AIR FORCE MIL-B-83183 B-1987 BARRIER AIRCRAFT ARRESTING《飞机拦阻挡板》.pdf
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1、-. . MIL-B-83183B 17 m 9999906 0205733 6 WG MIL- B-8 3 18 3 B (USAI? 1 6 APRIL 1987 SUPERSEDNG MIL-A-83183A(USAF) 23 March 1971 MILITARY SPECIFICATION BARRIER AIRCRAFT ARRESTING This specification is approved for use within the Department of the Air Force and is available for use by all departments
2、and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers a portable, rotary, hydraulic, barrier aircraft arresting system, designated BAK-l3A/F48A. 2. APPLICABLE DOCUMENTS A 2.1 Government documents. * 2.1.1 Specifications and standards. The following specifications a
3、nd standards form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of these documents shall be those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement thereto, cited in the solicitation. S
4、PECIFICATIONS FEDERAL .L .I- A A A .a. .- A-A-1 8 3 O TT-V-121 UU-L-81 PPP-B-601 PPP-B-621 PPP-F-320 PPP-P-40 MILITARY MIL-C-104 A MIL-P-116 3- Tape Pressure Sensitive Adhesive Box Closure Varnish, Spar, Water Resisting Tag, Shipping and Stock Box, Wood, Cleated Plywood Box, Wood , Nailed and Lock-C
5、orner Fiberboard, Corrugated and Solid, Sheet Stock (Container Grade) and Cut Shapes Packaging and Packing of Hand Tools Crate, Wood, Lumber and Plywood Sheathed, Nailed and Bolted Preservation, Methods of Beneficial comments (recommendations, additions, deletions) and any pertinent data which may b
6、e of use in improving this document should be addressed to: the Engineering Division, San Antonio ALC/MMEDO, Kelly AFB, Texas 78241 by using the self addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. I AMSC NIA - THIS DOCUMENT
7、CONTAINS lq PAGES. FSC 1710 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Licensed by Information Handling ServicesMIL-P-514 MIL-G-8402 * MIL-E-10062 * MIL-E-17555 MIL-W-38461 STANDARDS FEDERAL FED-STD-H28 MILITARY MIL-STD-12 MIL-STD-17 DOD-STD-100 * MIL-STD-129 M
8、IL-STD-130 MIL-STD-143 * MIL-STD-147 .k MIL-STD-163 MIL-STD-808 MIL-STD-810 MIL-STD-826 MIL-STD-831 MIL-STD-889 * MIL-STD-1186 * MIL-STD-2073 Plate, Identification, Instruction and Marking, Blank Gages, Pressure, Dial Indicating, General Specification for Engines, Preparation for Shipment and Storag
9、e of Electronic and Electrical Equipment, Accessories and Provisioned Items (Repafr Parts) Packaging of Webbing, Nylon, Aircraft Arresting Screw Thread Standards for Federal Services Abbreviations for Use on Drawings, Specifications, Standards, and in Technical Documents Mechanical Symbols Engineeri
10、ng Drawing Practices Marking for Shipment and Storage Identification Marking of U.S. Military Property Standards and Specifications, Order of Precedence for the Selection of Palletized Unit Loads Steel Mill Products, Preparation of Shipment and Storage Finish, Materials and Processes for Corrosion P
11、revention and Control in Support Equipment Environmental Test Methods and Engineering Guidelines Electromagnetic Interference Test Requirements and Test Methods Test Reports, Preparation of Dissimilar Metals Cushioning, Anchoring, Bracing, Blocking, and with Appropriate Test Methods DOD Materiel Pro
12、cedures for Development and Application of Packing Requirements 2.1.2 Other Government documents, drawings, and publications, The follow- ing other Government documents, drawings, and publications form a part of this specification to the extent specified herein. Unless otherwise specified, the issue
13、s shall be those in effect on the date of the solicitation. DRAWINGS Air Force 71211 71214 BAK-13A Arresting System Foundations, Hardware Kit Assembly, Anchoring and Leveling Hardware, BAK-13A Arresting System Foundations Structural Plans Licensed by Information Handling ServicesMIL-B-831838 17 9979
14、906 0205733 T W MIL-B-83183B (USAI?) Naval Air Engineering Center (Code 80020) 510445 Tape Connector Assembly 515053 Pendant Assembly E. W. Bliss Company 52-E-182 thoroughness of soldering, welding, brazing, painting, wiring, and riveting; alignment of all parts, and tightness of assembly screws and
15、 bolts. 3.22.1 Cleaning. The aircraft arresting system shall be thoroughly cleaned and loose, spattered, or. excess solder; metal chips; and other foreign material removed during and after -final assembly. 4. QUALITY ASSURANCE PROVISIONS * 4.1 Responsibility for inspection. Unless otherwise specifie
16、d in the con- tract or purchase order, the contractor is responsible for the performance of all inspection requirements as specified herein, Except as otherwise specified in the contract or purchase order, the contractor may use his own or any other facilities suitable for the performance of the ins
17、pection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the specifi- cation where such inspections are deemed necessary to assure supplies and services conform to prescribed requirements. * 4.1.1 Re
18、sponsibility for compliance. All items must meet all requirements of sections 3 and 5. become a part of the contractors overall inspection system or quality program. The absence of any inspection requirements in the specification shdl not relieve the contractor of the responsibility of assuring that
19、 all products or supplies submitted to the Government for acceptance comply with all require- ments of the contract. submission of known defective materia1,either indicated or actual, nor does it commit the Government to acceptance of defective material. The inspection set forth in this specificatio
20、n shall Sampling in quality conformance does not authorize 4.2 Classification of tests. The inspection and testing of the aircraft arresting system shall be classified as follows: a. First Article testing . . . . . . . . . . , . . . . . , . See 4.3 i2 Licensed by Information Handling ServicesMIL-B-8
21、3183B(USAF) b. Acceptance tests . . . . . . . . . . . . . . . . . . . . . . .See 4.4. 4.3 First Article testing (see 6.2) 4.3.1 Test sample. One barrier aircraft arresting system shall be subjected to the tests specified in 4.3.3. 4.3.2 Test report. After completion of first. article testing, a test
22、 report shall be prepared in accordance with MIL-STD-831 and three copies furnished to the procuring activity. 4.3.2.1 Reliability and maintainability information. The following infor- mation shall be included as an appendix to the test report: a. All failures, servicing, adjustments, maintenance, a
23、nd irregular functioning shall be identified by accumulated operating time, cycles, and miles or position in the test procedure, as approprrate. the time of the events identified shall be recorded ./. . Test conditions at b. A summary of the engineering analysis and tests conducted to determine assi
24、gnable. causes for any failure or irregular functioning c. A summary of the engineering analysis leading to any corrections made to design, construction, quality control or other procedures, or leading to any corrections or changes proposed to be made to production items. summary shall also include
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