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NATO - STANAG 3372

LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING

active, Most Current
Organization: NATO
Publication Date: 5 November 2014
Status: active
Page Count: 6

Document History

STANAG 3372
November 5, 2014
LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING
A description is not available for this item.
STANAG 3372
March 24, 1999
Low Pressure Air and Associated Electrical Connections for Aircraft Engine Starting
AIM The aim of this agreement is to standardize aircraft and ground equipment air and associated electrical half connectors for low-pressure air starting of aircraft engines to facilitate aircraft...
STANAG 3372
March 24, 1999
Low Pressure Air and Associated Electrical Connections for Aircraft Engine Starting
A description is not available for this item.
STANAG 3372
March 24, 1999
Low Pressure Air and Associated Electrical Connections for Aircraft Engine Starting
A description is not available for this item.
STANAG 3372
December 9, 1988
Low Pressure Air and Associated Electrical Connections for Aircraft Engine Starting
A description is not available for this item.
STANAG 3372
January 1, 1988
Low Pressure Air and Associated Electrical Connections for Aircraft Engine Starting
A description is not available for this item.
STANAG 3372
January 1, 1988
Low Pressure Air and Associated Electrical Connections for Aircraft Engine Starting
A description is not available for this item.
STANAG 3372
January 1, 1988
Low Pressure Air and Associated Electrical Connections for Aircraft Engine Starting
A description is not available for this item.
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References

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: 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.
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: PT1 SEC5 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 5: Powerplant
Published by MODUK on July 13, 2015
INTRODUCTION Requirements are provided to cover the following aspects: (a) General - covers installations and testing under ground and flight conditions. (b) Fuel System - covers fuel systems,...
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