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Full Description

This AIR provides descriptions of aircraft actuation system failure-detection methods. The methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight control. The AIR concentrates on full Fly-By-Wire (FBW) flight control actuation, but also includes one augmented-control system.

The purpose of this document is to aid the designers of the systems of the future by showing what succeeded in the past.
 

Document History

  1. SAE AIR5273A


    Aircraft Flight Control Actuation System Failure-Detection Methods

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  2. SAE AIR5273

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    Actuation System Failure Detection Methods

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