Search Results

Standard

Wide-Body and Standard-Body Aircraft Lower Deck Cargo Compartment ULD Capacities

2022-05-04

CURRENT

AIR1869D

This SAE Aerospace Information Report (AIR) covers information relative to ULDs (Unit Load Devices) container and pallet configurations, maximum usable container, pallet and bulk compartment volumes and tare weights for the lower deck of various wide-body aircraft. Bulk compartment volumes are also included for standard-body aircraft.

Standard

ULD for Aircraft Transportation of Horses

2023-05-26

WIP

ARP1621D

This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several.

Standard

ULD for Aircraft Transportation of Horses

2012-11-26

HISTORICAL

ARP1621B

This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several. There are two types of ULDs for aircraft transportation of horses: a Type 1: The ULD is an airworthiness certified structural container, satisfying the requirements of NAS 3610 for the appropriate base size. b Type 2: The ULD consists of a self-contained stall which is positioned on a standard aircraft pallet and restrained to the pallet by means of a cargo pallet net or by straps. WARNING: It is the carrier’s responsibility to obtain airworthiness approval for a Type 2 unit using strap-restraint. Refer to 7.1 b (Documentation).

Standard

ULD for Aircraft Transportation of Horses

2017-09-11

CURRENT

ARP1621C

This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several. There are two types of ULDs for aircraft transportation of horses:

Standard

ULD FOR AIRCRAFT TRANSPORTATION OF HORSES

1980-03-01

HISTORICAL

ARP1621

This ARP defines minimum requirements for horse stalls necessary to maintain a structurally safe operation and protect aircraft from corrosion created by waste spills.

Standard

ULD FOR AIRCRAFT TRANSPORTATION OF HORSES

1990-08-01

HISTORICAL

ARP1621A

This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several. There are two types of ULDs for aircraft transportation of horses: a Type 1: The ULD is an airworthiness certified structural container, satisfying the requirements of NAS 3610 for the appropriate base size. b Type 2: The ULD consists of a self-contained stall which is positioned on a standard aircraft pallet and restrained to the pallet by means of a cargo pallet net or by straps.

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

Stands, Shipping and Storage, Aircraft Engines, Reusable

2017-10-25

WIP

ARP4898A

This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.

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

2008-06-22

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

METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES

1983-07-01

HISTORICAL

AS1825

The scope of this Aerospace Standard 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 (ULD's) shall also be stated in order to provide the maximum OLD external contour and the methodology to define the OLD internal volumes. The methodology of defining and determining "maximum package sizes charts" for the cargo compartments shall also be included.

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

Interline Air Cargo Pallets

2012-09-05

HISTORICAL

AS1491A

This document establishes dimensional, structural and environmental requirements for two types of interline pallets. Type II covers NAS 3610 code sizes and Type III covers other sizes not currently included in NAS 3610.

Standard

Interline Air Cargo Pallets

2023-01-13

CURRENT

AS1491B

This SAE Aerospace Standard specifies the dimensional, design criteria, fabrication, performance, operational, environmental, and testing requirements for interline pallets requiring airworthiness approval for loading onto civil transport aircraft equipped with NAS3610/AS36100 restraint systems and using pallet nets meeting the requirements of AS1492. Type II/2 covers NAS3610/AS36100 code sizes. Type III pallets have been removed from this SAE Aerospace Standard revision.

Standard

Interline Air Cargo Pallet Nets

2023-01-13

CURRENT

AS1492C

This document establishes dimensional, structural, and environmental requirements for Type II/2 interline pallet nets. Type II/2 covers NAS3610/AS36100 code sizes.

Standard

INTERLINE AIR CARGO PALLETS

1982-03-01

HISTORICAL

AS1491

This document establishes dimensional, structural and environmental requirements for 1.5G interline pallets.

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.

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.