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Methodology of Calculating Aircraft Cargo Volumes
- Aerospace Standard
- AS1825C
- Stabilized
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
The SAE AGE-2A committee determined that the technology/practice defined in this standard has reached a level of maturity such that it is unlikely to change in the foreseeable future; therefore, it does not require regular 5-year reviews by the committee and it is appropriate for it to be stabilized.
Recommended Content
| Aerospace Standard | Effects of Hanging Loads (e.g., GOH) on ULD Performance |
| Aerospace Standard | Vehicle Transport Unit Load Device (ULD) |
| Aerospace Standard | Air Cargo Unit Load Devices – Center of Gravity Control Methods |
Data Sets - Support Documents
No Datasets Available
Issuing Committee
Committee AGE-2 reports to the Aerospace General Projects Division. The main, or governing committee, AGE-2, is composed of the most experienced members, mainly from the airlines, airframe manufacturers, and support equipment manufacturers, to provide leadership and guidance for the Membership to implement the work is drawn with reasonable balance from airlines, airframe manufacturers, support equipment manufacturers, and others with special aircraft related expertise. Members serve based on their knowledge, expertise, and experience and not as agents or representatives of any organization.
Reference
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