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  • MS33585 Revision B:1961

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT

    Available format(s):  PDF

    Withdrawn date:  28-08-1996

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    Publisher:  US Military Specs/Standards/Handbooks

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    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn

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

    MIL-I-25859 Revision C:1995 INDICATOR, THRUST AEU-2/A, SYNCHRO STYLE, PRESSURE RATIO, 1.2-3.4 UNITS, INTEGRALLY LIGHTED
    MIL-I-8580 Revision B:1965 INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1
    MIL-I-18856 Revision B:1969 INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067
    MIL-I-7062 Revision C:1975 INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR
    MIL-I-27191 Revision C:1995 INDICATOR, POSITION, VARIABLE NOZZLE
    MIL-I-83152 Revision B:1974 INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER)
    MIL-I-38121 Revision C:1989 INDICATOR, PRESSURE, EGU-9/A
    MIL I 27197 : C INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED
    MIL I 25688 : A INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE
    MIL-A-5885 Revision D:1987 ACCELEROMETER, AIRCRAFT
    MIL-T-38473 Revision A:1972 TIMER, PRECISION, BOMBING, 0 - 30 MINUTES
    MIL I 7231 : B INDICATOR, TRUE AIRSPEED, SYNCHRO REPEATER TYPE N 1
    MIL-I-21206 Revision B:1960 INDICATOR, RATE OF FLOW, FUEL; EFU-7/A (300-5000-15000 PPH)
    MIL-I-38338 Revision D:1991 INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC
    MIL-I-27196 Revision C:1988 INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED
    MIL I 27279 : B INDICATOR, MACH NUMBER AVU-11/A, INTEGRAL LIGHTING
    MIL-I-27202 Revision A:1980 INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED
    MIL-DTL-25949 Revision F:1995 ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED
    MIL-I-25091 Revision B:1985 INDICATOR, CABIN AIR PRESSURE, PRESSURIZED AIRCRAFT, 1-7/8 INCH DIAL, TYPE MA-2
    MIL-A-27195 Revision A:1989 ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A
    MIL-M-18012 Revision B:1964 MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF
    MIL I 5356 : A INDICATOR AIRSPEED, PITOT STATIC TYPE L 7
    MIL-I-6447 Revision C:1974 INDICATOR, TRUE AIRSPEED TYPE M 1A
    MIL-I-5418 Revision B:1963 INDICATOR: AIRSPEED, PITOT STATIC, SENSITIVE, 50-650 KNOTS
    MIL-I-25325 Revision A:1961 Indicator, Rate of Flow, Fuel, Totalizing, 0-100,000 PPH, Type MA-8
    MIL-I-27304 Revision E:1977 INDICATOR, RATE OF FLOW
    MIL-I-5419 Revision B:1969 INDICATOR, INDICATED AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED 50-650 KNOTS
    MIL-I-25863 Revision D:1990 INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED
    MIL-I-6533 Revision B:1970 INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION TYPE G 10
    MIL-G-23676 Base Document:1963 GAGE, PRESSURE, DIAL INDICATING, OXYGEN, HIGH PRESSURE
    MIL-I-5417 Revision D:1968 INDICATOR, INDICATED AIRSPEED 40-400 KNOTS
    MIL-I-5721 Revision C:1970 INDICATOR, INDICATED AIRSPEED 20-250 KNOTS
    MIL I 9304 : B INDICATOR, RATE OF FLOW, FUEL, SYNCHRO STYLE 0-12,000 PPH TYPE MA 6
    MIL-I-5482 Revision C:1960 INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE
    MIL I 25689 : A NOTICE 1 INDICATOR, ELECTRICAL TACHOMETER
    MIL I 5099 : B INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1
    MIL I 25725 : A INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8
    MIL-I-18804 Revision B:1964 INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH
    MIL I 38135 : B (3) INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY
    MIL-I-21718 Base Document:1958 INDICATOR, AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED, 4O-4OO KNOTS
    MIL G 8360 : A GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1
    MIL-I-58067 Revision A:1977 INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR
    MIL-A-25915 Revision A:1980 ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2
    MIL-I-22126 Revision B:1972 INDICATOR, TORQUEMETER, ENGINE, TURBOPROP
    MIL-I-27280 Revision A:1960 INDICATOR, INDICATED AIRSPEED AVU-10/A
    MIL-I-6514 Revision B:1988 INDICATOR, OIL PRESSURE, 0-200 PSI, 320 DEGREE, TYPE B-9C
    MIL-I-25861 Revision D:1967 INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED
    MIL-G-7734 Revision C:1981 GAGE, PRESSURE ENGINE AND UTILITY AIRCRAFT
    MIL O 38338 : C (1) OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR
    MIL I 8136 : A INDICATOR, FUEL FLOW RATE, SYNCHRO STYLE, SINGLE CLAMP MOUNTED 2 INCH SIZE 300 TO 3,000 PPH TYPE A 12
    MIL-I-6301 Revision B:1994 INDICATOR, PRESSURE, FUEL O-600 PSI
    MIL-I-27247 Revision C:1985 INDICATOR, TEMPERATURE, SYNCHRO
    MIL-A-27198 Revision B:1987 ALTIMETER, PRESSURE AAU-7/A
    MIL-I-38391 Base Document:1965 INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE)
    MIL-I-83262-2 Base Document:1977 INDICATOR, TEMPERATURE, THERMOCOUPLE, EHU-38/A
    MIL-I-8404 Revision A:1953 INDICATOR, PRESSURE, SINGLE 0 TO 35 PSI FUEL PRESSURE TYPE C 33
    MIL I 7491 : B INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1
    MIL-A-81403 Base Document:1967 ALTIMETER-ENCODER, AAU-21/A
    MIL-I-81400 Base Document:1966 INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-A-25933 Revision B:1985 ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL
    MIL-I-25479 Revision A:1987 INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5
    MIL-I-7085 Revision C:1994 INDICATOR, PRESSURE, ENGINE, 0-50 PSI
    MIL-I-27552 Revision C:1995 INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-15A/A, POTENTIOMETER TYPE, WHITE LIGHTED
    MIL-I-25482 Revision D:1993 INDICATOR, ENGINE TESTING
    MIL-I-27672 Revision B:1987 INDICATOR, POSITION ALU-4/1, HORIZONTAL STABILIZER
    MIL-G-26988 Revision C:1971 GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR
    MIL-I-7721 Revision D:1992 INDICATOR, VERTICAL SPEED, 3-INCH
    MIL-I-27673 Revision C:1993 INDICATOR, TRUE AIRSPEED AVU-15/A
    MIL-I-5914 Revision E:1993 INDICATOR, RATE OF FLOW, FUEL TYPE EFU 24/A AND TYPE EFU 25/A
    MIL-I-25950 Revision B:1967 INDICATOR, PRESSURE, OIL, 0-100 PSI
    MIL-I-7087 Revision A:1968 INDICATOR, PRESSURE OIL, 0-200 PSI
    MIL-I-83117 Revision B:1975 INDICATOR, ANGLE OF ATTACK
    MIL-I-25645 Revision D:1970 INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR
    MIL-G-5678 Revision C:1964 GAGE PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE
    MIL-I-7084 Revision A:1988 INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI
    MIL-I-83262-3 Base Document:1977 INDICATOR, TEMPERATURE, THERMOCOUPLE, EHU-43/A
    MIL I 27851 : B INDICATOR, INDICATED AIRSPEED AVU-17/A
    MIL A 25949 : E (2) ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED
    MIL-I-7075 Revision A:1965 INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION -50 DEGREES TO +50 DEGREES C 2 INCH SIZE
    MIL-I-5416 Revision B:1962 INDICATOR, INDICATED AIRSPEED 10-150 KNOTS
    MIL-I-23832 Revision A:1980 INDICATOR, TACHOMETER, TRIPLE POINTER, HELICOPTER
    MIL M 5388 : B MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B
    MIL-G-8170 Revision D:1987 GAGE, OIL PRESSURE, DIRECT INDICATING, SINGLE CLAMP MOUNTED 0 -200 PSI 320 DEGREE SCALE 2 INCH SIZE, TYPE AGU 12/A AND AGU 13/A
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