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NATO - STANAG 3456

Aircraft Electrical Power System Characteristics

inactive
Organization: NATO
Publication Date: 24 March 2014
Status: inactive
Page Count: 7

Document History

STANAG 3456
October 24, 2022
AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS
AIM The aim of this NATO standardization agreement (STANAG) is to respond to the following interoperability requirements.
STANAG 3456
March 24, 2014
Aircraft Electrical Power System Characteristics
A description is not available for this item.
STANAG 3456
October 20, 1997
Aircraft Electrical Power System Characteristics
AIM The aim of this agreement is to establish the essential electrical characteristics of systems for the generation, distribution and utilization of electrical power in aircraft.
STANAG 3456
January 1, 1994
Aircraft Electrical Power System Characteristics
A description is not available for this item.
STANAG 3456
January 1, 1976
Aircraft Electrical System Characteristics
A description is not available for this item.
STANAG 3456
January 1, 1976
Aircraft Electrical System Characteristics
A description is not available for this item.
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References

This document is referenced by:
DEF STAN 00-133: PART 0 - Aviation Arrangements in Surface Ships Part 0: Procedures for Use, Definitions and Content
Published by MODUK on April 14, 2021
A description is not available for this item.
This document is referenced by:
DEF STAN 00-133: PART 04 - Aviation Arrangements in Surface Ships Part 04: Acceptance of Aviation Arrangements
Published by MODUK on April 14, 2021
The scope of Part 4 of Defence Standard 00-133 is to set out how acceptance of aviation arrangements shall be conducted and includes inspection, testing and trials activity. Regulation for the...
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 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.
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...
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