MIL-STD-1293 Base Document:1979
Withdrawn
ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT (NO S/S DOCUMENT)
09-26-1979
12-05-1995
Defines design requirements for Electro-Mechanical Command Instrument Systems (Flight Directors) for Rotary Wing aircraft.
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This standard describes the primary control/display requirements for helicopter Command Instrument System (CIS) although it does not preclude unique or noval presentations over and above the basic instrument requirements.
| MIL-M-18012 Revision B:1964 | Markings for Aircrew Station displays Design and Configuration of (S/S by SAE-AS18012) |
| MIL-C-25050 Revision A:1963 | Colors, Aeronautical Lights and Lighting Equipment, General Specification for (S/S by SAE-AS25050) |
| MIL-C-14806 Revision A:1969 | Coating, Reflection Reducing, for Instrument Cover Glasses and Lighting Wedges |
| MS33558 Revision C:1968 | Numeral and Letters, Aircraft Instrument Dial, Standard Form of |
| MIL-L-27160 Revision C:1972 | Lighting, Instrument, Integral, White, General Specification for |
| MIL-L-25467 Revision D:1977 | Lighting, Integral, Red, Aircraft Instrument, General Specification for |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-STD-1553 Revision B:1978 | Digital Time Division Command/Response Multiplex Data Bus |
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