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Logistics Copper Documentation AGE-2 Air Cargo Identification

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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

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

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

General Requirements for Noncertified Cargo/Baggage Containers
2018-10-18
CURRENT
AS1677D
This SAE Aerospace Standard (AS) covers the design, fabrication, performance and operational testing requirements for lower deck containers for use in main line aircraft which do not require airworthiness certification when loaded under the conditions of compartment restraint and in accordance with the aircraft's Weight and Balance Manual and/or, where applicable according to the aircraft type's approved Weight and Balance Manual, AS36100A or NAS 3610 equivalent base plate restraint for these containers. Most sizes of containers covered by this document (base sizes K, L, P, and Q) cannot physically be loaded and latched on aircraft main deck cargo systems. Base size A and M containers can, but are not allowed on aircraft main decks, which do not accept non-certified units. Accordingly, all containers covered by this document are to be used/installed exclusively in aircraft lower deck compartments.
Standard

GENERAL REQUIREMENTS FOR NONCERTIFIED LD-2, LD-4, AND LD-8 CARGO/BAGGAGE CONTAINERS
1995-06-01
HISTORICAL
AS1677B
This SAE Aerospace Standard (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 Specification 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

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

General Requirements for Noncertified Cargo/Baggage Containers
2008-06-22
HISTORICAL
AS1677C
This SAE Aerospace Standard (AS) covers the requirements for lower deck containers in wide body and standard body aircraft which do not require airworthiness certification under the condition of compartment restraint and/or, where applicable according to aircraft type, NAS3610 equivalent baseplate-restraint for these containers. NOTE: IATA 50/0, “Requirements for interlining of ULDs”, should also be taken into account when designing and making equipment.
Standard

Air and Air/Surface (Platform) Cargo Pallet Nets
2018-10-18
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

Cargo Restraint on Aircraft Passenger Seats – Main Passenger Cabin
2011-12-12
CURRENT
ARP4049A
This SAE Aerospace Recommended Practice (ARP) establishes the basic recommendations for the following two types of configuration for securing cargo to aircraft passenger seats on transport category aircraft: It is emphasized that the two types of restraint shown are merely examples of methods currently used and does not imply that alternative methods are not acceptable. For the purposes of this document, the minimum essential criteria are identified by the use of the key word "shall," Recommended criteria are identified by the use of the key word "should," and while not mandatory are considered to be of significant importance in providing safe, economical, and practical means of cargo restraint. Deviation from recommended criteria should occur only after careful consideration, extensive testing, and thorough service evaluation have shown alternative methods to be satisfactory.
Standard

CARGO RESTRAINT ON AIRCRAFT PASSENGER SEATS - MAIN PASSENGER CABIN
2008-06-22
HISTORICAL
ARP4049
This SAE Aerospace Recommended Practice (ARP) establishes the basic recommendations for the following two types of configuration for securing cargo to aircraft passenger seats on transport category aircraft: It is emphasized that the two types of restraint shown are merely examples of methods currently used and does not imply that alternative methods are not acceptable. For the purposes of this document, the minimum essential criteria are identified by the use of the key word "shall." Recommended criteria are identified by the use of the key word "should," and while not mandatory are considered to be of significant importance in providing safe, economical, and practical means of cargo restraint. Deviation from recommended criteria should occur only after careful consideration, extensive testing, and thorough service evaluation have shown alternative methods to be satisfactory.
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.
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