|
描述 |
| 标准 |
MIL-I-23524 |
| 涵盖范围 |
This specification covers design and all performance requirements for two types of a remote attitude-director indicator, which is a component of the integrated flight instrumentation system. The indicator displays pitch and roll attitude and azimuth information with full freedom about each axis and flight director information controlled by remote circuits. |
| 描述 |
Indicator, Attitude-Director, Remote, ID 1329A (V) |
| 分类归属 |
6610 |
| 文档状态 |
停用
|
| 文档日期 |
1996-10-09 |
| 审查日期 |
2006-10-07 |
| 文档类型 |
Detail Specification |
| 文档注释 |
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| 起草机构 |
71 |
| 编制机构 |
Naval Air Systems Command |
| 协调级别 |
Limited |
| 海军管理 |
Naval Air Systems Command |
