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NATO - STANAG 7140

Aircraft Flight Intruments - Layout and Display

active, Most Current
Organization: NATO
Publication Date: 15 July 1999
Status: active
Page Count: 94
scope:

AIM

The aim of this agreement is to standardize the layout of flight data in pilot displays and the features of aircraft altimeters, tachometers and indicators.

Document History

STANAG 7140
July 15, 1999
Aircraft Flight Intruments - Layout and Display
AIM The aim of this agreement is to standardize the layout of flight data in pilot displays and the features of aircraft altimeters, tachometers and indicators.

References

This document references:
STANAG 3329 - Numerals and Letters in Aircrew Stations
Published by NATO on November 29, 1984
AIM The aim of this agreement is to provide standard forms and dimensions of numerals and letters for use in aircrew stations upon instruments, control panels and displays, and as a goal for...
This document references:
STANAG 3516 - ELECTROMAGNETIC INTERFERENCE, TEST METHODS FOR AIRCRAFT ELECTRICAL AND ELECTRONIC EQUIPMENT
Published by NATO on September 14, 2010
AIM The primary aim of this agreement is to foster international co-operation and commonality between participating nations concerning the control of electromagnetic interference (both emission and...
This document references:
STANAG 3701 - AIRCRAFT INTERIOR COLOUR SCHEMES
Published by NATO on March 26, 2010
AIM The aim of this agreement is to standardise the interior colour schemes in aircrew station areas.
This document references:
STANAG 3224 - AIRCRAFT INTERIOR AND EXTERIOR LlGHTlNG NIGHT VISION l GOGGLE (NVG) AND NON-NVG COMPATIBLE
Published by NATO on March 23, 2005
AIM The aim of this agreement is to establish criteria for aircraft interior and exterior lighting. Exterior lighting means aircraft navigation, position, formation, and anti-collision lights....
This document references:
STANAG 3643 - Coating, Reflection Reducing for Glass Elements Used in Aircrew Station Displays
Published by NATO on February 26, 1973
AIM The aim of this agreement is to standardize the coatings used on glass elements in displays to reduce the reflections under all ambient illuminated conditions in Aircrew Stations.
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...
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