UNLIMITED FREE
ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Select Your Free Newsletters

Industry Newsletters

Select Your Free Product Alerts

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NATO - STANAG 3218

Location, Actuation and Shape of Engine Controls and Switches

inactive, Most Current
Organization: NATO
Publication Date: 1 January 1986
Status: inactive
Page Count: 20

Document History

STANAG 3218
January 1, 1986
Location, Actuation and Shape of Engine Controls and Switches
A description is not available for this item.

References

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 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 3593 - Numbering of Engines and Their Associated Control and Displays in Aircraft
Published by NATO on February 11, 1997
A description is not available for this item.
This document references:
STANAG 3219 - Location and Grouping of Electrical Switches in Aircraft
Published by NATO on May 5, 1992
AIM To standardize the location and grouping of various electrical switches in aircraft so that a pilot can always expect to find switches for a particular service in the same cockpit area.
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 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 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.
View Less
View All
Advertisement