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NPFC - MIL-T-5522

TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS

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Organization: NPFC
Publication Date: 26 September 2000
Status: inactive
Page Count: 1

Document History

MIL-T-5522
September 26, 2000
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
MIL-T-5522
August 25, 1987
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
MIL-T-5522
September 28, 1979
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
MIL-T-5522D
September 30, 1975
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
- This specification is for use in determining methods for testing aircraft hydraulic and emergency pneumatic systems. - The hydraulic or emergency pneumatic system tests required by this...
MIL-T-5522C
March 20, 1966
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
MIL-T-5522B (1)
June 22, 1955
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
MIL-T-5522B
January 27, 1953
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
MIL-T-5522A CONT. DIST.
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
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References

This document references:
SD 24 - Value Engineering: A Guidebook of Best Practices and Tools
Published by NPFC on June 13, 2011
A description is not available for this item.
This document references:
MIL-B-8584 - BRAKE SYSTEMS, WHEEL, AIRCRAFT DESIGN OF
Published by NPFC on August 12, 1970
This specification covers the brake system design requirements for aircraft equipped with wheel-type landing gear. The brake systems shall be either hydraulic or pneumatic; manually operated, power...
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: V1 B3 - Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 3 (Chapters 711 on and Parts 8 to 10)
Published by MODUK on December 12, 1983
A description is not available for this item.
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:
MIL-D-23222 - DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
Published by NPFC on June 30, 1983
A description is not available for this item.
This document is referenced by:
MIL-P-23004 - POD (FOR GUN POD MARK 4 MOD 0)
Published by NPFC on April 12, 1983
A description is not available for this item.
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