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NATO - STANAG 3499

Characteristics of Supply Equipment for Liquid Oxygen

inactive, Most Current
Organization: NATO
Publication Date: 27 January 1989
Status: inactive
Page Count: 15
scope:

AIM

The aim of this agreement is to ensure minimum acceptable characteristics of charging connectors used in replenishment of aircraft liquid oxygen systems, thereby increasing the effectiveness of aircraft cross-servicing.

Document History

STANAG 3499
January 27, 1989
Characteristics of Supply Equipment for Liquid Oxygen
AIM The aim of this agreement is to ensure minimum acceptable characteristics of charging connectors used in replenishment of aircraft liquid oxygen systems, thereby increasing the effectiveness of...
STANAG 3499
January 1, 1989
Characteristics of Supply Equipment for Liquid Oxygen
A description is not available for this item.
STANAG 3499
January 1, 1989
Characteristics of Supply Equipment for Liquid Oxygen
A description is not available for this item.
STANAG 3499
January 1, 1989
Characteristics of Supply Equipment for Liquid Oxygen
A description is not available for this item.

References

This document references:
STANAG 3545 - Characteristics of Breathable Liquid Oxygen
Published by NATO on January 1, 1975
The aim of this agreement is to ensure minimal acceptable characteristics of breathing liquid oxygen provided for aircraft cross-servicing purposes.
This document references:
STANAG 3547 - Characteristics of Replenishment Equipment for Liquid Nitrogen
Published by NATO on November 28, 1983
A description is not available for this item.
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...
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:
JSSG-2010-10 VALID NOTICE 1 - Crew Systems Oxygen Systems Handbook
Published by AIR FORCE on June 16, 2023
A description is not available for this item.
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