MIL F 26685 : B NOTICE 1

Name: MIL F 26685 : B NOTICE 1
Brand: MIL

Withdrawn

FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF

Withdrawn date

23-07-2013

Published date

12-01-2013

Publisher

US Military Specs/Standards/Handbooks

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Status	Withdrawn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, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
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
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

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