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NPFC - MIL-B-8075

BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR

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Organization: NPFC
Publication Date: 10 March 1977
Status: active
Page Count: 1

Document History

MIL-B-8075
June 4, 2019
Brake Control Systems, Antiskid, Aircraft Wheels, Instructions for Preparation of Specifications for
A description is not available for this item.
MIL-B-8075
March 10, 1977
BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-B-8075
February 24, 1971
BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR
The antiskid brake control system covered by this specification is intended for use in conjunction with aircraft power brake systems.
MIL-B-8075
October 14, 1963
BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-B-8075
February 4, 1960
BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-B-8075
June 21, 1957
BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-B-8075
December 3, 1952
BRAKE CONTROL SYSTEMS, ANTISKID, AIRCRAFT WHEELS, GENERAL SPECIFICATION FOR
A description is not available for this item.
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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 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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