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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 Cargo Unit Load Devices - Performance Requirements and Test Parameters

2020-09-29
CURRENT
AS36100C
This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint requirements of Title 14 CFR Part 25, except for the 9.0-g forward ultimate inertia force of § 25.561 (b)(3)(ii).
Standard

Air Cargo Unit Load Devices - Performance Requirements and Test Parameters

2016-06-06
HISTORICAL
AS36100B
This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint requirements of Title 14 CFR Part 25, except for the 9.0g forward ultimate inertia force of § 25.561 (b)(3)(ii).
Standard

Air Cargo Unit Load Devices – Performance Requirements and Test Parameters

2011-12-12
HISTORICAL
AS36100A
This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint and occupant protection requirements of Title 14 CFR Part 25, except for the 9.0g forward ultimate inertia force of § 25.561 (b)(3)(ii).
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

Cargo Stopper Devices

2011-07-06
HISTORICAL
AS6554
The purpose of this SAE Aerospace Standard (AS) is to standardize the basic design, performance and testing requirements for “Cargo Stoppers” cargo tie-down accessories to be used in conjunction with approved tie-down straps meeting AS5385C (TSO C-172) requirements.
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.
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