Our landing gear control unit controls the movement of the landing gear structure and the landing gear doors. It receives crew commands from the cockpit, monitors the position of the landing gear and controls the hydraulic extension and retraction system to move the gear up or down.
Small, lightweight and reliable
Weight-on-wheels functionality
Design Assurance Level A -hardware and software
ARINC 2MCU construction
Two mechanically separate, independent and redundant control lanes
Controller can be configured to perform additional functions such as Nosewheel Steering and brake temperature monitoring
Convection cooled - forced air cooling is not required
Our controllers are fitted to the following civil aircraft:
Jet Military planes with Eaton PCS landing gear control include:
| Power supply: | 28VDC |
Power consumption: |
20W |
Software: |
DO-178 Level A |
Hardware: |
DO-254 Level A |
发送电子邮件
MyEatonFAQs
