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NATO - STANAG 3153

Aircraft Navigation and Anti-Collision Lights

inactive, Most Current
Organization: NATO
Publication Date: 24 June 1996
Status: inactive
Page Count: 24
scope:

AIM

The aim of this agreement is to establish common requirements for aircraft navigation and anti-collision lights.

Document History

STANAG 3153
June 24, 1996
Aircraft Navigation and Anti-Collision Lights
AIM The aim of this agreement is to establish common requirements for aircraft navigation and anti-collision lights.
STANAG 3153
January 1, 1996
Aircraft Navigation and Anti-Collision Lights
A description is not available for this item.
STANAG 3153
January 1, 1993
Aircraft Navigation and Anti-Collision Lights
A description is not available for this item.
STANAG 3153
January 1, 1993
Aircraft Navigation and Anti-Collision Lights
A description is not available for this item.
STANAG 3153
January 1, 1973
Aircraft Navigation and Anti-Collision Lights
A description is not available for this item.

References

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: 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 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: 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: PT 1: VOL 1 - General and Operational Requirements
Published by MODUK on November 1, 1990
A description is not available for this item.
This document is referenced by:
DEF STAN 00-970: VOL 2: PTS 0-3 - Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 1 (Parts 0 to 3)
Published by MODUK on July 31, 1984
SCOPE OF REQUIREMENTS The Defence Standard includes within its scope, requirements and recommendations which arise from the operational function of Service Rotorcraft. It covers the following main...
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 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.
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