AIR FORCE MIL-H-5364 D-1972 HARNESSES SHOULDER SAFETY GENERAL SPECIFICATION FOR《肩部安全降落伞背带一般规格》.pdf
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1、MIL-H-5364D 9 March 1972 SUPERSEDING MIL-H-5364C (USAF) 29 May 1968 MLLITAY SPECIFICATION HARNESSES, SHOULDER SAFETY, GENERAL SPECIFICATION FOR This specification is mandatory for use by all Departments and Agencies of the Department of Defensc, 1. SCOPE 1.1 This specification covers the general req
2、uirements for safety shoulder harnesses for use with both ejection and nonejection seats. 2. APPLICABLE DOCUMENTS * 2.1 The following documents, of the issue in effect on date of invitation for bids or request for proposal, fonn a part of this specification to the extent specified herein. SPECIFICAT
3、IONS Fed era 1 DDD-L-20 PPP-B-60 1 PPP-B-6 36 Military MIL-P-116 MIL-1-6903 SWARDS Federal FED-STD-595 Mil it ary MIL-STD-105 MIL-STD-129 MIL-STD-143 Label; for Clothing, Equipage, and Tentage, (General Use) Box, Wood, Cleated Plywood Box, Fiberboard Preservation, Methods of Ink, Marking (For Parach
4、utes and Other Textile Items) Colors Sampling Procedures and Tables for Inspection by Attributes Marking for Shipment and Storage Standards and Specifications, Order of Preceence for the Selection of FSC 1680 h Provided by IHSNot for ResaleNo reproduction or networking permitted without license from
5、 IHS-,-,-MIL-H-5364D MU-STD-1186 Cushioning, Anchoring, Bracing, Blocking, and Waterproofing; with Appropriate Test Methods Air Force 563534 Loop - Shoulder Harness, Lap Belt Attachment (Copies of specifications, standards, drawings, and publications required by suppliers in connection with specific
6、 procurement functions should be obtained from the procuring activity or as directed by the contracting officer.) 3. REQUIREMENTS 3.1 Preproduction, This specification provides for preproduction testing. 3.2 Selection of specifications and standards, Specifications and standards for necessary commod
7、ities and services not specified herein shall be selected in accordance with MIL-STD-143. 3.3 Detail drawing. The requirements of the applicable detail drawing (see 6.3) shall form a part of this specification. * 3.4 Strength. The Types MB-2A, MB-5, and MB-6 shoulder harnesses shall be capable of wi
8、thstanding a static load of 3,600 pounds without deformation of the metal fittings, slippage of the webbing through the adjusting hardware, weakening of the webbing, or weakening of the stitching. * 3.5 Identification of product. A label conforming to DDD-L-20, type II, class 11, shall be sewn on ea
9、ch shoulder harness as shown on the applicable detail drawing. label : The following specific information shall be included on the Harness, Aircraft Safety, Shoulder Adjustable 5pe (as specified on applicable detail drawing) Specif icat ion MIL-H-5364D Stock No, Order No. Date of Manufacture Manufac
10、turers Name or Trademark * 3.5.1 Proof load marking. Each harness shall have the proof load test date (see 4.5.3) stenciled on the underside of either shoulder strap, The informa- The month shall be indicated by the first three letters of the word and the year by the last two . tion shall include th
11、e letters PL followed by the date of test. I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-H-53bYD 16 W 777770b OLBYbL3 3 MIL-H-5364D numerals (example: The markings shall be made with ink conforming to MIL-1-6903, color No. 13538 of Jan 68“ wi
12、ll indicate a proof load date of January 1968). FED-STD-595 3.6 Workmanship. The harness, including all parts and accessories, shall be constructed and finished in a thoroughly workmanlike manner. tion shall be given to freedom of parts from burrs and sharp edges. 4. QUALITY ASSURANCE PROVISIONS Par
13、ticular atten- 4.1 Responsibility for inspection. Unless otherwise specified in the con- tract or purchase order, the supplier is responsible for the performance of all inspection requirements as specified herein. the contract or order, the supplier may use his own or any other facilities suitable f
14、or the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the specification where such inspec- tions are deemed necessary to assure supplies and services conform to prescr
15、ibed requirements Except as otherwise specified in * 4.2 Classification of inspections. The examining and testing of harnesses shall be classified as follows: (a) Preproduction inspect ion (b) Quality conformance inspection. * 4.3 Preproduction inspection. The preproduction test sample, consisting o
16、f one harness of each type on the.contract or order, shall be subjected to the following examinations and tests as described under 4.5: (a) Examination of product (4.5.1) (b) Examination of loop (4.5.2) (c) Ultimate load (4.5.4). * 4.4 Quality conformance inspection. Quality conformance inspection s
17、hall consist of: (a) Individual inspection ) Sampling inspection. 3 , Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-H-5 36411 * 4.4.1 Individual inspection. Each harness shall be subjected to the follow- ing examinations and test as described u
18、nder 4.5: (a) Examination of product (4.5.1) (b) Examination of loop (4.5.2) (c) Proof load (4.5.3). * 4.4.2 Sampling inspection. Unless otherwise specified by the procuring activity (see 6.2), harnesses shall be sampled in accordance with inspection level S-3 of Mu-STD-105. The acceptable quality l
19、evel shall be 1.5 percent defective. The test samples shall be subjected to the ultimate load test as described in 4.5.4. * 4.5 Inspection methods 4.5.1 Examination of product. The harness shall be examined to determine conformance to this specification with respect to materials, workmanship, dimens
20、ions, and markings. * 4.5.2 Examination of loop. Each end loop of each shoulder harness shall be examined to determine conformance to this specification with respect to dimen- sions. This examination shall be conducted on the MB-U and MB-6 harness loops only, subsequent to the proof load test after
21、a waiting period of not less than 24 hours. Loop acceptability shall be determined by use of an inspection tool conforming to figure 1. The inspection tool shall be held in one hand and the harness loop pushed over the small end of the tool with the sewn end of the loop against the chamfered side of
22、 the tool. up the tool as can be done easily without using excessive force. is defined as holding the loop tightly and pushing it by hand pressure only without bracing the tool upon or against anything. up the tool to such an extent as to cause the loop material to stretch or the threads to pull. Th
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