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MIL-I-38263
INDICATOR, ATTITUDE ARU-17/A, REMOTE
Year: 1964
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.
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| 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 |