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Standard

AIR-LAND DEMOUNTABLE CARGO PALLET NETS

1975-08-01
HISTORICAL
AS1131A
This document establishes four sizes of basic pallet nets as follows: Size F (10 ft) - To restrain a 96 x 117.75 x 96 in. (2,43 x 2,99 x 2,43 m) high (maximum) load. Size G (20 ft) - To restrain a 96 x 238.500 x 96 in. (2,43 x 6,05 x 2,43 m) high (maximum) load. Size H (30 ft) - To restrain a 96 x 359.25 x 96 in. (2,43 x 9,12 x 2,43 m) high (maximum) load. Size J (40 ft) - To restrain a 96 x 480 x 96 in. (2,43 x 12,19 x 2,43 m) high (maximum) load.
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

Air and Air/Surface (Platform) Cargo Pallet Nets

2002-02-24
CURRENT
AS1131C
This SAE Aerospace Standard (AS) provides dimensional, structural and environmental requirements for pallet nets to be used in conjunction with 2.44 m (8 ft) wide pallets described in AS1130. The pallet/net combination are used in freighter versions of certificated aircraft equipped to provide restraint to pallets tested to the requirements of NAS 3610 Class II restraint system. The minimum essential criteria are identified by use of the key word "shall". Recommended criteria are identified by use of the key word "should", and while not mandatory, are considered to be primary importance in providing serviceable, economical, and practical air transport pallet nets. Deviation from recommended criteria should occur only after careful consideration, extensive testing, and thorough service evaluation have shown alternate methods to be satisfactory.
Standard

Auto Transport Unit Load Device

2002-03-22
HISTORICAL
ARP1554C
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.
Standard

Auto Transport Unit Load Device

2000-05-01
HISTORICAL
ARP1554B
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.
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 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 Noncertified Cargo/Baggage Containers

2013-06-27
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 Cargo/Baggage Containers

2002-01-31
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

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.
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