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
25、an analysis of the predicted effectiveness of such operations The d. Clock time and man-hours required for each maintenance and servicing action during the tests. tions of the personnel taking such actions shall be included and shall be adequate to permit comparison to the personnel anticipated in s
26、imilar field work A brief description of the experi.ence and qualifica- e. Test activity or contractor comments on item features or requirements that, if modified, should improve the item f. to be avoided or cultivated to increase the reliability or useful life of the item Test activity or contracto
27、r comments on use or maintenance donditions g. Any of the above information that is already included in the test report body need not he repeated in the information required by this paragraph, but clear reference to the location of the data shall be included. 4.3.3 First Article tests. First article
28、 tests shall consist of all the tests described under 4.5. 4.3.3.1 First Article testin_g by the contractor. Unless otherwise speci- fied (see 6.2), one barrier aircraft arresting system shall be subjected to all tests under 4.5, except 4.5.4-, 4.5.6, and 4.5.7. The arresting system then shall be su
29、bmitted to the procuring activity for the tests specified in 4.5.4, 4.5.6, and 4.5.7. 4.4 Acceptance tests. The acceptance tests shall consist of the individual tests. 13 Licensed by Information Handling Services4,4.1 Individual tests. Each aircraft arresting system shall be subjected to the followi
30、ng tests as described under 4.5: a. Examination of product . .See 4.5.1 b. Mechanical inspection .See 4.5.2 4.5 Test methods 4.5.1 Examination of product. The aircraft arresting system shall be inspected to determine compliance with the requirements of this specification. All features and components
31、 shall be inspected with respect to materials, workmanship, dimensions, proper installation, and marking. 4.5.2 Mechanical inspection. A critical mechanical inspection shall be made of all components and parts of the aircraft arresting system to insure proper functioning of all mechanical parts, acc
32、essibility of controls and adjustments, installation, and to demonstrate interchangeability of removable parts without special matching. All components shall be moved through their maximum normal displacement and shall exhibit no malfunctioning, leakage, objectionable rough operation, or irregular m
33、ovements. The inspection shall include complete lubrication and servicing of the energy absorber unit to insure readiness for operation. 4.5.3 Environmental tests. The aircraft arresting system shall be subjected to the following tests conducted in accordance with the specified methods of MIL-STD-81
34、0: a. High temperature - method 501, procedure I, except the temperature shall be 12508 b. Low temperature - method 502, procedure I, except the temperature shall be -4OOF c. Humidity - method 507, procedure I, except the temperature shall be 125OF d. Fungus - method 508, procedure I e. Salt-fog - m
35、ethod 509, procedure I f. Rain - method 506, procedure I g. Dust - method 510, procedure I, except the temperature shall be 125OF. 4.5.4 Operational test (to be conducted by the procuring activity). The aircraft arresting system shall be functionally tested against manned aircraft to determine compl
36、iance with the requirements specified herein. These tests shall be conducted over a full range of aircraft weights and speeds as specified in 3.8.2.and shall include engagements made on-center and off-center up to 50 feet. 4.5.4.1 Energy absorber temperature. The energy absorber shall be engaged at
37、short-cycle intervals for 20 highyenergy arrestments in 1 hour during which time no critical energy absorber component shall exceed a temperature which would deteriorate or degrade system performance. The energy absorber shall be 14 Licensed by Information Handling Services0 L 8 o O I MIL-B-83183B 1
38、7 H 77777Ob 0205745 b MIL-B-83183B(USAF) capable of meeting the requirements specified in 3.8. 4.5.5 Electromagnetic interference. The aircraft arresting system shall be tested or electromagnetic interference, through all operations of. a com- plete arrestment cycle, in accordance with MIL-STD-826,
39、method 7001. 4.5.6 Reliability demonstration and testing (to be conducted by the procur- The entire arresting system shall be installed and tested under ing activity). operational conditions at a designated test site or operational base. This testing will be accomplished by the procuring activity. H
40、owever, on-site technical support personnel shall be provided when specified (see 6.2). 4.5.7 Maintainability evaluation (to be conducted by the procuring actviity). The aircraft arresting system shall be inspected and evaluated from the standpoint of ease of maintenance, servicing, and operation. P
41、articular attention shall be given maintenance with a minimum number of common tools, servicing, and operation by personnel wearing heavy gloves, and provisions made to prevent accumulation of dirt, snow, ice, etc., that may hinder servicing and operation. procuring activity. However, on-site techni
42、cal support personnel shall be provided when specified (see 6.2). The testing will be accomplished by the * 4.6 Inspection of packaging. Preservation, packaging, packing and marking shall be inspected tb determine conformance to the requirements of Section 5, herein. * PACKAGING * 5.1 Preservation a
43、nd packaging. Preservation and packaging shall be level A or Cy as specified (see 6.2). * 5.1.1 Level A * 5.1.1.1 Disassembly. Disassembly of the system components shall be accomplished to the extent practicable to reduce cube and facilitate packaging and packing of the system. * 5.1.1.2 Cleaning an
44、d drying. Component parts of the aircraft arresting svstem shall be cleaned in accordance with MIL-P-116, process C-1, and dried in accordance with MIL-P-116, procedure D-1 or D-4. * 5.1.1.3 Preservation application. Immediately after cleaning and drying, all expoied bare metal surfaces and critical
45、 parts (i.e., sprockets, gears, chain drives, etc) shall be coated with P-1 or P-2 preservative in accordance with MIL-P-116, method I. Where ease of removal is not a prime consideration, P-1 preservative should be used. * 5.1.1.4 Engines. Engines shall be preserved and packaged in accordance with M
46、IL-E-10062. * 5.1.1.5 Electrical components. Electrical components shall be preserved in accordance with MIL-E-17555. * 5.1.1.6 Instrument panel. Glass on the instrument panel shall be covered with fiberboard conforming to PPP-F-320 or other similr protective material and secured with tape conformin
47、g to A-A-1830. 15 - Licensed by Information Handling ServicesMIL-B-83183B(USAF) * 5.1.1.7 Hook cable. The hook cable (pendant) shall be preserved and packaged in accordance with MIL-STD-163. * 5.1.1.8 Purchase element tapes. Purchase element tapes shall be packaged in accordance with MIL-W-38461, ex
48、cept as modified in 5.2.1.2 herein. * 5.1.1.9 Tools. Special service tools shall be preserved and packaged in accordance with PPP-P-40. * 5.1.1.10 Kits. All kits supplied with the system shall be preserved and packaged in accordance with MIL-STD-2073-1, appendix D. * 5.1,2 Level C. The level C prese
49、rvation for the aircraft arresting system shall conform to the MIL-STD-2073-1 requirements for this level. * 5.2 Facking. Packing shall be Level A, By or C as specified (see 6.2). * 5.2.1 Level A. Components of the system, preserved and packaged as specified in 5.1, shall be packed as specified in 5.2.1.1 through 5.2.1.9. * 5.2.1.1 Energy absorber. Each energy absorber, including the purchase element tape cleaning device, shall be packed in a container conforming to MIL-C-104,- type I, class 2, style a. * 5.2.1,2 Purchase element tapes. Purchase element tapes shall be packed in -accor
