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AIR36108
AS36100 Background and Development Record
AS36100 Background and Development Record
有效
【范围】 1.1 Purpose 1.1.1 This 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, and its revision A published 2006-04, 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 C90(c) ]. 1.1.2 AS36100 was developed over a 5 year period (1999-2004) by a Panel of SAE AGE-2A designated as “NAS 3610 Oversight Panel“ (OSP), based on a worldwide industry consensus that NAS 3610, used since 1969 as technical reference for TSO C90(c), had become largely obsolescent, not properly understood by many of its users, and still contained errors while document sponsor AIA stated they were not going to update or revise this document. This consensus was initially reached at the International Standardization Organization (ISO) TC20/SC9 Air Cargo Sub-Committee meeting Nr 29 (1998, Memphis TN), which hence agreed to prepare a corrigendum (published 2001) to ISO 8097 (based on NAS 3610), and to entrust SAE AGE-2A, on behalf of the industry, with identification of the needs for a replacement document. AGE-2A thus created in 1999 the OSP, which undertook a systematic review of the air cargo industry’s actual requirements and the step by step development and discussion of AS 36100. AS36100 Revision A (published 2006-04) was subsequently developed in 2005 by AGE-2A in order to obviate the first edition's identified shortcomings prior to expected TSO C90(d) publication. 1.1.3 The scope of the OSP work, thus the present AIR, also included other documents - some of which existed, some of which were subsequently developed - associated with AS36100 or supplementing it, covering such other areas as continued airworthiness requirements, design and testing methods, unit load devices design specifications and accessories, and rules for their proper operation/utilization and operating staff training. A list of the identified areas is provided under 1.1 of AS36100. See 2.1.2 hereafter for other associated documents concerned. 1.2 Field of Application 1.2.1 The present AIR is intended to provide future users of AS36100, including Airworthiness Authorities, unit load devices designers, purchasers and operators as well as civil transport aircraft and aircraft cargo systems or ULD designers within the industry, with the background and rationales of the requirements and parameters retained therein, in order to achieve full understanding of the technical justifications for these requirements. 1.2.2 In the same way, it is intended to provide AGE-2A members with means to re-examine provisions of AS36100 for any future revisions resulting from operational experience or the evolutions of industry needs, while keeping track of the originally retained rationales. 1.2.3 It is intended such revisions will be evaluated by the AGE-2A permanent Airworthiness Panel established to continuously monitor AS36100 and the associated documents, and the rationales for these revisions documented and recorded at that time.strRefField
【与前一版的变化】

引用文件/被引文件

Track and Stud Fitting for Cargo Transport Aircraft
Air Cargo Unit Load Devices - Performance Requirements and Testing Parameters
Air Cargo Unit Load Devices - Load Distribution Model
Air Cargo Unit Load Devices - Test Methods
Air Cargo Unit Load Devices - Center of Gravity Control Methods
Air Cargo Pallets and Nets Compatibility
Air Cargo Unit Load Devices - Reference Standards [Bibliography]
Air Cargo Unit Load Devices - Use of Airworthiness Reference Documents
Cargo unit load devices - Specification for - [Revision 10
Aircraft - Rail and stud configuration
Aircraft - Minimum airworthiness requirements and test conditions for certified air cargo unit load devices [4 th edition
Air cargo equipment - Cast component of double-stud fitting assembly with a load capacity of 22 250 N (5000 lbf ) for aircraft cargo restraint
Aircraft - Pressure equalization requirements for cargo containers
Air cargo unit load devices - Performance requirements and test parameters [ETSO C90(d) pending]
Air Cargo Unit Load Devices - Use of Airworthiness Reference Documents

包含图表

PROPOSALS TO SAE AGE
PROPOSALS TO SAE AGE
TABLE 1
FIGURE 1
ULD CONFIGURATIONS R
ULD CONFIGURATIONS T
Applicable NAS 3610
TRACK
STUD
TRACK
STUD
CORRESPONDENCE TABLE
NAS 3610 restraint w
COMPUTATION ( in met
Since ultimate loads
NOMINAL DIMENSIONS
NOMINAL DIMENSIONS 2
GENERAL TOLERANCES
TABLE 2
7G-01
FORMULA 2
Figure 1
TABLE 3
COMPUTATION ( in met
The following compat
A summary of the ult
SAE AS 36100
TYPICAL CALCULATIONS
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Only sizes A, B and
The ULD testing rest
FORMULA 3
TABLE 4
FORMULA 4
TABLE 5
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