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NPFC - MIL-F-25173

FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT

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Organization: NPFC
Publication Date: 10 April 2001
Status: active
Page Count: 1

Document History

MIL-F-25173A VALID NOTICE 3
July 28, 2022
Fastener, Control Panel, Aircraft Equipment
A description is not available for this item.
MIL-F-25173
April 10, 2001
FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT
A description is not available for this item.
MIL-F-25173
August 22, 1994
FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT
NOTICE OF INACTIVATION FOR NEW DESIGN This notice should be filed in front of MIL-F-25173A dated 16 February 1956 MIL-F-25173A dated 16 February 1956 is inactive for new design.
MIL-F-25173
November 23, 1959
FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT
A description is not available for this item.
MIL-F-25173
February 16, 1956
FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT
The aircraft equipment control panel fastener covered by this specification is intended for attaching equipment control panels to the aircraft structure.
MIL-F-25173
May 4, 1955
FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT
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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