MIL-S-23535 Base Document:1963
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The latest, up-to-date edition.
SYSTEM, INTEGRATED FLIGHT INSTRUMENTATION
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Important note : Users cannot be edited or removed once added to your Multi user PDF.Details certain design and all performance requirements for the procurement of an Integrated Flight Instrumentation System.
| Committee |
FSC 6610
|
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 9/10/96
|
| DocumentType |
Standard
|
| Pages |
27
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| 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 |
| 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 |
| 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, REPRODUCTION, 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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