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Fluid power systems

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Standard

FLUIDIC TECHNOLOGY
1995-06-01
HISTORICAL
ARP993
The scope of this document is limited to encompass terminology, symbols, performance criteria and certain elementary test methods reflecting the current status of the technology.
Standard

Fluidic Technology
2007-01-11
HISTORICAL
ARP993C
The scope of this document is limited to encompass terminology, symbols, performance criteria and methods reflecting the current status of the technology.
Standard

Fluidic Technology
2012-05-31
CURRENT
ARP993D
The scope of this document is limited to encompass terminology, symbols, performance criteria and methods reflecting the current status of the technology.
Standard

FLUIDIC TECHNOLOGY
2011-08-10
HISTORICAL
ARP993A
The scope of this document is limited to encompass terminology, symbols, performance criteria and certain elementary test methods reflecting the current status of the technology.
Standard

FLUIDIC TECHNOLOGY
1995-06-01
HISTORICAL
ARP993B
The scope of this document is limited to encompass terminology, symbols, performance criteria and methods reflecting the current status of the technology.
Standard

Insulating Components, Molded, Electrical, Heat Shrinkable, Connector and Cable Accessory, Sealing Strain Relief, General Specification For
2004-07-22
HISTORICAL
AS5258
This specification covers connector and cable accessory heat shrinkable, electrical insulating, molded components fabricated from various polymer based compositions. These components are intended for use as connector and cable accessory components to provide strain relief, electrical insulation, and environmental sealing.
Standard

Tube Fittings, Aerospace Fluid Systems, Separable, for 24 Degree Cone, General Specification, Metric (ISO 7169)
2021-06-10
CURRENT
MA2005C
This document specifies performance and quality requirements for the qualification and manufacture of 24 degree cone fittings to ensure reliable performance in aircraft hydraulic systems. This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines. This document covers fittings of temperature types and pressure classes specified in MA2001.
Standard

8000 psi Hydraulic Systems: Experience and Test Results
2004-03-18
HISTORICAL
AIR4002
Shortly after World War II, as aircraft became more sophisticated and power-assist, flight-control functions became a requirement, hydraulic system operating pressures rose from the 1000 psi level to the 3000 psi level found on most aircraft today. Since then, 4000 psi systems have been developed for the U.S. Air Force XB-70 and B-1 bombers and a number of European aircraft including the tornado multirole combat aircraft and the Concorde supersonic transport. The V-22 Osprey incorporates a 5000 psi hydraulic system. The power levels of military aircraft hydraulic systems have continued to rise. This is primarily due to higher aerodynamic loading, combined with the increased hydraulic functions and operations of each new aircraft. At the same time, aircraft structures and wings have been getting smaller and thinner as mission requirements expand. Thus, internal physical space available for plumbing and components continues to decrease.
Standard

8000 psi Hydraulic Systems: Experience and Test Results
2012-11-15
CURRENT
AIR4002A
Shortly after World War II, as aircraft became more sophisticated and power-assist, flight-control functions became a requirement, hydraulic system operating pressures rose from the 1000 psi level to the 3000 psi level found on most aircraft today. Since then, 4000 psi systems have been developed for the U.S. Air Force XB-70 and B-1 bombers and a number of European aircraft including the tornado multirole combat aircraft and the Concorde supersonic transport. The V-22 Osprey incorporates a 5000 psi hydraulic system. The power levels of military aircraft hydraulic systems have continued to rise. This is primarily due to higher aerodynamic loading, combined with the increased hydraulic functions and operations of each new aircraft. At the same time, aircraft structures and wings have been getting smaller and thinner as mission requirements expand. Thus, internal physical space available for plumbing and components continues to decrease.
Standard

Rotorcraft: Application of Existing Aircraft Designed Tires, Wheels and Brakes
2021-04-23
CURRENT
ARP5632
This document covers recommendations for the application of existing qualified and approved in-service fixed wing aircraft tires, wheels and brakes to military and commercial rotorcraft. NOTE: This document does not address the use of radial tires due to insufficient data to support their approved use on rotorcraft, see paragraph 4.3.14 for specific impact on ground resonance.
Standard

Impulse Testing of Hydraulic Tubing and Fittings, S-N Curve
2013-01-07
CURRENT
AS4265
This aerospace test standard establishes the requirements and procedures for evaluating and comparing the impulse fatigue performance of high pressure hydraulic fittings and tubing. This test method may be used to test similar fluid system components, if desired.
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