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NATO - STANAG 4270

Aviation Fuel Design Parameter for Future NATO Land Based Turbine Powered Military Aircraft

inactive, Most Current
Organization: NATO
Publication Date: 1 January 1984
Status: inactive
Page Count: 5

Document History

STANAG 4270
January 1, 1984
Aviation Fuel Design Parameter for Future NATO Land Based Turbine Powered Military Aircraft
A description is not available for this item.

References

This document references:
STANAG 3747 - (RESTRICTED) GUIDE SPECIFICATIONS (MINIMUM QUALITY STANDARDS) FOR AVIATION TURBINE FUELS (F 24, F 27, F 34, F 35, F 37, F 40 AND F 44) - AFLP-3747 EDITION C
Published by NATO on August 16, 2017
A description is not available for this item.
This document references:
STANAG 1135 - (RESTRICTED) INTERCHANGEABILITY OF FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS USED BY THE ARMED FORCES OF THE NORTH ATLANTIC TREATY NATIONS - AFLP-1135 EDITION A
Published by NATO on November 7, 2017
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:
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.
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