MS33585 Revision B:1961

Withdrawn

POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT

Available format(s)

PDF

Withdrawn date

28-08-1996

Publisher

US Military Specs/Standards/Handbooks

DocumentType	Standard
Pages	2
PublisherName	US Military Specs/Standards/Handbooks
Status	Withdrawn

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