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Standard

Cargo Restraint Straps - Design Criteria and Testing Methods

2002-07-15
HISTORICAL
AS5385A
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: a cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of NAS 3610, or b non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
Standard

Cargo Restraint Straps - Design Criteria and Testing Methods

2004-11-17
HISTORICAL
AS5385B
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: a cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of NAS 3610, or b non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
Standard

Cargo Restraint Straps - Design Criteria and Testing Methods

2017-05-08
CURRENT
AS5385D
This SAE Aerospace Standard (AS) aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22250 N (5000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain cargo on board civil transport aircraft during flight: a cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main/upper deck cargo systems and meeting the requirements of NAS 3610 or AS36100, or b non-unitized individual pieces of cargo, or pieces of, cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
Standard

Cargo Restraint Straps - Design Criteria and Testing Methods

2007-01-09
HISTORICAL
AS5385C
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22,250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: a cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main/upper deck cargo systems and meeting the requirements of NAS 3610 or AS36100, or b non-unitized individual pieces of cargo, or pieces of, cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
Standard

ENVIRONMENTAL DEGRADATION OF TEXTILES

1988-05-01
HISTORICAL
AIR1490A
Since the ULD device containing textiles should have a predictable service life, there should be data available so that predictions can be made. This technical report compiles available information on textiles of the types used in air cargo ULD devices and reviews the degradation characteristics of each. Textiles are used primarily in cargo restraint nets on air cargo pallets and non structural containers, restraint nets installed in cargo aircraft, and similar applications.
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

Environmental Degradation of Textiles

1995-08-01
HISTORICAL
AIR1490B
Since the ULD device containing textiles should have a predictable service life, there should be data available so that predictions can be made. This document compiles available information on textiles of the types used in air cargo ULD devices and reviews the degradation characteristics of each. Textiles are used primarily in cargo restraint nets on air cargo pallets and nonstructural containers, restraint nets installed in cargo aircraft, and similar applications.
Standard

Environmental Degradation of Textiles

2019-04-24
CURRENT
AIR1490C
Since cargo restraint devices made with textiles should have a predictable service life, there should be data available so that predictions can be made. This document compiles available information on textiles of the types used in air cargo restraint devices and reviews the degradation characteristics of each. Textiles are used primarily in cargo restraint nets on air cargo pallets and nonstructural containers, restraint nets installed in cargo aircraft, and similar applications.
Standard

Fire Containment Cover - Design, Performance, and Testing Requirements

2013-08-06
CURRENT
AS6453
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.
Standard

GENERAL REQUIREMENTS FOR POWERED DRIVE UNITS IN AIRCRAFT CARGO SYSTEMS

1992-11-12
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

2019-01-16
WIP
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.
Standard

General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems

2012-11-01
CURRENT
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

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.
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