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Environment Thermodynamics Heat transfer AGE-2 Air Cargo Interiors, Cabins, and Cockpits

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Standard

Tie Down, Cargo, Aircraft, CGU-1/B
2000-11-01
HISTORICAL
AS27260
This specification covers one type of 5,000-pound capacity aircraft cargo tie down. The tie down is designated CGU-1/B and is furnished in a minimum length of 240 inches.
Standard

INSULATED AIR CARGO CONTAINER
1992-12-01
HISTORICAL
ARP1523
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.
Standard

INSULATED AIR CARGO CONTAINER
1995-07-01
HISTORICAL
ARP1523A
The purpose of this document is to establish minimum operational requirements that will ensure that perishable cargoes in insulated standard airborne containers can be kept in prime condition during the ground handling and air transportation cycle within a maximum time span of 48 h.
Standard

General Requirements for Noncertified Cargo/Baggage Containers
2018-10-18
CURRENT
AS1677D
This SAE Aerospace Standard (AS) covers the design, fabrication, performance and operational testing requirements for lower deck containers for use in main line aircraft which do not require airworthiness certification when loaded under the conditions of compartment restraint and in accordance with the aircraft's Weight and Balance Manual and/or, where applicable according to the aircraft type's approved Weight and Balance Manual, AS36100A or NAS 3610 equivalent base plate restraint for these containers. Most sizes of containers covered by this document (base sizes K, L, P, and Q) cannot physically be loaded and latched on aircraft main deck cargo systems. Base size A and M containers can, but are not allowed on aircraft main decks, which do not accept non-certified units. Accordingly, all containers covered by this document are to be used/installed exclusively in aircraft lower deck compartments.
Standard

GENERAL REQUIREMENTS FOR NONCERTIFIED LD-2, LD-4, AND LD-8 CARGO/BAGGAGE CONTAINERS
1995-06-01
HISTORICAL
AS1677B
This SAE Aerospace Standard (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 Specification 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.
Standard

GENERAL REQUIREMENTS FOR NON-CERTIFIED LD-2, LD-4 & LD-8 CARGO/BAGGAGE CONTAINERS
1988-11-01
HISTORICAL
AS1677A
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.
Standard

General Requirements for Noncertified Cargo/Baggage Containers
2008-06-22
HISTORICAL
AS1677C
This SAE Aerospace Standard (AS) covers the requirements for lower deck containers in wide body and standard body aircraft which do not require airworthiness certification under the condition of compartment restraint and/or, where applicable according to aircraft type, NAS3610 equivalent baseplate-restraint for these containers. NOTE: IATA 50/0, “Requirements for interlining of ULDs”, should also be taken into account when designing and making equipment.
Standard

Cargo Restraint on Aircraft Passenger Seats – Main Passenger Cabin
2011-12-12
CURRENT
ARP4049A
This SAE Aerospace Recommended Practice (ARP) establishes the basic recommendations for the following two types of configuration for securing cargo to aircraft passenger seats on transport category aircraft: It is emphasized that the two types of restraint shown are merely examples of methods currently used and does not imply that alternative methods are not acceptable. For the purposes of this document, the minimum essential criteria are identified by the use of the key word "shall," Recommended criteria are identified by the use of the key word "should," and while not mandatory are considered to be of significant importance in providing safe, economical, and practical means of cargo restraint. Deviation from recommended criteria should occur only after careful consideration, extensive testing, and thorough service evaluation have shown alternative methods to be satisfactory.
Standard

CARGO RESTRAINT ON AIRCRAFT PASSENGER SEATS - MAIN PASSENGER CABIN
2008-06-22
HISTORICAL
ARP4049
This SAE Aerospace Recommended Practice (ARP) establishes the basic recommendations for the following two types of configuration for securing cargo to aircraft passenger seats on transport category aircraft: It is emphasized that the two types of restraint shown are merely examples of methods currently used and does not imply that alternative methods are not acceptable. For the purposes of this document, the minimum essential criteria are identified by the use of the key word "shall." Recommended criteria are identified by the use of the key word "should," and while not mandatory are considered to be of significant importance in providing safe, economical, and practical means of cargo restraint. Deviation from recommended criteria should occur only after careful consideration, extensive testing, and thorough service evaluation have shown alternative methods to be satisfactory.
Standard

Air Mode Active Containers Conditioning Performance
2010-11-15
CURRENT
ARP5741
This Aerospace Recommended Practice (ARP) defines a series of test procedures to determine the temperature conditioning performance of air mode containers with active conditioning systems, a classification system for air mode containers with active condition systems, a standard means of expressing conditioning performance within each classification and a standard means of documenting test results.
Standard

Environmental Degradation of Composite Materials
2018-10-18
CURRENT
ARP6287
In accordance with § 4.11 of AS36100, materials used in the construction of pallets, nets, and containers shall take into account the effects of environmental conditions, such as temperature, humidity, and UV degradation, expected in service. In accordance with (E)TSO-C90, the applicant shall consider environmental degradation due to aging, ultra-violet (UV) exposure, weathering, etc., for any materials used in the construction of pallets, nets, and containers. The purpose of this Aerospace Recommended Practice (ARP) is to provide guidelines for the basic requirements to be considered regarding environmental degradation effects when qualifying composite materials in the design to fulfill the (E)TSO-C90 Minimum Performance Standard. Material qualification is the verifying of a materials attributes and characterizations, which are typically determined through testing.
Standard

GENERAL REQUIREMENTS FOR POWERED DRIVE UNITS IN AIRCRAFT CARGO SYSTEMS
2008-06-22
HISTORICAL
AIR4165
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.
Standard

General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems
2012-11-01
HISTORICAL
AIR4165A
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.
Standard

General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems
2019-10-02
CURRENT
AIR4165B
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.
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