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Page Title:
Control and Stabilization Systems: Automatic, Piloted Aircraft, General Specification |
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|  MIL-C-18244A(WEP)
1 DECEMBER 1962
SUPERSEDING
MIL-C-18244(AER)
16 MARCH 1955
MILITARY SPECIFICATION
CONTROL AND STABILIZATION SYSTEMS: AUTOMATIC,
PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
This specification has been approved by the
Bureau of Naval Weapons, Department of the Navy.
SCOPE
1.
Scope - This specification covers design. test and performance requirements for either
1.1
GFE or CFE automatic control and stabilization systems for all U.S. Navy piloted aircraft. In the event
of conflict between this specification and other referenced documents the requirements of this specifica-
tion shall govern. The detail requirements for a particular system shall be as specified in the detailed
specification, contract or purchase order for that system. (See 6.2)
APPLICABLE DOCUMENTS
2.
2.1
General - The following documents, of the issue in effect on the date of invitation for
bids, shall be used wherever applicable in the design installation and operation of the automatic
control and stabilization system.
SPECIFICATIONS
Military
Interference Measurements, Radio, Methods of, 150 Kilocycles
JAN-I-225
to 20 Megacycles (For Components and Complete Assemblies)
Terminal; Cable, Steel (For Swaging)
JAN-T-781
Fittings, Lubrication
MIL-F-3541
MIL-S-3950
Switches, Toggle
Electron Tubes and Transistors, Choice and Application of
MIL-E-4682
Wiring, Aircraft, Installation of
MIL-W-5088
Environmental Testing, Aeronautical and Associated Equipment,
MIL-E-5272
General Specification for
Electronic Equipment, Aircraft, General Specification for
MIL-E-5400
Hydraulic System; Aircraft Type I and II Installation and Data
MIL-H-5440
Requirements for
Instrument Systems, Pitot Tube and Flush Static Port Operated,
MIL-I-6115
Installation of
Interference Control Requirements, Aircraft Equipment
MIL-I-6181
Lubrication of Aircraft, General Specification for
MIL-L-6880
Electrical Equipment, Piloted Aircraft Installation and Selection
MIL-E-7080
of, General Specification for
MIL-M-7969
Motors, Alternating Current, 400-Cycle, 115/200 Volt System,
Aircraft, General Specification for
Actuators and Actuating Systems, Aircraft, Class A and B, Electrical,
MIL-A-8064
Mechanical, General Requirements for
FSC N/A
1
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