1、MIL-STD-3001-5(AS)15 May 2001SUPERSEDING(See Section 6.)DEPARTMENT OF DEFENSESTANDARD PRACTICEDIGITAL TECHNICAL INFORMATIONFORMULTI-OUTPUT PRESENTATIONOFTECHNICAL MANUALSAIRCRAFT WIRING INFORMATION(PART 5 OF 8 PARTS)AMSC A7194 AREA TMSSDISTRIBUTION STATEMENT A. Approved for public release; distribut
2、ion is unlimited.NOT MEASUREMENTSENSITIVEProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3001-5(AS) ii FOREWORD 1. This eight-part standard establishes the requirements needed to prepare digital technical information for multi-output presenta
3、tion of NAVAIR work package Technical Manuals (TMs). The technical content and mandatory style and format requirements contained in this eight-part standard can be used to develop and assemble complete TMs for aircraft weapon systems, aeronautical equipment, airborne weapons/equipment, and support e
4、quipment work package technical manuals. The requirements are applicable for the output of paper technical manuals or for the display of page-orie nted, scrollable and frame-based technical manuals on an Electronic Display System (EDS). 2. MIL-STD-3001-5 is Part 5 of 8 Parts and is incomplete withou
5、t Parts 1 through 4 and Parts 6 through 8. Part 5 establishes the technical content requirements for the preparation of wiring information for the aircraft and its systems, subsystems, and equipment. This data can be used to develop TMs in a variety of output forms, including interactive screen pres
6、entations and page-based, printed manuals. 3. MIL-STD-3001-1 contains general preparation requirements for the multi-output presentation of NAVAIR work package TMs. MIL-STD-3001-2 through MIL-STD-3001-8 contain specific functional technical content requirements for the preparation of all NAVAIR work
7、 package TMs and revisions. Parts 1 through 8 are identified below. MIL-STD-3001-1 Preparation of Digital Technical Information for Multi-output presentation of Technical Manuals. MIL-STD-3001-2 Description, Principles of Operation, and Operation Data. MIL-STD-3001-3 Testing and Troubleshooting Proc
8、edures. MIL-STD-3001-4 Maintenance Information with IPB. MIL-STD-3001-5 Aircraft Wiring Information. MIL-STD-3001-6 Structural Repair Information. MIL-STD-3001-7 Periodic Maintenance Requirements. MIL-STD-3001-8 Separate Illustrated Parts Breakdown (IPB). 4. MIL-HDBK-3001, Guide to the General Style
9、 and Format of U.S. Navy Work Package Technical Manuals, complements this eight-part standard. MIL-HDBK-3001 provides Navy-preferred, nonmandatory style and format requirements for the preparation of page-oriented, scrollable and frame-based work package technical manuals. 5. Beneficial comments (re
10、commendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commander, Naval Air Warfare Center Aircraft Division, Code 414100B120-3, Highway 547, Lakehurst, NJ 08733-5100 by using the Standardization Document Improvement Proposa
11、l (DD Form 1426) appearing at the end of this document or by letter. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3001-5(AS) CONTENTS PARAGRAPH PAGE iii FOREWORDii 1. SCOPE.1 1.1 Scope 1 2. APPLICABLE DOCUMENTS.1 3. DEFINITIONS.1 4. GENERA
12、L REQUIREMENTS1 4.1 General1 4.2 Maintenance level applicability.1 4.3 Selective application and tailoring.1 4.4 Preparation of digital data for electronic delivery .1 4.4.1 Use of the DTDs .1 4.5 Technical content .1 4.5.1 Work packages2 4.5.2 Style and format requirements 2 4.6 Standard tables and
13、 lists2 5. DETAILED REQUIREMENTS.2 5.1 Preparation of aircraft wiring information 2 5.2 Work package content 2 5.2.1 Title block (Aircraft Wire Bundle Manual and Aircraft Wiring Connector Repair Manual only)2 5.2.2 Work package information (Aircraft Wire Bundle Manual and Aircraft Wiring Connector R
14、epair Manual only)3 5.2.2.1 Reference material list 3 5.2.2.2 Record of Applicable Technical Directives .3 5.2.2.3 Support equipment required list 4 5.2.2.4 Materials required list .5 5.2.2.5 Additional work package information (ETMs and IETMs only).5 5.2.3 Required aircraft wiring diagram informati
15、on 5 5.2.3.1 Identification and numbering of aircraft wires, cables, harnesses, and other miscellaneous parts.6 5.2.3.2 Wiring diagram identification and information work package 6 5.2.3.3 Wiring diagram work packages 6 5.2.3.4 Wire list work packages7 5.2.3.4.1 Wire run list work package .7 5.2.3.4
16、.2 Wiring reference designation list work package .7 5.2.3.5 Wire and connector component identification and location list work package 8 5.2.4 Required aircraft wire bundle information.8 5.2.4.1 Wiring system bundle assembly identification and information work package 8 5.2.4.2 Access information w
17、ork package 9 5.2.4.3 Wire bundle assembly routing work packages 9 5.2.5 Required aircraft wiring connector repair information9 5.2.5.1 Development of aircraft wire connector repair work packages .9 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL
18、-STD-3001-5(AS) CONTENTS PARAGRAPH PAGE iv 5.2.5.2 Wiring systems repair identification and information work package 10 5.2.5.3 Wiring system component repair tool list work package (standard military type components only).10 5.2.5.4 Aircraft specific wiring systems repair kit work package 10 5.2.5.
19、5 Wire type list work package .11 5.2.5.6 Aircraft specific repair tools work package 11 5.2.5.7 Wiring system component repair work packages 11 5.2.5.7.1 Terminals, ring tongue crimped barrel installation 13 5.2.5.7.2 Shielded terminal ferrules (high temperature).13 5.2.5.7.3 Electrical cable assem
20、blies sealing 13 5.2.5.7.4 Circular and rectangular connectors 13 5.2.5.7.5 Single contact and triaxial connectors14 5.2.5.7.6 Protective boot installation for environmental type connectors with metal or molded plastic cable clamps 14 5.2.5.7.7 Fabrication of shielded harness terminated with electro
21、magnetic interference backshells.15 5.2.5.7.8 Silicone rubber tape boots.16 5.2.5.8 Aircraft cable assembly parts data work package 16 6. NOTES.17 FIGURE FIGURE 1. Example of aircraft wiring systems circuit identification. 18 FIGURE 1. Example of aircraft wiring systems circuit identification - cont
22、inued. 19 FIGURE 1. Example of aircraft wiring systems circuit identification - continued. 20 FIGURE 1. Example of aircraft wiring systems circuit identification - continued. 21 FIGURE 2. Example of wire identification. .22 FIGURE 3. Example of an aircraft wire run list. 23 FIGURE 4. Example of a wi
23、ring reference designation list. 24 FIGURE 5. Example of a reference designation aircraft section identification. .25 FIGURE 5. Example of a reference designation aircraft section identification - continued. .26 FIGURE 6. Example of an access door and area location list. .27 FIGURE 6. Example of an
24、access door and area location list - continued. 28 FIGURE 7. Example of aircraft wire bundle routing. 29 FIGURE 8. Example of an aircraft wire bundle parts list. .30 FIGURE 9. Example of a wire type list. 31 FIGURE 10. Example of cable assembly repair parts data. .32 Provided by IHSNot for ResaleNo
25、reproduction or networking permitted without license from IHS-,-,-MIL-STD-3001-5(AS) 1 1. SCOPE. 1.1 Scope. This part of the standard establishes the technical content requirements for the preparation of wiring information for the aircraft and its systems, subsystems, and equipment. This data can be
26、 used to develop Technical Manuals (TMs) in a variety of output forms, including interactive screen presentations and page-based, printed manuals. 2. APPLICABLE DOCUMENTS. The applicable documents in section 2 of MIL-STD-3001-1 apply to this Part. 3. DEFINITIONS. The definitions in section 3 of MIL-
27、STD-3001-1 apply to this Part. 4. GENERAL REQUIREMENTS. 4.1 General. Sufficient information shall be developed necessary for a user to familiarize and comprehend the wiring for the aircraft weapon system, subsystem and equipment. Wiring diagrams and/or wiring lists shall be included. In addition, sp
28、ecific wire and connector repair information peculiar to the aircraft being covered shall also be developed. This wiring data shall be used by organizational level personnel to support associated aircraft maintenance procedures and to perform maintenance on aircraft wiring systems. 4.2 Maintenance l
29、evel applicability. Requirements contained in this standard are applicable to all types and maintenance levels of TMs unless specifically noted in bold and in parentheses (i.e., Support Equipment Manuals only, Depot Level only, etc.). 4.3 Selective application and tailoring. This Part contains some
30、requirements that may not be applicable to the preparation of all technical manuals. Selective application and tailoring of requirements contained in this Part shall be accomplished through the use of the Technical Manual Content Selection Matrixes contained in MIL-STD-3001-1, Appendix A. The applic
31、ability of some requirements is also designated by one of the following statements: unless specified otherwise by the requiring activity or as/when specified by the requiring activity. 4.4 Preparation of digital data for electronic delivery. Technical manual data prepared and delivered digitally in
32、accordance with this Part shall be SGML-tagged and assembled using the modular Document Type Definition (DTD). Refer to MIL-STD-3001-1 for information on obtaining or accessing this modular DTD. SGML tags used in the modular DTD are noted throughout the text of this standard in bracketed, bold chara
33、cters (i.e., ) as a convenience for the TM author and to denote the appropriate tag to be used for the specific information when developing a document instance. 4.4.1 Use of the DTDs. The modular DTDs referenced in this Part interpret the technical content and structure for the functional requiremen
34、ts contained in this Part and are mandatory for use. 4.5 Technical content. Technical content requirements contained in this Part are considered mandatory and are intended for compliance. The content structure for the technical data being developed shall conform to the associated modular Document Ty
35、pe Definition (DTD) for Aircraft Wiring information. For examples of typical technical content for specific work packages covered in this standard, refer to MIL-HDBK-3001. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3001-5(AS) 2 4.5.1 Wor
36、k packages. There are basically two types of work packages (WPs). The first type is an information-oriented work package. It provides support information such as principles of operation, general descriptive information, and controls and indicators descriptions for the weapon system/ equipment. Addit
37、ional data that supports procedural and maintenance tasks, such as lists of materials required, lists of support equipment, etc., are also considered information-oriented WPs. The second type of WP is task-oriented. Task-oriented WPs reflect all required maintenance or operation tasks at the assigne
38、d level of maintenance, and environment, material, and support equipment required for each defined task. WPs shall reflect the maintenance concept developed from the Logistics Support Analysis (LSA) or Logistics Management Information (LMI), the Level of Repair Analysis (LORA), or the approved maint
39、enance plan, and the established repair concept (SM repetition of the manual title and publication number is not required. f. Additional WPs within the same manual that are required to complete the task or discussion shall be presented first in numerical sequence. The WP title and WP number shall al
40、so be identified. The publication number is not required. g. Referenced publications not prepared in WP format shall be presented in numerical sequence. The title and publication number shall also be included. 5.2.2.2 Record of Applicable Technical Directives . Technical directives applicable to a s
41、pecific work package shall be listed in a record of applicable technical directives list (standard list). If no technical directives apply, the heading “Record of Applicable Technical Directives“ shall be omitted from the work package. The record of technical directives shall be prepared in accordan
42、ce with the following guidelines. a. All issued technical directives having any impact on the WP shall be listed upon incorporation into the WP. b. Approved engineering change proposals (ECPs) that have no effect on retrofit of the end item, shall not be listed in the record of applicable technical
43、directives (e.g., “no technical directive will be issued“). Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3001-5(AS) 4 c. All technical directives and related ECPs or Rapid Action Minor Engineering Changes (RAMECs) shall be listed upon inco
44、rporation into the WP. (1) “TD Type/No.“ - Enter the type and number of the technical directive, e.g., “A6 AFC 454“ or “AVC 1492.“ Note: The “TD Type/No.“ is identified on the Change Control Board (CCB) formal letter of ECP or RAMEC approval. Refer to NAVAIR 00-25-300. (2) “TD Date“ - Enter the date
45、 of issue of the technical directive. If the number of the technical directive has been assigned but the directive has not been issued, a dash (-) shall be entered. (3) “Title and ECP/RAMEC No.“ - The title of the technic al directive and the ECP number or RAMEC, if applicable, shall be listed. If a
46、 technical directive listed is the direct result of an approved ECP or RAMEC, the acronym ECP or RAMEC and number shall be shown in parentheses following the technical directive title. (4) “Date Inc.“ - The date the information affected by the technical directive or the ECP was incorporated into the
47、 WP. (a) If the technical directive number has been assigned and the directive has not yet been issued (retrofit program), but the ECP that incorporates the change in the production program has been approved, the production ECP coverage shall be included, and the notation “Production coverage only“
48、shall be entered under “Remarks.“ (b) When the retrofit TD is approved and incorporated in a change or revision following the incorporation of the production ECP coverage, the TD date of issue shall be entered under “TD Date,“ the notation “Production coverage only“ shall be removed from under “Rema
49、rks,“ and the date of retrofit coverage incorporation shall be listed under “Date Inc.“ (in lieu of the production ECP coverage incorporation date). (5) “Remarks“ - Enter any applicable remarks. 5.2.2.3 Support equipment required list . All support equipment (SE), including special tools required to perform operational type procedures, shall be listed (standard list) immediately following the record of applicable technical
