Search Results

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

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

AIR MODE GENERAL PURPOSE CONTAINERS

2008-06-22

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

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

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

REQUIREMENTS FOR AIRCRAFT ON BOARD WEIGHT AND BALANCE SYSTEM

1992-12-01

HISTORICAL

ARP1409A

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

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

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 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

1992-12-01

HISTORICAL

AS1131B

This document establishes four sizes of basic pallet nets as follows and are covered by NAS 3610 codes 2FIN, 2GIN, 2HIN and 2JIN.

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

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

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

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.