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NPFC - MIL-R-81367

RAIN REMOVAL SYSTEM, AIRCRAFT WINDSHIELD, JET AIR BLAST

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Organization: NPFC
Publication Date: 10 June 1974
Status: active
Page Count: 1

Document History

MIL-R-81367
June 20, 2019
Rain Removal System, Aircraft Windshield, Jet Air Blast
A description is not available for this item.
MIL-R-81367
June 10, 1974
RAIN REMOVAL SYSTEM, AIRCRAFT WINDSHIELD, JET AIR BLAST
A description is not available for this item.
MIL-R-81367
April 4, 1966
RAIN REMOVAL SYSTEM, AIRCRAFT WINDSHIELD, JET AIR BLAST
- The jet air blast rain removal system is intended for use to remove rain from the windshields of manned aircraft.

References

This document references:
MS33576 REV B - DIMENSIONS, BASIC, COCKPIT, WHEEL CONTROLLED, FIXED WING AIRCRAFT
Published by AIR FORCE on January 27, 1978
A description is not available for this item.
This document references:
MIL-B-81365 - BLEED AIR SYSTEMS, GENERAL SPECIFICATION FOR
Published by NPFC on September 10, 1997
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 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 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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