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NATO - STANAG 3312

Profile Dimensions of Flanges for V-Band Couplings for Piping and Ducting

active, Most Current
Organization: NATO
Publication Date: 27 November 1975
Status: active
Page Count: 25
scope:

AIM

The aim of this agreement is to standardize on the profile dimensions of flanges for use with V-band couplings for aerospace piping and ducting, and the equipment connected thereto, and to establish ranges of flange diameters, so as to permit interchangeability of V-band couplings.

Document History

STANAG 3312
November 27, 1975
Profile Dimensions of Flanges for V-Band Couplings for Piping and Ducting
AIM The aim of this agreement is to standardize on the profile dimensions of flanges for use with V-band couplings for aerospace piping and ducting, and the equipment connected thereto, and to...
STANAG 3312
November 27, 1975
Profile Dimensions of Flanges for V-Band Couplings for Piping and Ducting
A description is not available for this item.
STANAG 3312
January 1, 1975
Profile Dimensions of Flanges for V-Band Couplings for Piping and Ducting
A description is not available for this item.

References

This document references:
ISO 2563 - Aircraft ducting and piping — Profile dimensions for flanges of V-band couplings
Published by ISO on September 1, 2009
This International Standard gives the profile dimensions of V-band couplings, and the associated inch-based aircraft ducting and piping for the following external flange profiles: — lightweight solid...
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.
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 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 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: VOL1 - Installations Chapter 711 on
Published by MODUK on March 10, 1998
This chapter states the design requirements for the installation of armament equipment in all aeroplanes. Armament Equipment, for the purpose of these requirements , comprises the weapon...
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