SAE International METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES AS1825

Description
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.
Description
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.

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METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES - AS1825 - SAE International
Warrendale, PA, United States
METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES
AS1825
METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES 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.

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.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number AS1825
Product Name METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES
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