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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 Standard (AS) covers the design, fabrication, performance, and testing requirements for general-purpose, base-restrained, containers requiring airworthiness approval for installation/use in aircraft lower deck compartments. See 10.1 and 10.2.

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 SAE Aerospace Information Report (AIR) is intended to assist the user (aircraft manufacturer/airline) in the following areas: a In the decision of whether or not to plan for the installation of a powered drive system in the cargo loading system (CLS) during the definition of the aircraft on-board cargo loading system. b If a powered drive system is decided upon, to provide general requirements to be considered during the preparation of component specifications for the powered drive units (PDUs) to be used. This provides a selection of criteria in order to obtain an optimum PDU for the application considered.

This SAE Aerospace Information Report (AIR) is intended to assist the user (aircraft manufacturer/airline) in the following areas: a In the decision of whether or not to plan for the installation of a powered drive system in the cargo loading system (CLS) during the definition of the aircraft on-board cargo loading system. b If a powered drive system is decided upon, to provide general requirements to be considered during the preparation of component specifications for the powered drive units (PDUs) to be used. This provides a selection of criteria in order to obtain an optimum PDU for the application considered.

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 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 Standard (AS) specifies the minimum design and performance criteria and testing methods of fire containment covers (FCCs) used either: a In those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations, or b On a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not mandate their use.

This SAE Aerospace Standard (AS), identical to ISO 14186, specifies the minimum design and performance criteria and testing methods of fire containment covers (FCCs) used either: a in those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations, or b on a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not mandate their use.

This Aerospace Standard (AS) specifies the minimum design and performance criteria and testing methods of passive fire resistant containers (FRCs) used either: a In those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations, or b On a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not mandate their use.