MIL-I-23524 Revision A:1986
Current
The latest, up-to-date edition.
Indicator, Attitude-Director, Remote, ID 1329A (V)
10-03-1986
Outlines certain design and all performance requirements for the procurement of one type of the above, a component of the Integrated Flight Instrumentation System, displaying roll and pitch attitude and azimuth information with full freedom about each axis and flight director information controlled by remote circuits.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 9/10/96
|
| DocumentType |
Standard
|
| Pages |
53
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
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.
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