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NPFC - MIL-STD-8651

Installation of Identification and Modification Plates (For Aircraft)

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Organization: NPFC
Publication Date: 10 February 2015
Status: active
Page Count: 1

Document History

MIL-STD-8651
November 19, 2019
INSTALLATION OF IDENTIFICATION AND MODIFICATION PLATES (FOR AIRCRAFT)
A description is not available for this item.
MIL-STD-8651
February 10, 2015
Installation of Identification and Modification Plates (For Aircraft)
A description is not available for this item.
MIL-STD-8651
November 10, 1997
INSTALLATION OF IDENTIFICATION AND MODIFICATION PLATES (FOR AIRCRAFT)
Identification and modification plates for major structural assemblies are intended for identification of the assembly and for the determination of changes incorporated in the assembly.

References

This document is referenced by:
DEF STAN 00-970: PART 9 - Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
Published by MODUK on September 28, 2017
(a) The mandatory requirements set out in this Standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services based on the requirements...
This document is referenced by:
DEF STAN 00-970: PART 13 - Certification Specifications for Airworthiness Part 13: MILITARY COMMON FIT EQUIPMENT
Published by MODUK on August 28, 2020
Note 1 Where a CS makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
This document is referenced by:
DEF STAN 00-970: PART 11 - Certification Specifications for Airworthiness Part 11: ENGINES
Published by MODUK on August 28, 2020
Unless otherwise specified in this Standard, the certification requirements of EASA CS-E (amendment 6) including related AMC and Appendices shall be applied. Additionally, the requirements of CS-E...
This document is referenced by:
DEF STAN 00-970: PT7 SEC1 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Section 1: Introduction
Published by MODUK on July 13, 2015
This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Rotorcraft Aircraft for UK Military operation.
This document is referenced by:
DEF STAN 00-970: PART 5 - Certification Specifications for Airworthiness Part 5: LARGE TYPE AIR SYSTEMS
Published by MODUK on March 14, 2021
Where CS 25 makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
This document is referenced by:
DEF STAN 00-970: PART 0 - Certification Specifications for Airworthiness Part 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Published by MODUK on March 14, 2021
Part 0 provides guidance and content information, together with definitions of terms used throughout this Standard.
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