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Air Cargo Unit Load Devices - Performance Requirements and Test Parameters
- Aerospace Standard
- AS36100C
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint requirements of Title 14 CFR Part 25, except for the 9.0-g forward ultimate inertia force of § 25.561 (b)(3)(ii).
Rationale
After publication of AS36100B (2016-06), it was decided to add ULD configurations and restraint conditions for 55 x 96 inches (U) and 125 x 196 inches (T) nominal base sizes in Sections 7, “ULD Configurations," and 8, “Testing Restraint Conditions." Further, words have been added to 3.5, “Classification Identifier," to describe requirements regarding dual certification and orientation depiction for RC Q has been corrected.
Revision C is proposed for reference by future TSO-C90 revisions.
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | LIST OF CURRENT PAGES | |
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Unnamed Dataset 4 | ||
| Table 1 | ULD sizes | |
| Table 2 | ULD configurations | |
| Table A7 | Ultimate load criteria | |
| Table A8 | Ultimate load criteria | |
| Table B7 | Ultimate load criteria | |
| Table B8 | Ultimate load criteria | |
| Table G1 | Ultimate load criteria | |
| Table K4 | Ultimate load criteria | |
| Table L5 | Ultimate load criteria | |
| Table L6 | Ultimate load criteria | |
| Table M4 | Ultimate load criteria | |
| Table M5 | Ultimate load criteria | |
| Table N1 | Ultimate load criteria | |
| Table P1 | Ultimate load criteria | |
| Table Q1 | Ultimate load criteria | |
| Table R1 | Ultimate load criteria | |
| Table S1 | Ultimate load criteria | |
| Table T1 | Ultimate load criteria | |
| Table U1 | Ultimate load criteria | |
| Table 3 | Testing restraint conditions |
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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