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Standard

Aircraft Cargo Door Opening/Sill Details for Ground Support Equipment Interface

2002-04-16
HISTORICAL
AIR1673A
Manufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers into or out of the aircraft holds. Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with the appropriate ground equipment. This SAE Aerospace Information Report (AIR) has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who utilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position.
Standard

Aircraft Cargo Door Opening/Sill Details for Ground Support Equipment Interface

2014-09-30
CURRENT
AIR1673B
Manufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers into or out of the aircraft holds. Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with the appropriate ground equipment. This SAE Aerospace Information Report (AIR) has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who utilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position.
Standard

AIRCRAFT CARGO DOOR OPENING/SILL DETAILS FOR GROUND SUPPORT EQUIPMENT INTERFACE

1986-07-08
HISTORICAL
AIR1673
Manufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers into or out of the aircraft holds. Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with the appropriate ground equipment. This Aerospace Information Report has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who utilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position.
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

Air Cargo Unit Load Devices - Reference Standards

2005-04-15
HISTORICAL
AIR36105
The present Aerospace Information Report (AIR) provides a list of the main government regulations, SAE and international standards, and standing industry recommendations applying to air cargo unit load devices (pallets, nets and containers) to be loaded with either baggage or freight on board civil transport aircraft.
Standard

Air Cargo Unit Load Devices - Reference Documents

2017-04-13
CURRENT
AIR36105B
The present SAE Aerospace Information Report (AIR) provides a list of the main government regulations, SAE and international standards, and standing industry recommendations applying to air cargo unit load devices (pallets, nets, and containers) to be loaded with either baggage or freight on board civil transport aircraft.
Standard

Air Cargo Unit Load Devices – Reference Documents

2011-11-04
HISTORICAL
AIR36105A
The present Aerospace Information Report (AIR) provides a list of the main government regulations, SAE and international standards, and standing industry recommendations applying to air cargo unit load devices (pallets, nets and containers) to be loaded with either baggage or freight on board civil transport aircraft.
Standard

Effects of Hanging Loads (e.g., GOH) on ULD Performance

1997-11-01
HISTORICAL
AIR4359
This SAE Aerospace Information Report (AIR) provides information on the subject of Air Mode containers used for transporting “Hanging Loads” such as Garment-On-Hangers (GOH), or other roof supported cargo. It suggests considerations and recommendations for roof loaded containers to transport hanging loads efficiently and safely by air and to protect the aircraft floor and cargo system from damage due to overload conditions.
Standard

Effects of Hanging Loads (e.g., GOH) on ULD Performance

2016-05-24
CURRENT
AIR4359A
This SAE Aerospace Information Report (AIR) provides information on the subject of Air Mode containers used for transporting "Hanging Loads" such as Garment-On-Hangers (GOH), or other roof supported cargo. It suggests considerations and recommendations for roof loaded containers to transport hanging loads efficiently and safely by air and to protect the aircraft floor and cargo system from damage due to overload conditions.
Standard

METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES

1995-03-01
HISTORICAL
AS1825A
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

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

Methodology of Calculating Aircraft Cargo Volumes

2003-03-27
HISTORICAL
AS1825B
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

Aircraft Cargo Systems - Missing Restraint Limitations Layouts

2014-12-28
CURRENT
ARP5492A
This SAE Aerospace Recommended Practice (ARP) provides recommendations for aircraft manufacturers and operating carriers about how to establish common information for the use of cargo systems with missing/inoperative restraints. Because of the fact that the certified restriction requirements due to missing/inoperative restraints are dependent of the specific aircraft structure and the system layout of the cargo loading system, this document shall only recommend common layout of information for the users based on the certified data provided to allow for common training, understanding and handling. This shall be used right from the beginning for future aircraft types for certified data.
Standard

Aircraft Cargo Systems - Missing Restraint Limitations Layouts

2004-12-30
HISTORICAL
ARP5492
This SAE Aerospace Recommended Practice (ARP) provides recommendations for aircraft manufacturers and operating carriers about how to establish common information for the use of cargo systems with missing/inoperative restraints. Because of the fact that the certified restriction requirements due to missing/inoperative restraints are dependent of the specific aircraft structure and the system layout of the cargo loading system, this document shall only recommend common layout of information for the users based on the certified data provided to allow for common training, understanding and handling. This shall be used right from the beginning for future aircraft types for certified data.
Standard

Certified Containers for Lower Deck Compartments

2014-01-03
CURRENT
AS5896
This SAE Aerospace Standard (AS) covers the design, fabrication, performance, and testing requirements for general-purpose, base-restrained, containers requiring airworthiness approval for installation/use in aircraft lower deck compartments. See 10.1 and 10.2.
Standard

AIR MODE GENERAL PURPOSE CONTAINERS

1995-08-01
HISTORICAL
AS4041A
This SAE Aerospace Standard (AS) establishes the basic requirements for the design, construction and testing of air mode 2.44 m X 2.44 m (8 ft X 8 ft) cross-section containers. These containers are to be used exclusively in conjunction with the air mode in freighter versions of wide-body commercial transport aircraft. Air mode containers will normally be on aircraft roller conveying systems and/or on similarly equipped ancillary ground handling devices. Similar requirements for air/surface (intermodal) containers are provided in AS832.
Standard

Air Mode General Purposes Containers

2014-03-25
CURRENT
AS4041B
This SAE Aerospace Standard (AS) establishes the basic requirements for the design, construction and testing of air mode 2.44 m × 2.44 m (8 ft × 8 ft) cross-section containers. These containers are to be used exclusively in conjunction with the air mode in freighter versions of wide-body commercial transport aircraft. Air mode containers will normally be on aircraft roller conveying systems and/or on similarly equipped ancillary ground handling devices. Similar requirements for air/surface (intermodal) containers are provided in AS832.
Standard

REQUIREMENTS FOR AIRCRAFT ON BOARD WEIGHT AND BALANCE SYSTEM

1995-06-01
HISTORICAL
ARP1409B
This SAE Aerospace Recommended Practice (ARP) establishes requirements for the function, characteristics, and installation of an aircraft On Board Weight and Balance System (OBWBS) for use on civil transport aircraft. This document is not intended to specify design methods, mechanisms, or material to accomplish the requirements set forth.
Standard

Aircraft On Board Weight and Balance System Requirements

2003-03-27
CURRENT
ARP1409C
This SAE Aerospace Recommended Practice (ARP) establishes requirements for the function, characteristics, and installation of an aircraft On Board Weight and Balance System (OBWBS) for use on civil transport aircraft. This document is not intended to specify design methods, mechanisms, or material to accomplish the requirements set forth.
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