SAE AS 8091-1999
飞行器连接千斤顶支承点的设计和安装

Adapter, Aircraft, Jacking Point, Design and Installation of FSC 1730; Should Be Used Instead of MIL-STD-809B, Which Was Cancelled on 1 July 1999


 

 

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标准号
SAE AS 8091-1999
发布日期
1999年04月01日
实施日期
废止日期
中国标准分类号
V22
国际标准分类号
49.035
发布单位
US-SAE
代替标准
SAE AS 8091A-2014
适用范围
1.1 Purpose:This standard provides requirements for design and installation of aircraft jacking point adapters, asidentified by ASCC AIR STD 25/7 Aircraft Jacking Pads, to permit use of standard jackingequipment.1.2 Classification:Each adapter shall be classified by type and class.1.2.1 Types: The design of the adapter shall be determined as to type by the loads imposed as follows:Type I - Primary flight structure adapters for reactions of less than 10,000 pounds (4536 kg).Type II - Primary flight structure adapters for reactions of 10,000 (4536 kg) to 112,000 pounds(50,803 kg).Type III - Axle adapters for reactions of less than 10,000 pounds (4536 kg).Type IV - Axle adapters for reactions of 10,000 (4536 kg) to 150,000 pounds (68,000 kg).Type V - Axle or primary flight structure adapters for reactions of 150,000 (68,000 kg) to 300,000pounds (136,080 kg).1.2.2 Classes: All types of adapters shall be designed in accordance with one of the following classes;Class 1 - Removable when the aircraft is flown.Class 2 - Integral or permanently attached.




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