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NATO - STANAG 3220

Location, Actuation and Shape of Airframe Controls for Fixed Wing Aircraft

inactive, Most Current
Organization: NATO
Publication Date: 1 January 1974
Status: inactive
Page Count: 11

Document History

STANAG 3220
January 1, 1974
Location, Actuation and Shape of Airframe Controls for Fixed Wing Aircraft
A description is not available for this item.

References

This document references:
STANAG 3221 - Automatic Flight Control System (AFCS) in Aircraft - Design Standards and Location of Controls
Published by NATO on January 1, 1977
AIM The aim of this agreement is to standardize the AFCS controls and panel location, the nomenclature, and other functional areas of AFCS.
This document references:
STANAG 3217 - Operation of Controls and Switches at Aircrew Stations
Published by NATO on November 21, 2006
AIM The aim of this agreement is the standardization of the direction of actuation of controls and switches at aircrew stations and the location and grouping of various electrical switches in...
This document references:
STANAG 3341 - Emergency Control Colour Schemes
Published by NATO on January 1, 1972
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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