AIR FORCE MIL-Q-87152 A-1992 QUICK RELEASE PERSONNEL PARACHUTE HARNESS MX-683(V) 1P《MX-683(V) 1P快速释放单人降落伞吊带》.pdf
《AIR FORCE MIL-Q-87152 A-1992 QUICK RELEASE PERSONNEL PARACHUTE HARNESS MX-683(V) 1P《MX-683(V) 1P快速释放单人降落伞吊带》.pdf》由会员分享,可在线阅读,更多相关《AIR FORCE MIL-Q-87152 A-1992 QUICK RELEASE PERSONNEL PARACHUTE HARNESS MX-683(V) 1P《MX-683(V) 1P快速释放单人降落伞吊带》.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、c. br MIL-Q-87152A lab 9999906 la165891 676 MIL-Q-87152A(USAF) 31 August 1992 SUPERSEDING 21 March 1980 MIL-Q-87152(USAF) MILITARY SPECIFICATION QUICK RELEASE, PERSONNEL PARACHUTE HARNESS MX-683(V) 1P This specification is approved for use within the Department of the Air Force and is available for
2、use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers a quick release for personnel parachute harness. The quick release is designated MXU-683(V)l/P. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications, standards. Unless ot
3、herwise specified, specifications, standards form a part of this specification to extent specified herein. listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement thereto, cited in the solicitation. Unless otherwise specified, the issues of thes
4、e documents shall be those SPECIFICATIONS FEDERAL PPP-B-6 36 Boxes, Shipping, Fiberboard MIL I TARY MIL-P-116 Preservation, Method of STANDARDS MIL I TARY MIL-STD-105 Sampling Procedures and Tables for MIL-STD-129 Marking for Shipment and Storage Inspection by Attributes. Beneficial comments (recomm
5、endations, additions, deletions) and any pertinent data which may be of use in improving this use in improving this document should be addressed to the SA-ALC/TIRDM, Kelly AFB, TX 78241-5609, by using the self-addressed Standardization Document Proposal DD Form 1426) appearing at the end of this doc
6、ument or bv letter. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-Q-87152A Lb 9999906 LLb5892 502 W ?4 MIL-STD-130 Identification Marking of US MIL-STD-831 Test Reports, Preparation of MIL-STD-970 Standards incorrect; incomplete; illegible; or
7、improper size, location, sequence, or method of application Any component missing or not as specified Any component damaged or otherwise defect ive Inadequate application of components such as incomplete closure of case liners or container flaps; loose strapping; or inadequate stapling Bulging or di
8、stortion of containers Gross or net weight exceeds requirement Quantity of hardware assemblies per container more or less than specified 4.6.4 Static operation. The components shall be subjected to the static operation test. that is capable of applying and maintaining the load specified in 3.5.3 all
9、owing access to and operation of the release assembly. mounted and restrained so that the release assembly can be operated and the load can be The quick release shall be installed in a tensile testing apparatus but still The quick release shall be 7 Provided by IHSNot for ResaleNo reproduction or ne
10、tworking permitted without license from IHS-,-,-MIL-Q-87152A(USAF) released without damage to the release assembly or the canopy link assembly and without risk of injury to the test operator. release assembly shall then be operated both manually and via calibrated spring scale. This step may have to
11、 be repeated several times before the release force stabilizes. The force required to effect release during the first static operation test shall not exceed 35 pounds. operation test shall be within plus or minus 20 percent of the force that was obtained in the first static operation test but shall
12、not exceed 35 pounds. Th( The load specified in 3.5.3 shall be applied. The force required to effect release during the second static 4.6.5 Proof load. Each major component(3.2) shall be subjected to the proof load test. Suitable lengths of nylon webbing that has a breaking strength at least equal t
13、o the ultimate strength of the hardware shall be installed in a manner simulating its use in a parachute harness section. grips. The proof load shall be sustained for 5seconds and then reduced to zero. The hardware shall be examined for freedom from permanent deformation and damage. The hardware sha
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