NAVY MIL-L-85314 A-1983 LIGHT SYSTEMS AIRCRAFT ANTI-COLLISION STROBE GENERAL SPECIFICATION FOR《飞机照明频闪防撞系统一般规定》.pdf
《NAVY MIL-L-85314 A-1983 LIGHT SYSTEMS AIRCRAFT ANTI-COLLISION STROBE GENERAL SPECIFICATION FOR《飞机照明频闪防撞系统一般规定》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-L-85314 A-1983 LIGHT SYSTEMS AIRCRAFT ANTI-COLLISION STROBE GENERAL SPECIFICATION FOR《飞机照明频闪防撞系统一般规定》.pdf(20页珍藏版)》请在麦多课文档分享上搜索。
1、- m fl43-57 MIL-L-853 14A 30 June 1983 L SUPBRBEDINC 27 December 1982 MIL-L-85314 MILITARY SPECIFICATION LIGHT SYSTEMS, AIRCRAFT, ANTI-COLLISION, STROBE, GENEW SPECIFICATION FOR This specification is approved for use by all Departments and Agencies of the Department of Defense, 1. SCOPE . -. * 1.1 S
2、cope. This specification covers the general require- ments for two types of anti-collision, aircraft lighting strobe systems, The lighting system shall be defined as thg total number of lightheads and power supplies required to provide 360 protctve lighting in the horizontal pane of the aircraft. pr
3、ovided by the lighting system is dependent on the system selected in accordance with the applicable specification sheet. Vertical protective lighting coverage 1*2 Classification, Strobe anti-collision, aircraft light systems shall be of the following types, as specified (see 6.2): Type I - For use w
4、ith 28 volt direct current (VDC) aircraft power source Type II - For use with one phase of a three phase 115 volt alternating current (VAC) 400 hertz (Hz) aircraft power source 2, APPLICABLE DOCUMENTS 2.1 Government documents, 2.1.1 Specifications, stanards, and handbookg, Unless otherwise specified
5、, the following specifications, standards, and handbooks of the issue listed in that issue of the Department of Defense Index of Specifications and Standards (DoDfSS) specified in the solicitation form a part of this specification to the extent specified herein, Beneficial comments (recommendations,
6、 additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commanding Officer, ESSD, Code 93, Naval Air Engiqesring Center, Lakehurst, NJ 08733, by using the self-addreesed Btanderdizstion Docunient Improvement Proposal (DD Form 1426) appeari
7、ng at the end of . thio, document or by letter. I / -3 THIS DOCUMENT CONTAINS 20 PAGES. ;- FSC 6220 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SPECIFICATIONS 3r p.lita.rJ MIL-W-5088 MIL-E-5400 MIL-S-7742 MIL-E-17555 MIL-C-25050 MIL-C-38999 STAND
8、ARD6 Federal FED-STD-395 Military DOD-STD-100 MIL-STD-105 MIL-STD-129 MIL-STD-130 ML-STD-454 MIL-STD-461 MIL-STD-462 MIL-L-85314A Wiring, Aerospace Vehicle Electronic Equipment, Aerospace, General Specification E or Bcrew Threads, Btandard, Optimum Helecteid Geriee, General BpeciEication for Electro
9、nic and Electrical Equipment, Acceeaories and Repair Parts! Packaging and Packing of Color, Aeronautical Light8 and Lighting Equipment, General Requiremente for Connector, Electrical, Circular, Miniature, HI. Density I Quick Disconnect, (Bayonet, Threaded and Breech Coupling) I Environment Reeistant
10、, Removable Crimp and Hermetic golder Contacts, General flpeciftcation for Colors Engineering Drawing Practicee Sampling Procedure8 and Tables for Impection by Attributes Marking for Shipment and Storage Identification Msrlcing of U.6. Military Property Standard General Requiremente for Electronic E
11、quipment Electromagnetic Emission and Susceptibility, Requirements for the Control of Electromagnetic Interference Electromagnetic Enterference Characteristics, Measurement of Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-L-85324A 62 7777906 OL
12、LLO T W e a a MIL-L-85314A STANPARPS (Continued) . Military_ (Gont inued) MIL-STD-704 ALrcraft, Electr,c Power Characteristics MIE-STD-781 Reliability Testa: Exponential Distribution MIL-STD-794 Parts and Equipment, Procedures or Packaging and Packing of MIL-CTD-810 Envirorimental Test Methods MIL-S
13、TD-831 Test Reports, Preparation of MIL-STD-882 System Safety Program Requirements MIL-STD-88 9 Dissimilar Metals MIL-STD-1568 Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems (Copies of specifications, standards, handbooks, drawings, and publications require
14、d by manufacturers in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting officer.) 3 . REQUIREMENTS . 3.1 Specification sheets. The individual item requirements shall be ae specified herein and in accordance with the appl
15、icable specification sheet. of this specification and the specification sheet, the latter shall govern, (If a specific requirement specified herein is not required for an item, it shall ba as indicated on the specification sheet (e.g., shock - N/A) .) In the event of any conflict between requirement
16、s 3*2 F,irst article. The strobe, anti-collision, aircraft light systems furnished under this specification shall be a product which has been inspected and passed the first article inspection specified herein (see 4.3). * 3.3 Materials and components. Materials and components shall conform to applic
17、able specifications and standards as specified herein and in the applicable specification sheet. not specified herein or in the applicable specification sheet shall be selected in accordance with MIL-E-5400. are not covered by applicable specifications or standards or which are not specifically desc
18、ribed herein or in the applicable specification sheet shall be o the best quality, of the lightest practicable weight and suitable for the purpose intended. Materials and components Materials and components which Materials used shall be self- 3 Provided by IHSNot for ResaleNo reproduction or network
19、ing permitted without license from IHS-,-,-MIL-L- 85 3 14A extinguishing, shall not give off noxious gases in harmul quantitiee, shall not give off gases in quantities sufficient to cause exploston of sealed anclosures, and shall not cause contamination of the contacte or other parts of the system w
20、hen subdected to any of the tests specified herein or environmental conditions encountered in service usage, The selection of materials shall be such ao to provide a shelf life of at least 3 years without affecting the operation of the system, Maintenance action to reform electrolytic capacitore eha
21、ll be pertniesibe ae epecified in 3.12, 3e4 moeionEevention and cuntrol, The materiae and processes coneidered in deeign, the corrosion protection during manufacturing operations, and protective treatment finishes Eiheill be eelected with the guidance of MIL-STD-1568. 3e4 e 1 Metal parts, All metal
22、parts ahall be of a corroeion reeistant material or treated in a matter ta render them adequately resistant to corroeion. 3e4elel Diesiiar metals. DissimiEai: metals as defined in MIL-STD-889 shall not be in direct contact with each other unless appropriately protected against electrolytic corrosion
23、 with protective coatinge, 3,4,2 Protective treatment. When materials are ueed in the construction of the strobe, anti-collision light syetems that are subject to corrosion in salt air or other atmospheric conditions likely to occur during service usage, they shall be protected against such corrosio
24、n in a manner that shall in no way prevent compliance with the performance requirements of this and the applicable specification eheet. Protective coatings that shall chip or scale during normal service Life or under extremes of atmoepheric conditions, shall not be ueed, treatment shall conform to r
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