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INDICATOR, ATTITUDE ARU-17/A, REMOTE

contributor authorAIR FORCE - 84 - Air Force Sustainment Center - Warner Robins
date accessioned2017-09-04T18:28:25Z
date available2017-09-04T18:28:25Z
date copyright02/28/1964
date issued1964
identifier otherIQSMDAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/210617
description abstractThis specification covers the requirements for one type of remote attitude indicator, designated ARU-17/A. Intended Use: The ARU-17/A remote attitude indicator covered by this specification is intended for use in helicopters. The indicator will be controlled by a vertical reference control that will provide transmitting synchro pitch and roll output signals.
languageEnglish
titleMIL-I-38263num
titleINDICATOR, ATTITUDE ARU-17/A, REMOTEen
typestandard
page34
statusActive
treeAIR FORCE - 84 - Air Force Sustainment Center - Warner Robins:;1964
contenttypefulltext


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