• SAE ARP5007A

SAE ARP5007A

  • Development Process - Aerospace Fly-By-Wire Actuation System
  • standard by SAE International, 04/26/2012
  • Category: SAE

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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.
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SAE AMS3801/3C

SAE AMS3801/3C

Cloth, Parachute, Meta-Aramid, Low Modulus 12.0(407) Weight, Special Weave (Stabilized: Oct 2016)..

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SAE AMS3801/4C

SAE AMS3801/4C

Cloth, Parachute, Meta-Aramid, Low Modulus 7.0 (237) Weight, Plain Weave (Stabilized: Oct 2016)..

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SAE AMS3801/5C

SAE AMS3801/5C

Cloth, Parachute, Meta-Aramid, Low Modulus 18.0 (610) Weight, Basket Weave, Resin Treated (Stabilize..

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SAE AS85049/133

SAE AS85049/133

CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, 90¿¿, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIE..

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