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ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR

contributor authorAIR FORCE - 84 - Air Force Sustainment Center - Warner Robins
date accessioned2017-09-04T16:26:32Z
date available2017-09-04T16:26:32Z
date copyright05/24/2013
date issued2013
identifier otherUARNDFAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/89767
description abstractThis specification establishes the general requirements for hydraulic linear actuators used in any aircraft hydraulic system except for those associated with flight controls.Intended Use: The actuators covered by this specification are intended for use in aeronautical hydraulic systems covered by SAE AS5440 to actuate such individual units as landing gears and bomb bay doors. The complete actuator assembly may incorporate other components, such as check valves, solenoid valves, bypass valves, and pressure switches, in addition to the actuator. The actuator may be controlled by mechanical linkage, electrical means, or direct hydraulic power.
languageEnglish
titleMIL-PRF-5503Gnum
titleACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FORen
typestandard
page16
statusActive
treeAIR FORCE - 84 - Air Force Sustainment Center - Warner Robins:;2013
contenttypefulltext


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