MIL-S-23535 Base Document:1963
Current
The latest, up-to-date edition.
System, Integrated Flight Instrumentation
01-04-1963
Details certain design and all performance requirements for the procurement of an Integrated Flight Instrumentation System.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 9/10/96
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers certain design and all performance requirements for the procurement of an Integrated Flight Instrumentation System.
| MIL-C-23367 Base Document:1963 | Computer, Flight Director, Aircraft |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL-I-23524 Revision A:1986 | Indicator, Attitude-Director, Remote, ID 1329A (V) |
| MIL-R-7060 Revision A:1956 | RADIO SET, AN/ARN-21(*) (NO S/S DOCUMENT) |
| MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
| MIL-I-23524 Revision A:1986 | Indicator, Attitude-Director, Remote, ID 1329A (V) |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL-R-18401 Revision A:1959 | RADIO SET AN/ARC-52 AND AN/ARC-52X (NO S/S DOCUMENT) |
| MIL-C-23367 Base Document:1963 | Computer, Flight Director, Aircraft |
| MIL R 23094 : LATEST | RELIABILITY ASSURANCE FOR PRODUCTION ACCEPTANCE OF AVIONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
| MIL S 3950 : F | SWITCH, TOGGLE ENVIRONMENTALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL-T-18303 Revision B:1966 | Test Procedures; Preproduction, Acceptance, and Life for Aircraft Electronic Equipment, Format for |
| MIL S 3786 : F | SWITCH, ROTARY, CLOSED CONSTRUCTION, 2 AMPERES, LOW LEVEL, POSITIVE SHAFT GROUNDING STYLE SR04 |
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