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AGE-2 Air Cargo Optics Tools and equipment Design Engineering and Styling

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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
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

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
2018-10-18
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.
Standard

Air Cargo Unit Load Devices - Use of Airworthiness Reference Documents
2018-10-18
CURRENT
AIR36106A
This SAE Aerospace Information Report (AIR) provides instructions for intended proper use of Aerospace Standard AS36100A, published 2006-04 [TSO pending], as the technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded on board civil transport aircraft. For consistency and cross-checking purposes, it also includes instructions for proper use of previous NAS 3610 [Revision 10, 1990, referenced in TSO C90c], as commonly understood by the industry.
Standard

Air Cargo Unit Load Devices - Use of Airworthiness Reference Documents
2006-03-21
HISTORICAL
AIR36106
This Aerospace Information Report (AIR) provides instructions for intended proper use of Aerospace Standard AS36100 published 2005-02, as the technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded on board civil transport aircraft. For consistency and cross-checking purposes, it also includes instructions for proper use of previous NAS 3610 [Revision 10, 1990, referenced in TSO C90c], as commonly understood by the industry.
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

Symbology for Standardization of Cargo Handling Systems
2013-03-01
CURRENT
ARP1757B
The symbols specified in this SAE Aerospace Recommended Practice (ARP) are applicable to all aircraft cargo handling systems for lower deck as well as for upper deck systems. Utilizing the symbols the conveyance, guidance, restraint, power drive unit and the degree of automation for the total cargo handling system can be depicted.
Standard

Symbology for Standardization of Cargo Handling Systems
2007-12-07
HISTORICAL
ARP1757A
The symbols specified in this SAE Aerospace Recommended Practice (ARP) are applicable to all aircraft cargo handling systems for lower deck as well as for upper deck systems. Utilizing the symbols the conveyance, guidance, restraint, power drive unit and the degree of automation for the total cargo handling system can be depicted.
Standard

SYMBOLOGY FOR STANDARDIZATION OF ULD HANDLING DEVICES
1995-02-01
HISTORICAL
ARP1757
The symbols specified in this ARP are applicable to all aircraft cargo handling systems for underfloor as well as for maindeck systems. Utilizing the symbols the conveyance, guidance, restraint, power drive unit and the degree of automation for the total cargo handling system can be depicted.
Standard

Certified Containers for Lower Deck Compartments
2018-10-18
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

GENERAL REQUIREMENTS FOR POWERED DRIVE UNITS IN AIRCRAFT CARGO SYSTEMS
2008-06-22
HISTORICAL
AIR4165
This Aerospace Information Report (AIR) serves a dual purpose. It enables the user (aircraft manufacturer/airline) to do the following: a To make a positive decision for the installation of a powered drive system in the cargo loading system during the definition of the aircraft on-board cargo loading system to be developed/procured. b To provide the user with general requirements to be taken into consideration during the preparation of component specifications for powered drive units (PDUs) to be used in aircraft cargo systems. This is to provide the author of such a component specification with a selection of criteria in order to obtain an optimum component suitable for the users’ applications.
Standard

General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems
2012-11-01
HISTORICAL
AIR4165A
This SAE Aerospace Information Report (AIR) is intended to assist the user (aircraft manufacturer/airline) in the following areas: a In the decision of whether or not to plan for the installation of a powered drive system in the cargo loading system (CLS) during the definition of the aircraft on-board cargo loading system. b If a powered drive system is decided upon, to provide general requirements to be considered during the preparation of component specifications for the powered drive units (PDUs) to be used. This provides a selection of criteria in order to obtain an optimum PDU for the application considered.
Standard

General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems
2019-10-02
CURRENT
AIR4165B
This SAE Aerospace Information Report (AIR) is intended to assist the user (aircraft manufacturer/airline) in the following areas: a In the decision of whether or not to plan for the installation of a powered drive system in the cargo loading system (CLS) during the definition of the aircraft on-board cargo loading system. b If a powered drive system is decided upon, to provide general requirements to be considered during the preparation of component specifications for the powered drive units (PDUs) to be used. This provides a selection of criteria in order to obtain an optimum PDU for the application considered.
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