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NATO - STANAG 3659

Electrical Bonding Requirements for Metallic Aircraft Systems

active, Most Current
Organization: NATO
Publication Date: 20 November 1998
Status: active
Page Count: 24
scope:

AIM

The aim of this agreement is to specify electrical bonding performance requirements and verification provisions for metallic aircraft systems and associated support equipment.

Document History

STANAG 3659
November 20, 1998
Electrical Bonding Requirements for Metallic Aircraft Systems
AIM The aim of this agreement is to specify electrical bonding performance requirements and verification provisions for metallic aircraft systems and associated support equipment.
STANAG 3659
November 20, 1998
Electrical Bonding Requirements for Metallic Aircraft Systems
A description is not available for this item.
STANAG 3659
November 20, 1998
Electrical Bonding Requirements for Metallic Aircraft Systems
A description is not available for this item.
STANAG 3659
February 3, 1995
Electrical Bonding Requirements for Metallic Aircraft Systems
A description is not available for this item.
STANAG 3659
January 1, 1995
Electrical Bonding Requirements for Metallic Aircraft Systems
A description is not available for this item.
STANAG 3659
January 1, 1975
Bonding and in-Flight Lightning Protection for Aircraft
A description is not available for this item.
STANAG 3659
January 1, 1975
Bonding and in-Flight Lightning Protection for Aircraft
A description is not available for this item.
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References

This document references:
STANAG 3632 - AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING
Published by NATO on October 24, 2022
AIM The aim of this NATO standardization agreement (STANAG) is to respond to the following interoperability requirements.
This document references:
STANAG 3456 - AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS
Published by NATO on October 24, 2022
AIM The aim of this NATO standardization agreement (STANAG) is to respond to the following interoperability requirements.
This document references:
STANAG 3632 - AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING
Published by NATO on October 24, 2022
AIM The aim of this NATO standardization agreement (STANAG) is to respond to the following interoperability requirements.
This document references:
AEP-29 - Protection of Aircraft Crew and Sub-Systems in Flight Against Electrostatic Charges
Published by NATO on February 1, 1999
PURPOSE The purpose of this document is to provide design guidance and concepts to protect aircraft crew and sub-systems in flight against the effects of electrostatic charge accumulation by: (a)...
This document is referenced by:
STANAG 7009 - (RESTRICTED) AIRCRAFT ELECTRICAL HAZARDS ON THE FLIGHT LINE - AEP-24 EDITION B
Published by NATO on October 3, 2022
A description is not available for this item.
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: 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.
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