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.

MODUK - DEF STAN 16-6

Charging Valve for Aircraft Liquid Spring Undercarriage Units

inactive, Most Current
Organization: MODUK
Publication Date: 1 January 1991
Status: inactive
Page Count: 7

Document History

DEF STAN 16-6
January 1, 1991
Charging Valve for Aircraft Liquid Spring Undercarriage Units
A description is not available for this item.

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 16-26 - Charging Valves for Aircraft High Pressure Nitrogen and Hydraulic Fluid Systems
Published by MODUK on January 1, 1983
This Standard covers the requirements relating to valves for use on aircraft for charging aircraft high pressure nitrogen and hydraulic fluid systems and components with nitrogen. It includes the...
This document is referenced by:
DEF STAN 00-970: PART 9 - Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
Published by MODUK on September 28, 2017
(a) The mandatory requirements set out in this Standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services based on the requirements...
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: PART 13 - Certification Specifications for Airworthiness Part 13: MILITARY COMMON FIT EQUIPMENT
Published by MODUK on August 28, 2020
Note 1 Where a CS makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
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...
This document is referenced by:
DEF STAN 00-970: V1 B2 P4 - Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials
Published by MODUK on October 1, 1992
GENERAL In the detailed design of the aeroplane the variety of materials and parts to be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight. The...
This document is referenced by:
DEF STAN 00-970: V2 P7 - Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 3 (Parts 7 to 10) Part 7: Installations
Published by MODUK on March 10, 1998
INTRODUCTION The requirements of this Chapter are applicable to the design and construction of all turbine engine propulsion system installations including all the equipment and sub-systems necessary...
This document is referenced by:
DEF STAN 00-970 PT7: VOL1 - Installations Chapter 711 on
Published by MODUK on March 10, 1998
This chapter states the design requirements for the installation of armament equipment in all aeroplanes. Armament Equipment, for the purpose of these requirements , comprises the weapon...
View Less
View All
Advertisement