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NPFC - MIL-T-18606

TEST PROCEDURES FOR AIRCRAFT ENVIRONMENTAL SYSTEMS

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Organization: NPFC
Publication Date: 31 October 1969
Status: active
Page Count: 1

Document History

MIL-T-18606
October 10, 2018
TEST PROCEDURES FOR AIRCRAFT ENVIRONMENTAL SYSTEMS
A description is not available for this item.
MIL-T-18606
October 31, 1969
TEST PROCEDURES FOR AIRCRAFT ENVIRONMENTAL SYSTEMS
A description is not available for this item.
MIL-T-18606
March 31, 1955
TEST PROCEDURES FOR AIRCRAFT ENVIRONMENTAL SYSTEMS
-This specification covers the testing of cabin pressurizing and air conditioning systems as installed in aircraft, including defogging and defrosting, for the purpose of: (a) Demonstrating safety...

References

This document references:
MIL-T-5842 - Transparent Areas On Aircraft Surfaces (Windshields And Canopies), Rain Removing And Washing Systems For, De-Frosting, De-Icing, Defogging, General Specification For
Published by NPFC on July 31, 2019
A description is not available for this item.
This document references:
MIL-T-5842 - Transparent Areas On Aircraft Surfaces (Windshields And Canopies), Rain Removing And Washing Systems For, De-Frosting, De-Icing, Defogging, General Specification For
Published by NPFC on July 31, 2019
A description is not available for this item.
This document is referenced by:
DEF STAN 00-970: PT1 SEC4 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 4: Design and Construction
Published by MODUK on July 13, 2015
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
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 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.
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