SAE AS 56761-1999 Splicing Cable Terminal Process for Aircraft《FSC 5130飞机电缆接头接合程序 应代替1999年10月29日作废的MIL-S-567标准》.pdf
《SAE AS 56761-1999 Splicing Cable Terminal Process for Aircraft《FSC 5130飞机电缆接头接合程序 应代替1999年10月29日作废的MIL-S-567标准》.pdf》由会员分享,可在线阅读,更多相关《SAE AS 56761-1999 Splicing Cable Terminal Process for Aircraft《FSC 5130飞机电缆接头接合程序 应代替1999年10月29日作废的MIL-S-567标准》.pdf(14页珍藏版)》请在麦多课文档分享上搜索。
1、SAE-AS56761ADOPTION NOTICESAE-AS56761, “SPLICING; CABLE TERMINAL, PROCESS FOR, AIRCRAFT“,was adopted on 29-OCT-99 for use by the Department of Defense(DoD). Proposed changes by DoD activities must be submitted tothe DoD Adopting Activity: Commander, Naval Air Warfare Center,Aircraft Division, Code 4
2、14100B120-3, Highway 547, Lakehurst, NJ08733-5100. Copies of this document may be purchased from theSociety of Automotive Engineers 400 Commonwealth DriveWarrendale, Pennsylvania, United States, 15096-0001. http:/www.sae.org/_Custodians: Adopting Activity:Navy - ASNavy - ASAir Force - 99FSC 5130DIST
3、RIBUTION STATEMENT A: Approved for public release; distributionis unlimited.SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirelyvoluntary, and its applicability and suitabilit
4、y for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright 19
5、99 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.A.QUESTIONS REGARDING THIS DOCUMENT: (724) 772-8510 FAX: (724) 776-0243TO PLACE A DOCUMENT ORDER: (724) 776-4970 FAX: (724) 776-0790SAE WEB ADDRESS: http:/www.sae.org400 Commonwealth Drive, Warrendale, PA 15096-0001AEROSPACE
6、 STANDARDAS56761Issued 1999-07Splicing; Cable Terminal, Process for, AircraftNOTICEThis document has been taken directly from U.S. Military Specification MIL-S-5676A, Amendment 1 and contains only minor editorial and format changes required to bring it into conformance with the publishing requiremen
7、ts of SAE technical standards. The initial release of this document is intended to replace MIL-S-5676A, Amendment 1. Any part numbers established by the original specification remain unchanged.The original Military Specification was adopted as an SAE standard under the provisions of the SAE Technica
8、l Standards Board (TSB) Rules and Regulations (TSB 001) pertaining to accelerated adoption of government specifications and standards. TSB rules provide for (a) the publication of portions of unrevised government specifications and standards without consensus voting at the SAE Committee level, and (
9、b) the use of the existing government specification or standard format.Under Department of Defense policies and procedures, any qualification requirements and associated qualified products lists are mandatory for DOD contracts. Any requirement relating to qualified products lists (QPLs) has not been
10、 adopted by SAE and is not part of this SAE technical document.SAE AS56761 - 2 -1. SCOPE AND CLASSIFICATION:1.1 This specification is designed to present detailed procedure to be followed in splicing cable terminals. The types of cable to which this specification applies are listed in Section 2 and
11、table I. 2. APPLICABLE SPECIFICATIONS AND DRAWINGS:2.1 The following specifications and drawings of the issue in effect on date of invitation for bids shall form a part of this specification to the extent specified herein:2.1.1 SpecificationsFederal: QQ-S-571 Solder; Soft (Tin, Tin-Lead, and Lead-Si
12、lver)V-T-276 Thread; CottonMilitaryMIL-C-1511 Cable; Steel (Carbon), Flexible PreformedMIL-C-5424 Cable; Steel (Corrosion-Resisting), Flexible Preformed (For Aeronautical Use)MIL-C-6708 Compound; Exterior-Surface, Hard-Film, Corrosive-PreventiveMIL-C-6940 Cable, Single Strand Non-Flexible Carbon Ste
13、el (Preformed)Air Force-Navy AeronauticalAN-W-22 Wire; Zinc Coated, Soft Steel2.1.2 Drawings:Air Force-Navy Aeronautical Standard DrawingAN100 Thimble - Wire Cable(Copies of this publication and copies of other publications referenced herein or required for Government procurement, and the Index of M
14、ilitary Aeronautical (AN or MIL) Standards, may be obtained upon application to the Commanding General, Air Materiel Command, Wright-Patterson Air Force Base, Dayton, Ohio; or the Commanding Officer, U.S. Naval Air Station, Johnsville, Pennsylvania.)SAE AS56761 - 3 -3. MATERIAL AND EQUIPMENT:3.1 Mat
15、erials:3.1.1 Thimbles: Thimbles shall conform to the requirements of Drawing AN100.3.1.2 Serving Cord: Serving cord shall conform to Specification V-T-276, type 111A, 12-ply.3.1.3 Preservative: The preservative shall conform to the requirements of Specification MIL-C-6708, type 1.3.1.4 Serving Wire:
16、 Serving or wrapping wire shall be in accordance with Specification AN-W-22.3.1.5 Solder: Solder shall conform to Specification QQ-S-571, class A.3.1.6 Flux: Solder flux shall be a compound of stearic acid (free from mineral acids) and rosin of the following proportions:Stearic acid 25 to 50%Rosin 5
17、0 to 75%3.2 Equipment:The following tools (see figure 14) are recommended for use in the preparation of cable terminal splices.3.2.1 Marlin Spike: This is a small pointed tool of oval cross-section with a screw driver handle.3.2.2 Side Cutting Pliers: The side cutting pliers are required for clippin
18、g off the strands after splicing.3.2.3 Splicing Clamp: A splicing clamp is useful for holding the cable in place in the thimble and in positioning the terminal during splicing operations.3.2.4 Mallet: A rawhide or hardwood mallet is needed for hammering the splice after finishing and before serving,
19、 in order to produce a neat looking splice.4. PREPARATION AND PROCEDURE:4.1 Cutting of Cable:4.1.1 Flexible Cable: The cable shall be cut to length by mechanical means only, such as a fine tooth hacksaw. The use of oxy-acetylene torches in any manner is not permitted.SAE AS56761 - 4 -4.1.2 Non-Flexi
20、ble Cable: Before cutting the cable the wires must be soldered or welded together to prevent slipping. The preferable process is to thoroughly tin and solder the cable for 2 to 3 inches by placing in a solder trough as shown in figure 15 and finishing smooth with a soldering tool. The cable may be c
21、ut diagonally to conform to the required taper finish shown in figure 16. The cable shall be cut to length by mechanical means, such as a fine tooth hacksaw, except as allowed in applicable subparagraphs under “Procedure.”4.2 Procedure:4.2.1 Operations for Flexible Cable: The procedure for the prepa
22、ration of terminal splices for flexible splices for flexible cable is described in the following paragraphs. The splice shall have five full tucks. For 1/16-inch 7 x 7 flexible steel cable, the procedure described herein for nonflexible cable may be used as an optional method.4.2.1.1 Forming of Term
23、inals: The cable shall be bent snugly around the proper size of thimble as specified in table I and clamped, the points of the thinble having previously been bent back at an angle of approximately 45 degrees to permit a close splice. If a regular splicing clamp is not available, the cable may be hel
24、d in place on the thimble by binding with cord, as shown in the accompanying illustrations. The length of the free end of the cable should be about 8 inches for sizes up to and including 5/32-inch 7 x 19 cable. For cable of larger sizes the length should be slightly greater. The standing wire should
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