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This recommended practice covers a self-contained detection system which is capable of pressurizing a closed system up to 70 psig with halogen (tracer) gas and up to 3500 psig with nitrogen.

This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.

The primary purpose of the shipping closure is to protect the aircraft parts or system from damage and foreign material ingress/egress (e.g., dust, dirt or other contaminants) during transport and storage. Shipping closures are not airworthy items. Therefore, their usage is defined as preventative for the parts to be protected as opposed to operational. Military and commercial customer requirements for the prevention of damage or contamination to stored parts are generally limited to the generic instructions “all openings should be sufficiently covered to prevent the entrance of dust, dirt, moisture or other foreign contaminants”. This recommended practice outlines basic minimum parameters for suggested item construction and usage. Additionally, this recommended practice provides instruction on how to apply these closures to various openings.

This SAE Aerospace Standard (AS) details the design of fork pockets on containers and equipment for use with pallet lift trucks and forklift trucks.

This document lists recommended noun titles for drawings of support equipment and provides definitions for each. The use of secondary modifiers to distinguish a part from similar parts is also covered.

Perishable cargoes, e.g., dairy produce, fruit, vegetables, flowers, frozen foods, meat, fish, etc., require maintenance of specific temperature ranges during air related door-to-door transportation.

This SAE Aerospace Recommended Practice (ARP) specifies requirements for those portions of the aircraft Unit Load Device ground and terminal handling equipment that will have a direct bearing on the life of the ULD for the purpose of preventing undue wear on the ULD. Past experience has shown that in-service defects in regard to the above equipment cause high ULD cost. Greater control of maintenance is required.

This SAE Aerospace Recommended Practice (ARP) specifies requirements for those portions of the aircraft Unit Load Device ground and terminal handling equipment that will have a direct bearing on the life of the ULD for the purpose of preventing undue wear on the ULD. Past experience has shown that in-service defects in regard to the above equipment cause high ULD cost. Greater control of maintenance is required.

Included in this document are requirements for conveyor systems, guides, stops, restraint hardware that are used on trucks, transporters, dollies, storage provisions, pallet build-up hoists, or other device-handling equipment. These requirements reflect state of the art criteria applied to known successfully operated hardware. Any design deviations shall be required to demonstrate equivalency to this specification criteria.

Included in this document are requirements for conveyor systems, guides, stops, restraint hardware that are used on trucks, transporters, dollies, storage provisions, pallet build-up hoists, or other device-handling equipment. a) These requirements reflect state of the art criteria applied to known successfully operated hardware. Any design deviations shall be required to demonstrate equivalency to this specification criteria. b) These devices usually form an integral part of the aircraft and as such are subject to regulatory agencies' requirements to assure structural integrity.

This Aerospace Information Report (AIR) serves a dual purpose. It enables the user (aircraft manufacturer/airline) to do the following: a To make a positive decision for the installation of a powered drive system in the cargo loading system during the definition of the aircraft on-board cargo loading system to be developed/procured. b To provide the user with general requirements to be taken into consideration during the preparation of component specifications for powered drive units (PDUs) to be used in aircraft cargo systems. This is to provide the author of such a component specification with a selection of criteria in order to obtain an optimum component suitable for the users’ applications.

This AS covers the requirements for three sizes of compartment restrained lower deck containers (Unit Load Devices) for the 767 airplane and which do not require airworthiness certification.

This AS covers the requirements for three sizes of compartment restrained lower deck containers (Unit Load Devices) for the 767 airplane and which do not require airworthiness certification. NOTE: IATA Specificaton 50/0, General Technical Requirements and Serviceability limits, should also be taken into account when designing and making equipment according to this Specification as certain provisions contained therein will also be applicable.

This specification covers general requirements for covers intended to protect the following aircraft parts: Cockpit Fuselage Canopy Engine Armament Propeller or Rotor Miscellaneous

The tests are static in nature to minimize complexity and cost of required testing facilities. As far as practical, applied static loads should take into account the combined static and dynamic loads anticipated in service.

The tests are static in nature to minimize complexity and cost of required testing facilities. As far as practical, applied static loads should take into account the combined static and dynamic loads anticipated in service.