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  • MIL-C-18244 Revision A:1962

    Current The latest, up-to-date edition.

    CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR

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    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Describes test and performance requirements for GFE or CFE automatic control and stabilization systems for all US Navy piloted aircraft.

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    Committee FSC 1680
    Document Type Standard
    Product Note NEW CHILD NOT 1 2019 IS NOW ADDED.
    Publisher US Military Specs/Standards/Handbooks
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
    DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/17(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    MIL-D-23143 Revision A:1982 DATA, TECHNICAL AIRCRAFT, FOR DESIGN OF AVIATION TRAINING DEVICES
    MIL-D-23222 Revision A:1971 DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    MIL I 18373 : B INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF
    MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-I-6115 Revision A:1951 INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF
    MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL A 8064 : B NOTICE 1 ACTUATOR AND ACTUATING SYSTEMS, AIRCRAFT ELECTROMECHANICAL, GENERAL REQUIREMENTS FOR
    MIL M 7793 : F METER, TIME TOTALIZING
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MS15001 Revision A:1959 FITTINGS, LUBRICATION (HYDRAULIC) SURFACE CHECK, 1/4-28 TAPER THREADS, STEEL, TYPE 1
    MIL-M-8609 Revision B:1965 MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-203 Revision G:1991 AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING 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-S-8512 Revision D:1974 SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    MIL-D-18300 Revision H:1993 DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR
    MIL-M-7969 Revision C:1965 Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for
    MIL-H-5440 Revision H:1993 HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
    MIL-H-8501 Revision A:1961 HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (AF USE MIL F 83300)
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    MIL-F-3541 Revision C:1989 FITTING, LUBRICATION, GENERAL SPECIFICATION FOR
    MIL-E-7080 Revision B:1962 ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
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