UNLIMITED FREE
ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Select Your Free Newsletters

Industry Newsletters

Select Your Free Product Alerts

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NPFC - MIL-W-6729

Watertightness of Aircraft, General Specification for

active, Most Current
Buy Now
Organization: NPFC
Publication Date: 9 September 2014
Status: active
Page Count: 1

Document History

MIL-W-6729
July 10, 2019
Watertightness of Aircraft, General Specification for
A description is not available for this item.
MIL-W-6729
September 9, 2014
Watertightness of Aircraft, General Specification for
A description is not available for this item.
MIL-W-6729
March 8, 1993
WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR
Procedures for testing aircraft described herein are intended to ensure watertightness and proper drainage when the aircraft is exposed to natural humid and rainy environments or washing procedures.
MIL-W-006729B (1)
January 15, 1984
WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-W-006729B
April 28, 1983
WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-W-6729A
September 10, 1962
WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
View Less
View All

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...
View Less
View All
Advertisement