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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

Cargo Compartments Maximum Package Size Calculation Methodology

2003-04-24
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

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

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

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 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

INTERLINE AIR CARGO PALLET NETS

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

Interline Air Cargo Pallet Nets

1992-07-01
CURRENT
AS1492B
This document establishes dimensional, structural, and environmental requirements for two types of interline pallet nets. Type II covers NAS 3610 code sizes and Type III covers other sizes not currently included in NAS 3610.
Standard

INTERLINE AIR CARGO PALLET NETS

1985-01-01
HISTORICAL
AS1492A
This specification establishes dimensional, structural and environmental requirements for two types of interline pallet nets. Type II covers NAS 3610 code sizes and Type III covers other sizes not currently included in NAS 3610.
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

Air Cargo Unit Load Devices – Load Distribution Model

2011-09-07
CURRENT
AS36101A
This SAE Aerospace Standard (AS) defines an industry agreed reference model for load distribution on air cargo unit load device (ULD) bases, to reflect maximum allowable center of gravity (CG) eccentricity and ensure the maximum allowable area load is not exceeded.
Standard

Air Cargo Unit Load Devices - Load Distribution Model

2004-01-14
HISTORICAL
AS36101
This SAE Aerospace Standard (AS) defines an industry agreed reference model for load distribution on air cargo unit load device (ULD) bases, to reflect maximum allowable center of gravity (CG) eccentricity and ensure the maximum allowable area load is not exceeded.
Standard

Air Cargo Unit Load Devices – Testing Methods

2017-03-14
CURRENT
AS36102B
This SAE Aerospace Standard (AS) specifies the testing methods to be used to substantiate performance of air cargo containers, pallets and nets (Unit Load Devices) for airworthiness approval in accordance with NAS 3610 or AS36100.
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

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

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