MIL-I-38263
INDICATOR, ATTITUDE ARU-17/A, REMOTE
contributor author | AIR FORCE - 84 - Air Force Sustainment Center - Warner Robins | |
date accessioned | 2017-09-04T18:28:25Z | |
date available | 2017-09-04T18:28:25Z | |
date copyright | 02/28/1964 | |
date issued | 1964 | |
identifier other | IQSMDAAAAAAAAAAA.pdf | |
identifier uri | https://yse.yabesh.ir/std/handle/yse/210617 | |
description abstract | This 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. | |
language | English | |
title | MIL-I-38263 | num |
title | INDICATOR, ATTITUDE ARU-17/A, REMOTE | en |
type | standard | |
page | 34 | |
status | Active | |
tree | AIR FORCE - 84 - Air Force Sustainment Center - Warner Robins:;1964 | |
contenttype | fulltext |