MS33558 Revision C:1968
Current
Current
The latest, up-to-date edition.
NUMERAL AND LETTER, AIRCRAFT INSTRUMENT DIAL, STANDARD FORM OF
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Publisher
| Committee |
FSC 6610
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| DevelopmentNote |
C NOTICE 1 - Notice of Validation. C NOTICE 2 - Notice of Cancellation without Replacement. C NOTICE 3 - Notice of Reinstatement. (07/2007) C NOTICE 4 - Notice of Validation. (04/2012) C NOTICE 5 - Notice of Validation. (01/2017)
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| DocumentType |
Standard
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| Pages |
6
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-G-23081 Revision C:1972 | Gyroscope Indicator System, Vertical |
| MIL-I-8580 Revision B:1965 | INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
| MIL-I-7062 Revision C:1975 | INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| 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 25688 : A | INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE |
| MIL-A-22145 Revision C:1992 | ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-A-5885 Revision D:1987 | ACCELEROMETER, AIRCRAFT |
| MIL-I-27677 Revision E:1990 | INDICATOR, LIQUID OXYGEN QUANTITY |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-C-27298 Revision B:1980 | CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
| MIL-T-38473 Revision A:1972 | TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
| MIL-I-8691 Revision A:1955 | INDICATOR, AZIMUTH, ID 307/ARN [ASG] |
| MIL I 27220 : B | INDICATOR SET, LIQUID OXYGEN QUANTITY A/A24J-8 |
| MIL-I-83449 Base Document:1974 | INDICATOR SET, LIQUID OXYGEN QUANTITY, A/A24J-21 |
| MIL-I-21206 Revision B:1960 | Indicator, Rate of Flow, Fuel; EFU-7/A (300-5000-15000 PPH) |
| MIL-I-27709 Revision A:1962 | INDICATOR, ATTITUDE ARU-14/A, REMOTE |
| MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-A-55503 Base Document:1966 | ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
| 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 |
| SAE AIR 1093 : 2002 | NUMERAL, LETTER AND SYMBOL DIMENSIONS FOR AIRCRAFT INSTRUMENT DISPLAYS |
| MIL-PRF-27197 Revision F:2017 | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| SAE AS 5604 : 2012 | COMPASS: MAGNETIC, PILOT'S STANDBY |
| MIL I 38120 : A (3) | INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A |
| MIL-A-6752 Revision A:1953 | AMMETER, VOLTMETERS, AND LOADMETERS; DIRECT CURRENT |
| MIL-PRF-38135 Revision D:2014 | INDICATOR, INDICATED AIRSPEED AVU-19A, STANDBY |
| MIL-I-25091 Revision B:1985 | INDICATOR, CABIN AIR PRESSURE, PRESSURIZED AIRCRAFT, 1-7/8 INCH DIAL, TYPE MA-2 |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
| MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
| MIL-C-5604 Revision B:1962 | COMPASS, MAGNETIC, PILOTS STANDBY |
| MIL P 22629 : NOTICE 3 | PRINTED WIRING BOARDS |
| 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-PRF-38120 Revision B:1997 | INDICATOR, RATE OF FLOW AND TRANSFER EFU-20/A |
| MIL-I-21203 Revision A:1962 | Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro |
| MIL-I-27304 Revision E:1977 | INDICATOR, RATE OF FLOW |
| MIL-I-87216 Base Document:1984 | INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
| MIL I 7077 : B | INDICATOR, TEMPERATURE ELECTRICAL RESISTANCE, MULTIFUNCTION -70 DEG TO PLUS 150 DEG. C 2 INCH SIZE |
| MIL-I-81454 Base Document:1967 | INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
| MIL-A-81852 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-I-27882 Revision A:1963 | INDICATOR, LIQUID OXYGEN, QUANTITY GMU-37/A |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MIL C 5033 : C | CLOCK, AIRCRAFT, CIVIL DATE 24 HOUR DIAL 2 3/4 IN DIAMETER |
| MIL I 6839 : C | INDICATOR, POSITION, LANDING GEAR |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| MIL-I-5482 Revision C:1960 | INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE |
| MIL-DTL-83361 Revision B:2007 | INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
| MIL-I-26382 Revision C:1994 | INDICATOR SET, LIQUID OXYGEN QUANTITY A/A24J-4 AND A/A24J-8 |
| MIL-I-21735 Revision A:1969 | Indicator, Airspeed and Mach Number, Pitot Static, 60 to 650 Knots |
| 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, 40-400 Knots |
| MIL-C-6720 Revision C:1964 | CLOCK, AIRCRAFT, ELAPSED TIME, CIVIL DATE 24 HOUR 2 3/4 INCH DIAL |
| 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-V-5622 Revision A:1963 | Volt-Ammeter, Dual Pointer Direct Current |
| MIL L 3661 : B | LAMPHOLDER, INDICATOR LIGHTS, INDICATOR LIGHT HOUSINGS AND INDICATOR LIGHT LENSES GENERAL SPECIFICATION FOR |
| MIL-I-25931 Revision B:1964 | INDICATOR, POSITION, LANDING GEAR, SYMBOL-INDICATING, INTEGRALLY LIGHTED |
| MIL-A-25915 Revision A:1980 | ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
| MIL I 25137 : A | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED, TYPE ME-4 |
| MIL-C-26485 Revision D:1968 | CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-25861 Revision D:1967 | INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
| MIL-DTL-7627 Revision G:2010 | INDICATOR, TURN AND SLIP, 28 V DC |
| MIL-G-7734 Revision C:1981 | GAGE, PRESSURE ENGINE AND UTILITY AIRCRAFT |
| MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
| MIL-C-60618 Revision C:1989 | COUNTER, ROTATING, MECHANICAL, DIRECT DRIVE: 8587543 (3200 MIL RESET) |
| MIL-C-6499 Revision E:1970 | CLOCK, AIRCRAFT MECHANICAL TYPE A 13A |
| MIL-C-8412 Revision B:1969 | COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
| MIL-DTL-6508 Revision C:2011 | THERMOMETER, SELF-INDICATING, BIMETALLIC, GENERAL SPECIFICATION FOR |
| MIL I 6424 : A NOTICE 1 | INDICATOR, INDUCTION COMPASS, TYPE V 8 |
| MIL I 26359 : B | INDICATOR, ATTITUDE, REMOTE ARU-4/A |
| 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 A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-A-22165 Base Document:1959 | Amplifier, Compass, Servo (Type MF-1 Compass) |
| MIL I 7491 : B | INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
| MIL-I-21685 Base Document:1958 | INDICATOR, COMPASS REPEATER, ROTATING DIAL, TYPE MW-2 |
| MIL-A-27261 Revision A:1966 | Accelerometer, Aircraft |
| MIL-A-81403 Base Document:1967 | ALTIMETER-ENCODER, AAU-21/A |
| MIL-I-81400 Base Document:1966 | INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL A 87211 : NOTICE 1 | AIR DATA SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD ENES, WRIGHT PATTERSON, AFB OH 45433 6503 |
| MIL-F-8378 Revision B:1975 | FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
| MIL-I-85112 Base Document:1978 | INDICATOR SET, VERTICAL SCALE |
| MIL-A-25933 Revision B:1985 | ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
| MIL C 17850 : A | COMPASS MAGNETIC, CARD, POCKET, TYPE MC-1 |
| MIL-I-38021 Revision A:1963 | INDICATOR, LIQUID OXYGEN QUANTITY GMU 39/A |
| MIL-I-27552 Revision C:1995 | INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-15A/A, POTENTIOMETER TYPE, WHITE LIGHTED |
| MIL-S-85018 Revision A:1978 | Second Order Attitude Reference System (Soars) AN/ASN-116 |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-I-7112 Revision B:1985 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, CYLINDER HEAD 0 DEGREES C TO 300 DEGREES C |
| MIL-I-27672 Revision B:1987 | INDICATOR, POSITION ALU-4/1, HORIZONTAL STABILIZER |
| MIL-A-27670 Revision D:1994 | AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| MIL-A-81605 Revision D:1984 | ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
| MIL-I-7721 Revision D:1992 | INDICATOR, VERTICAL SPEED, 3-INCH |
| MIL-I-83262 Revision B:1977 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| SAE AS 22145 : 2012 | ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
| MIL-I-27673 Revision C:1993 | INDICATOR, TRUE AIRSPEED AVU-15/A |
| MIL T 25502 : C | TRUE HEADING COMPUTER GROUP AN/AJA-I |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| 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-7071 Revision B:1972 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-I-25941 Revision D:1986 | INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
| 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-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL-C-87975 Base Document:1985 | CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
| MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
| MIL-A-27671 Revision B:1965 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
| MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
| MIL-DTL-7077 Revision D:2011 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION, -70 DEGREES C TO 150 DEGREES C, 2-INCH SIZE |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL-C-38207 Revision A:1965 | CLOCK, AIRCRAFT, MECHANICAL ABU 11/A |
| MIL-DTL-6839 Revision E:2011 | INDICATOR, POSITION, LANDING GEAR |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL-C-38418 Revision E:1981 | Control Assembly, Gyroscope, Attitude A/A24G-39 |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| MIL-I-25437 Revision B:1984 | INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-7075 Revision A:1965 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION -50 DEGREES TO +50 DEGREES C 2 INCH SIZE |
| MIL-A-58066 Revision A:1966 | ALTIMETER, PRESSURE, PARACHUTIST'S |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-I-7802 Revision A:1967 | INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
| MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL C 38333 : 0 | CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
| MIL-I-7906 Revision A:1961 | INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB 1 |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-STD-1293 Base Document:1979 | ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| MIL-I-26380 Revision B:1964 | INDICATOR, LIQUID OXYGEN QUANTITY GMU-5/A |
| MIL-I-25992 Revision A:1959 | INDICATOR, BEARING DISTANCE HEADING ID 526A ARN |
| MIL-DTL-27193 Revision D:2017 | INDICATOR, ATTITUDE ARU-2B/A |
| MIL-A-27391 Revision B:1963 | ALTIMETER, PRESSURE AAU-2A |
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