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This specification covers the general requirements for the design and installation of fluid anti-icing, de-greasing, and washing systems installed in military aircraft.

This document describes guidelines and methods of performing the safety assessment for certification of civil aircraft. It is primarily associated with showing compliance with FAR/JAR 25.1309. The methods outlined here identify a systematic means, but not the only means, to show compliance. A subset of this material may be applicable to non-25.1309 equipment. The concept of Aircraft Level Safety Assessment is introduced and the tools to accomplish this task are outlined. The overall aircraft operating environment is considered. When aircraft derivatives or system changes are certified, the processes described herein are usually applicable only to the new designs or to existing designs that are affected by the changes. In the case of the implementation of existing designs in a new derivation, alternate means such as service experience may be used to show compliance.

This specification covers two types and three weight/speed categories of personnel carrying parachute assemblies:

This document defines the minimum performance standards for personnel parachute assemblies to be carried in aircraft or worn by passengers, crew, or parachutists for emergency use. This document covers three types of personnel carrying parachute assemblies and the operating limitations for each:

This specification covers the requirements for one (1) type of pocket photographic interpretation kit, containing viewing and measuring instruments, for use in the field.

This specification covers the requirements for disposable self-pressurized kits which utilize a propellant can pressurized with a liquified gas to atomize a product contained in a separate but attached jar (see 6.1).

This specification establishes environmental criteria for designing Aerospace Ground Equipment (AGE) in support of space systems. The test levels in this specification have been elevated to compensate for absence of combined environments during test, and to allow for variations in equipment and operating conditions. Environmental requirements are summarized in Table 1.

This document provides guidelines for consolidation and standardization of commercial jet transport parts, materials, and processes currently defined by two or more company or industry standards. Included in this ARP are processes for selecting and evaluating standardization opportunities as well as a procedure for initiating the development and release of global aerospace industry standards. These practices are intended to be used when two or more company standards appear to have significant overlap or in fact be technically identical. Benefits of such standardization efforts include part numbers and potentially reduced inventory levels, reduced errors, reduced qualification costs, and reduced equipment life cycle costs. This ARP is intended to be used by any two or more companies involved in the aerospace industry that wish to benefit from standardization.

This specification covers the requirements for an interval timer for controlling the duration of an electrical pulse to a solenoid valve for use in Rain Repellent systems covered by Specification MIL-R-81589.

This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60°F) solid propellant rocket engine hereinafter specified as 5 S-4500.

This specification covers canisters for shipment and storage of lithium hydroxide (LiOH), to be used in receptacle for CO2 absorbent (see MIL-R-24159).

This specification covers the requirements for one type of water repellent compound.

The reader of specifications sometimes needs some help understanding the reasoning behind certain usage of terms. The scope of this AIR is to explain the functions of the various sections of the specifications, why some of the terms in AMS specifications are used, and how the specification system works. After the introduction, the topics are shown in the order they usually appear in specifications.

This specification covers the design requirements and configuration of letters, numerals, and identification for aircrew station displays and control panels.

This specification is designed to present detailed procedure to be followed in splicing cable terminals. The types of cable to which this specification applies are listed in Section 2 and table I.