systems manage many parameters as the tire pressure, brake temperature, wheel tachometry, slaving of the nose wheel deflection angle, anti-lock braking, landing gear extension and retraction kinematics, coordinated opening and closing of the doors or Built-in fault diagnostic (BITE), etc.
- © Safran
- © Safran Electronics & Defense
- © Philippe Stroppa / Safran
- © Christian Fleury / CAPA Pictures / Safran