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.
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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
Fittings and Cargo Rings, Tie-Down, Aircraft Floor
2012-12-03
CURRENT
AS8905A
This specification establishes requirements for two types of aircraft floor fittings for tiedown of cargo and seats, and two types of cargo tiedown rings.
Standard
Fittings and Cargo Rings, Tie-Down, Aircraft Floor
2006-07-25
HISTORICAL
AS8905
This specification establishes requirements for two types of aircraft floor fittings for tiedown of cargo and seats, and two types of cargo tiedown rings.
Standard
Tie Downs, Cargo, Aircraft
2000-11-01
HISTORICAL
AS25959
This specification covers four types of aircraft cargo tie downs.
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
Net, Cargo Tiedown, Pallets, HCU-7/E, HCU-15/C, HCU-11/C, and HCU-16/C
2000-11-01
HISTORICAL
AS27444
This specification covers pallet cargo tiedown nets, designated HCU-7/E, HCU-15/C, HCU-11/C and HCU-16/C.
Standard
Tie Down, Cargo, Aircraft, Nylon Web Net
2000-11-01
HISTORICAL
AS26780
This specification covers two types of aircraft cargo tie downs, each having a capacity of 10,000 pounds.
Standard
AS36100 Background and Development Record
2018-10-18
CURRENT
AIR36108
This Aerospace Information Report (AIR) provides a record of the development by SAE AGE-2A Air Cargo Sub-Committee of Aerospace Standard AS36100, Air Cargo Unit Load Devices — Performance Requirements and Test Parameters, published 2005-02, and its revision A published 2006-04, intended as a technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded with either baggage or freight on board civil transport aircraft, and to partly supersede previously used NAS 3610, Cargo unit load devices - Specification for — [ Revision 10, 1990, referenced in TSO C90(c) ].
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
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
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
AS36100 Background and Development Record
2006-02-28
HISTORICAL
AIR36107
This SAE Aerospace Information Report (AIR) provides a record of the development by SAE AGE-2A Air Cargo Sub-Committee of Aerospace Standard AS36100, Air Cargo Unit Load Devices - Performance Requirements and Test Parameters, published 2005-02, intended as a technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded with either baggage or freight on board civil transport aircraft, and to partly supersede previously used NAS 3610, Cargo unit load devices - Specification for - [Revision 10, 1990, referenced in TSO C90c].
Standard
AS36100 Background and Development
2011-11-23
CURRENT
AIR36107A
This SAE Aerospace Information Report (AIR) provides a record of the development by SAE AGE-2A Air Cargo Sub-Committee of Aerospace Standard AS36100, Air Cargo Unit Load Devices - Performance Requirements and Test Parameters, published 2005-02, intended as a technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded with either baggage or freight on board civil transport aircraft, and to partly supersede previously used NAS 3610, Cargo unit load devices - Specification for - [Revision 10, 1990, referenced in TSO C90c].
Standard
Cargo Compartments Maximum Package Size Calculation Methodology
2008-06-22
HISTORICAL
AIR4899
The methodology for maximum package size loading is based on a mathematical method allowing the calculation of maximum package size tables. This method does not in principal differentiate between bulk loading and cargo system loading. However, some restrictions have to be considered: Some cargo systems generate pre-determined pallet trajectories. Envelope curves depending on the pallet size and the possible trajectories have to be determined first. Door geometric limitations (with or without cargo loading system) Turning limitations due to weight, load geometry and conveyance capability Securing requirements This document is not intended for airline operational use. It should be used by engineers performing calculations or developing computer programs to produce Maximum Package Size tables specified in AS1825.
Standard
Cargo Compartments Maximum Package Size Calculation Methodology
2014-03-25
CURRENT
AIR4899A
The methodology for maximum package size loading is based on a mathematical method allowing the calculation of maximum package size tables. This method does not in principal differentiate between bulk loading and cargo system loading. However, some restrictions have to be considered: Some cargo systems generate pre-determined pallet trajectories. Envelope curves depending on the pallet size and the possible trajectories have to be determined first. Door geometric limitations (with or without cargo loading system) Turning limitations due to weight, load geometry and conveyance capability Securing requirements This document is not intended for airline operational use. It should be used by engineers performing calculations or developing computer programs to produce Maximum Package Size tables specified in AS1825.
Standard
Methodology of Calculating Aircraft Cargo Volumes
2014-03-25
CURRENT
AS1825C
The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the "internal volumes" of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) shall also be stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.
Standard
Cargo Stopper Devices
2009-05-05
HISTORICAL
ARP6022
The purpose of this SAE Aerospace Recommended Practice (ARP) 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 requirements.
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.
