MIL F 26685 : B NOTICE 1
Withdrawn
Withdrawn
FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF
Published date
01-12-2013
Publisher
Withdrawn date
07-23-2013
Sorry this product is not available in your region.
Details design installation and requirements for a flight director system.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MS 17322 : LATEST | |
| MIL-I-27619 Revision G:1974 | Indicators, Attitude Director |
| MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL I 5949 : G | INSTRUMENTS, FLIGHT AND ENGINE, AIRCRAFT, FUNCTIONAL TESTS AND TOLERANCES OF |
| MIL-C-38418 Revision E:1981 | Control Assembly, Gyroscope, Attitude A/A24G-39 |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL S 3950 : F | SWITCH, TOGGLE ENVIRONMENTALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-D-38134 Revision A:1971 | Detector, Magnetic Azimuth DSU-4/A, High Temperature (No S/S Document) |
| MS33545 Base Document:1954 | Case Instrument, 5 X 5-1/4, Standard Dimensions for |
| MIL S 3786 : F | SWITCH, ROTARY, CLOSED CONSTRUCTION, 2 AMPERES, LOW LEVEL, POSITIVE SHAFT GROUNDING STYLE SR04 |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL W 16878 : F | WIRE, ELECTRICAL, INSULATED, GENERAL SPECIFICATION FOR |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
Summarise
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