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AIR FORCE - MIL-D-87213 CANC NOTICE 1

DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED

inactive, Most Current
Organization: AIR FORCE
Publication Date: 8 June 1988
Status: inactive
Page Count: 1

Document History

MIL-D-87213 CANC NOTICE 1
June 8, 1988
DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED
A description is not available for this item.
MIL-D-87213
September 18, 1984
DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED
This specification establishes the development requirements for electronically generated displays for airborne use, including Head Up Displays (HUDs) and Multi-Function Displays (MFDs), including...

References

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:
AFGS-87216A CANC NOTICE 2 - INSTRUMENT SYSTEMS, AIRBORNE
Published by AIR FORCE on February 27, 1997
A description is not available for this item.
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: PT1 SEC6 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
Published by MODUK on September 19, 2016
INTRODUCTION This Clause specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
This document is referenced by:
DEF STAN 00-970: V2 P7 - Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 3 (Parts 7 to 10) Part 7: Installations
Published by MODUK on March 10, 1998
INTRODUCTION The requirements of this Chapter are applicable to the design and construction of all turbine engine propulsion system installations including all the equipment and sub-systems necessary...
This document is referenced by:
DEF STAN 00-970:PT7:S2 S6 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Supplement 6: Equipment (Subpart F)
Published by MODUK on July 13, 2015
A description is not available for this item.
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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