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Standard

Auto Transport Unit Load Device

2008-06-22
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

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

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

2000-09-01
HISTORICAL
AS5385
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

2012-11-26
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

Drum, Metal-Shipping and Storage

2017-11-03
CURRENT
AS6054
This specification covers new cylindrical drums to be used as exterior shipping containers (see 6.1).
Standard

Fittings, Cargo Tiedown, Aircraft

2006-04-27
HISTORICAL
AS7092A
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
Standard

Fittings, Cargo Tiedown, Aircraft

2012-10-15
CURRENT
AS7092B
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
Standard

Fittings, Cargo Tiedown, Aircraft

1999-07-01
HISTORICAL
AS7092
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
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

GROUND EQUIPMENT REQUIREMENTS FOR COMPATIBILITY WITH AIRCRAFT UNIT LOAD DEVICES

1984-10-01
HISTORICAL
ARP1334A
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.
Standard

GROUND EQUIPMENT REQUIREMENTS FOR COMPATIBILITY WITH AIRCRAFT UNIT LOAD DEVICES

1973-11-01
HISTORICAL
ARP1334
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.
Standard

Ground Equipment Requirements for Compatibility With Aircraft Unit Load Devices

2004-07-02
HISTORICAL
ARP1334B
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.
Standard

Ground Equipment Requirements for Compatibility with Aircraft Unit Load Devices

2011-09-07
CURRENT
ARP1334C
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.
Standard

INTERLINE AIR CARGO PALLET NETS

1982-03-01
HISTORICAL
AS1492
This specification establishes dimensional, structural and environmental requirements for interline pallet nets.
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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