• ARP5007

• 1997-06-01

• Historical. Access the latest revision: ARP5007A

• A-6a3 Flight Control Systems Committee

This document provides a description of a process for development of fly-by-wire actuation systems. Included are (1) the development of requirements for the servo-actuator hardware, and the electronics hardware and software, (2) actuator and servo-electronics interface definitions and, (3) the required communications and interactions between the servo-actuator and the servo-electronics designers.

• SAE ARP 5007

• Aerospace

• Flight control systems
• Flight control actuators
• Fly-by-wire control systems
• Flight management systems
• Sensors and Actuators
• Parts
• Fluid power systems
• Hydraulic systems
• Electrohydraulics
• Hydraulic control
• Hydraulic drives
• Hydraulic equipment
• Hydraulic fittings
• Hydraulic fluids
• Hydraulic motors
• Fuel pumps
• Safety
• Tests and Testing
• Military aircraft
• Unmanned aerial vehicles