標(biāo)準(zhǔn)號(hào)：SAE AIR 36106A-2008
中文標(biāo)準(zhǔn)名稱(chēng)：空運(yùn)貨物成組裝運(yùn)設(shè)備.耐飛性參考文件的使用
英文標(biāo)準(zhǔn)名稱(chēng)：Air Cargo Unit Load Devices - Use of Airworthiness Reference Documents
標(biāo)準(zhǔn)類(lèi)型：V50
發(fā)布日期：2008/8/13 12:00:00
實(shí)施日期：1999/12/31 12:00:00
中國(guó)標(biāo)準(zhǔn)分類(lèi)號(hào)：V50
國(guó)際標(biāo)準(zhǔn)分類(lèi)號(hào)：49.120
引用標(biāo)準(zhǔn)：SAE AS 1825;SAE ARP 1334;SAE AS 33601;SAE AS 36100A;SAE AS 36101;SAE AS 36102;SAE ARP 36103;SAE ARP 36104A;Title 14 CFR (FAR) Part 21;SAE AIR 3610**;SAE AIR 36108;FAA Technical Standard Order (TSO) C90, Cargo Pallets, Nets and Containers;Title 14 CFR (FAR
適用范圍：1.1 Purpose1.1.1 This SAE Aerospace Information Report (AIR) provides instructions for intended proper use of Aerospace Standard AS36100A, published 2006-04 [TSO pending], as the technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded on board civil transport aircraft. For consistency and cross-checking purposes, it also includes instructions for proper use of previous NAS 3610 [Revision 10, 1990, referenced in TSO C90c], as commonly understood by the industry.1.1.2 This AIR does not provide detailed background or rationale for the technical contents of AS36100A, which are separately provided in AIR36108, AS36100A background and development record.1.1.3 AS36100A exclusively defines the general geometric parameters (insofar as they affect restraint on board aircraft), minimum performance requirements and testing parameters of unit load devices. Additional areas as perAS36100A paragraph 1.1, such as continued airworthiness and maintenance requirements, design and testing methods, unit load devices design specifications and accessories, and rules for proper operation/utilization andoperating staff training also need to be considered for designing unit load devices, and are covered by other documents, listed in AIR3610**.1.2 Field of Application1.2.1 This AIR is intended to provide AS36100A users including Airworthiness Authorities, unit load devices designers, purchasers and operators as well as civil transport aircraft and aircraft cargo systems designers within the industry,with a single agreed method for using AS36100A to determine applicable airworthiness requirements.1.2.2 In the same way, it is intended to provide them with the commonly understood though more complex method for using NAS 3610 [Revision 10, 1990, referenced in TSO C90c], to determine the airworthiness requirements applicable to unit load devices approved or to be approved under TSO C90c (e.g., because their size or type arenot covered in AS36100A).