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The purpose of this AIR is to provide a comprehensive description document that displays various examples of low pressure seals and wipers utilized within mechanical and electromechanical actuators. The document is intended as an overview for those specifying or designing actuators in order to compare existing solutions as reference for implementation.

Failures due to moisture ingress to vulnerable electrical and mechanical equipment are not uncommon on aircraft and in test programs. This Aerospace Information Report aims to inform the aerospace community of considerations to be taken regarding potential moisture damage in the design of EM actuation equipment.

This Recommended Practice provides a guide for specifying general design, performance, and test requirements for power drive units (PDUs) for flight controls and other applications.

This SAE Aerospace Recommended Practice (ARP) shall provide guidelines for the maintenance, inspection, and support of rotary and linear mechanical actuators on in-service and aging aircraft.

Most of the Trimmable Horizontal Stabilizer Actuators (THSA) feature a dual structural load path, the primary load path being loaded, the secondary load path being normally unloaded, or both load paths sharing in parallel the Horizontal Stabilizer load. This document describes existing methods for detecting rupture or disconnection of loaded load paths as an overview for those specifying or designing Horizontal Stabilizer Trim Actuators in order to compare existing solutions as reference for implementation in new aircraft programs.

This Aerospace Information Report provides examples of single mechanical failure modes for components used in fixed wing, high lift actuation systems’ load paths, as well as the typical hazards posed by those failures at the aircraft level.

This Aerospace Information Report provides an overview of published data on different methods for designing electromechanical actuators with a very low probability of jam or disconnect.

This project will create an Aerospace Recommended Practice that provides comprehensive guidelines for the design and specifications for rotary and linear mechanical actuators for use in aircraft mechanically distributed actuation systems including but not limited to flap, slat , cargo door, and weapons bay door actuators.

This Aerospace Recommended Practice (ARP) provides general guidelines for defining a specification for an EMA motor. This document is tailored specifically for permanent magnet brushed and brushless motors.

This SAE Aerospace Information Report (AIR) provides descriptions of trimmable horizontal stabilizer actuators that are installed on a variety of transport and business aircraft systems.

The purpose of this AIR is to provide a comprehensive description document that displays various examples of transport and business aircraft systems driving Trimmable Horizontal Stabilizers. The main focus is on mechanical systems which may be actuated hydraulically or electrically. The document is intended as an overview for those specifying or designing Horizontal Stabilizer Trim Actuators in order to compare existing solutions as reference for implementation in new aircraft programs.

This document provides an overview of the tests, and issues related to testing, that are unique to Electromechanical Actuators (EMAs). The tests, and issues documented, are not necessarily all-inclusive. This document discusses both the tests applicable to EMAs and the test methodologies to accomplish the test objectives. EMAs may be used in a wide variety of applications such as utility, secondary flight controls and primary flight controls, in a wide variety of markets including manned and unmanned civil and military aircraft, small missile fin and thrust vector control applications up to high powered utility and flight controls. EMAs may also have either a rotary or a linear output, be servo controlled or use simple open loop point-to-point or other control topologies. As such this document covers a wide range of potential applications, the application of any given test requirement is determined by the application and the user.