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ATA 32 Landing, braking and steering control systems

Landing Braking Systems Airbus A350 XWB

ATA 32 landing gear control computers

Safran Electronics & Defense

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

Product Aircraft electronic equipment and critical software

Safran Electronics & Defense

Fault detection BITE

Software download via Ethernet

Fully modular architecture

A level of redundancy adapted to your needs

 Enhanced flight safety

+ 25
million accumulated flight hours
Analog brake control unit in cicuit test

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.
 

Installation of electronic cards for the electronic calculator EBAC

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 Electronics & Defense
  • © Philippe Stroppa / Safran
  • © Christian Fleury / CAPA Pictures / Safran