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Standard

Development Process - Aerospace Fly-By-Wire Actuation System

2018-04-23
WIP
ARP5007B
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.
Standard

Cover, Flight - Governor Mounting Pad

2018-04-19
WIP
AS307A
To establish criteria for acceptability of discontinuities as revealed by inspection by magnetic particle, fluorescent penetrant, or contrast dye penetrant inspection. Criteria for acceptability of discontinuities cited herein revealed by other methods required by applicable part specification shall be as specified in applicable part specification. This specification is primarily intended to cover standard parts such as pins, nuts and fittings. It may be applied to any item which must meet the specified requirements except that the requirements of AS 1177 apply to bolts, screws and studs.
Standard

Bolt, Tee Head, Interface Surface, Dimensions for

2018-04-19
WIP
ARP1902B
This recommended practice provides the dimensional data for the diameters of surfaces that interface with the following tee head bolt series: AS 3232 thru AS 3235, MS 9397 thru MS 9402 and MS 9432 thru MS 9437, or other parts with compatible dimensions.
Standard

A Guide for the Damaging Effects of Tire and Wheel Failures

2018-04-19
WIP
AIR5699A
Consideration for the damaging effects to aircraft from the failure of wheels and tires should be evaluated. This document discusses the types of problems in-service aircraft have experienced and methodology in place to assist the designers when evaluating threats for new aircraft design. The purpose of this document is to provide a history of in-service problems, provide a historical summary of the design improvements made to wheels and tires during the past 40 years and to offer methodology which has been used to help designers assess the threat to ensure the functionality of systems and equipment located in and around the landing gear and in wheel wells.
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