1、NOT MEASUREMENT SENSITIVEMIL-STD-865110 November 1997SUPERSEDINGMIL-I-8651C10 August 1992DEPARTMENT OF DEFENSESTANDARD PRACTICEINSTALLATION OF IDENTIFICATION ANDMODIFICATION PLATES(FOR AIRCRAFT)AMSC NIA FSC 9905Provided by IHSNot for ResaleNo reproduction or networking permitted without license from
2、 IHS-,-,-MIL-STD-8651iiFOREWORD1. This standard is approved for use by all Departments and Agencies of the Department ofDefense.2. MIL-STD-8651 has been prepared to reflect current DoD policy and procedures forstandardization documents used by DoD and is redesignated as a Department of Defense stand
3、ardpractice.3. Beneficial comments (recommendations, additions, deletions) and any pertinent data whichmay be of use in improving this document should be addressed to: Commander, Naval AirWarfare Center Aircraft Division, Code 414100B120-3, Highway 547, Lakehurst, NJ 08733-5100, by using the Standar
4、dization Document Improvement Proposal (DD Form 1426) appearingat the end of this document or by letter.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-8651iiiCONTENTSPARAGRAPH PAGEFOREWORD ii1. SCOPE . 11.1 Scope . 12. APPLICABLE DOCUMENTS .
5、 13. DEFINITIONS . 13.1 Identification plate. . 13.2 Modification plate. 14. GENERAL REQUIREMENTS 14.1 Application . 14.2 Identification and modification plates. . 14.3 Categories of changes to be recorded 15. DETAIL REQUIREMENTS 15.1 Marking details . 15.2 Serial numbers. . 15.2.1 Letter designatio
6、n. 25.2.2 Number designation. . 25.2.3 Consecutive numbering. 25.3 Installation. . 25.3.1 Permane ntly attached plates. . 35.3.2 Removable plates. . 36. NOTES 36.1 Intended use. 36.2 Subject term (key word) listing. 36.3 Typical example. . 3CONCLUDING MATERIAL . 4Provided by IHSNot for ResaleNo repr
7、oduction or networking permitted without license from IHS-,-,-MIL-STD-865111. SCOPE1.1 Scope . This standard establishes the practices for the installation and modification plateson major structural aircraft assemblies.2. APPLICABLE DOCUMENTS(This section is not applicable to this standard.)3. DEFIN
8、ITIONS3.1 Identification plate . An identification plate provides information about a major assembly,subassembly or component.3.2 Modification plate . A modification plate contains information regarding anymodification or change made to a major assembly, subassembly or component.4. GENERAL REQUIREME
9、NTS4.1 Application . Identification and modification plates shall be applied to all major structuralaircraft assemblies, either installed on the complete aircraft or procured spares. This requirementdoes not apply to useful load items, engines, propellers, or other equipment items, but does applyto
10、helicopter major drive system components including transmissions, gear boxes, rotor blades,rotor heads and clutches.4.2 Identification and modification plates . Identification and modification plates used shallbe designed and manufactured to provide information (see 5.1). Lettering shall be permanen
11、t andlegible. Material shall resist deterioation.4.3 Categories of changes to be recorded . Only those changes in the following categoriesshall be recorded on the plates:a. “Hidd en“ changes (changes not readily identified by visual inspection).b. Changes affecting interchangability.c. Changes requi
12、red for safety of flight.5. DETAILED REQUIREMENTS5.1 Marking details . Marking of plates shall be as specified in table I. It is mandatory thatthe information recorded be accurate.5.2 Serial numbers . So that identification of changes may be accomplished to the fullestextent, a code system shall be
13、established for identification of all major aircraft structuralassemblies (including spares) by the serial number of the assembly rather than by the aircraft serialnumber. A typical example is shown in 6.3.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-
14、,-,-MIL-STD-86512TABLE I. Marking details .Designation RequirementAircraft model Record the military service model designation of the aircraft.Cage code Record the manufacturers codePart number Record the part number of the assembly.Serial number Record the assembly unit serial number (see 5.2)Contr
15、act number Applicable to U.S. Air Force only.Contract inspector Record the designation of the contrators inspectorCustomer inspector Record the designation of the customers inspector.Modification incorporated Add the modifications incorporatedAircraft service changes Stamp the heading “A.S.C.“ on th
16、e line directly below“Modification Incorporated,“ and record the “numbers“ of themilitary aircraft service changes incorporated in the assemblyprior to delivery5.2.1 Letter designation . The prime contractor and each subcontractor involved in themanufacture of major structural assemblies for a parti
17、cular model aircraft shall each have aseparate and distinct “letter“ designation, e.g., “A” for the prime contractor, “B” for the firstsubcontractor, and “C” for another subcontractor. The letter designations shall be assigned by theprime contractor. The letter designation of the prime contractor sh
18、all always be theletter “A”.5.2.2 Number designation . Each type of major structural assembly shall have a separate anddistinct “number“ designation. “1” may be assigned for outboard wing panels, “2” for centerpanels, “3” for ailerons, and “4” for flaps. These designations shall be assigned by the p
19、rimecontractor.5.2.3 Consecutive numbering . All structural assemblies of the same type manufactured byeach contractor shall be numbered consecutively, starting with number 1, to include thenumerically manufactured unit by the prime contractor and the respective subcontractors. Thenumerical sequence
20、 shall continue as long as a given part numbered assembly is manufactured. Ifthe part number of an assembly is changed, the units manufactured under the new part numbershall be consecutively numbered starting with number 1. If the part number of an assembly ischanged because of a modification, seria
21、lization of the new parts shall begin with the number 1.However, if rework of the superseded parts is contemplated, serialization of the new parts shall beconsecutive with the superseded part. Alternatively, a letter may be incorporated in the new partserial number, to preclude duplication of serial
22、 numbers if superseded parts are worked to the newpart configuration. Symmetrically opposite assemblies of a set shall be assigned the same serialnumber, as these assemblies will be further identified by the part numbers on the identification andmodification plates.5.3 Installation . The plates shal
23、l be mounted on the right-hand side of the fuselage or hulland on the inboard end of the right- and left-hand major structural assemblies, so as to be visibleafter final assembly. On closed assemblies, the plate shall be so located as to be accessible fromProvided by IHSNot for ResaleNo reproduction
24、 or networking permitted without license from IHS-,-,-MIL-STD-86513the hand holes or access covers and the exterior surface of access covers shall be stenciled toidentify the location of the plate.5.3.1 Permanently attached plates . Permanently attached plates shall be readily accessiblewith the ass
25、embly installed in place on the aircraft. The plates shall be installed on rigid structuralmembers so that the recording of additional information, by service activities using stamping dies,will not cause any damage or deformation of any kind to the structure to which the plate isattached.5.3.2 Remo
26、vable plates . Plates not meeting the installation requirements of 5.3.1, or notreadily accessible, shall be removable. Install removable plates with screws, bolts, clamps, orother means so that the plates can be removed for recording additional information by serviceactivities and be reinstalled. R
27、emovable plates shall be readily accessible with the assemblyinstalled in place on the aircraft.6. NOTES(This section contains information of a general or explanatory nature that may be helpful, but isnot mandatory.)6.1 Intended use . Identification and modification plates for major structural assem
28、blies areintended for identification of the assembly and for the determination of changes incorporated inthe assembly.6.2 Subject term (key word) listing .Drive systemModelPart numberSerial numberStructural assembliesWing panel6.3 Typical example . A typical example of a code system for a serial num
29、ber described in5.2 would be an outer wing panel assembly part number 83204-1 bearing the serial numberB1 -87, wherein the dash number “1“ after the part number signifies a left (or right) assembly andthe serial number is formed as follows:B - The letter designation of the subcontractor who had manu
30、factured the particular outerpanel.1 - The number designation for the all outer wing panels manufactured for the particularmodel aircraft, regardless of whether the prime contractor or subcontractor manufactured theitem(s).87 - The 87th left-hand outer wing panel manufactured by the subcontractor wh
31、osedesignation is “B”.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-86514CONCLUDING MATERIALCustodians: Preparing activity:Army - AV Navy - AsNavy - AS (Project 9905-0335)Air Force - 99Review Activities:Air Force - 84Provided by IHSNot for
32、ResaleNo reproduction or networking permitted without license from IHS-,-,-STANDARDIZATION DOCUMENT IMPROVEMENT PROPOSALINSTRUCTIONS1. The preparing activity must complete blocks 1, 2, 3, and 8. In block 1, both the document number and revision letter should begiven.2. The submitter of this form mus
33、t complete blocks 4, 5, 6, and 7.3. The preparing activity must provide a reply within 30 days from receipt of the form.NOTE: This form may not be used to request copies of documents, nor to request waivers, or clarification of requirements oncurrent contracts. Comments submitted on this form do not
34、 constitute or imply authorization to waive any portion of the referenced document(s) or to amend contractual requirements.I RECOMMEND A CHANGE: 1. DOCUMENT NUMBERMIL-STD-8651 2. DOCUMENT DATE (YYMMDD)9711103. DOCUMENT TITLEINSTALLATION OF IDENTIFICATION AND MODIFICATION PLATES (FOR AIRCRAFT)4. NATU
35、RE OF CHANGE (Identify paragraph number and include proposed rewrite, if possible. Attach extra sheets as needed.)5. REASON FOR RECOMMENDATION6. SUBMITTERa. NAME (Last, First, Middle Initial) b. ORGANIZATIONc. ADDRESS (Include Zip Code) d. TELEPHONE(Include Area Code)(1) Commercial:(2) DSN:(If Appli
36、cable)7. DATE SUBMITTED(YYMMDD)8. PREPARING ACTIVITYa. NAMECOMMANDERNAVAL AIR WARFARE CENTERAIRCRAFT DIVISIONb. TELEPHONE NUMBER (Include Area Code)(1) Commercial (2) DSN(908) 323-2947 624-294c. ADDRESS (Include Zip Code)CODE 414100B120-3HIGHWAY 547LAKEHURST, NJ 08733-5100IF YOU DO NOT RECEIVE A REP
37、LY WITHIN 45 DAYS, CONTACT:Defense Quality and Standardization Office, 5203 Leesburg Pike,Suite 1403, Falls Church, VA 22041-3466Telephone (703) 756-2340 DSN 289-2340DD Form 1426, OCT 89 Previous editions are obsolete 198/290Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
