MS33558 Revision C:1968
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Current
The latest, up-to-date edition.
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Published date
26-01-1968
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Excluding VAT
| 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 (No S/S Document) |
| 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-9A (No S/S Document) |
| 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) (S/S by SAE-AS22145) |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-A-5885 Revision D:1987 | Accelerometer, Aircraft (No S/S Document) |
| MIL-I-27677 Revision E:1990 | Indicator, Liquid Quantity Oxygen (No S/S Document) |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-C-27298 Revision B:1980 | Clock, Aircraft, Mechanical ABU-9-A |
| MIL-T-38473 Revision A:1972 | Timer, Precision, Bombing, 0 - 30 Minutes (No S/S Document) |
| 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, Altitude, ARU-14/A, Remote (No S/S Document) |
| 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 (No S/S Document) |
| 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 AIR1093A | Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays |
| MIL-PRF-27197 Revision F:2017 | Indicator, Airspeed, Mach Number and Maximum Allowable Speed |
| SAE AS5604A | 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 | Ammeters, Voltmeters, and Loadmeters; Direct Current |
| MIL-PRF-38135 Revision D:2014 | Indicator, Indicated Airspeed AVU-19/A, Standby (No S/S Document) |
| 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 | Gages, 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 (No S/S Document) |
| MIL-C-5604 Revision B:1962 | Compass, Magnetic, Pilot\'s Standby (S/S by SAE-AS5604) |
| MIL P 22629 : NOTICE 3 | PRINTED WIRING BOARDS |
| MIL-I-6447 Revision C:1974 | Indicator, True Airspeed, Type M-1A (No S/S Document) |
| 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 (S/S by AFGS-87216) |
| 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 (No S/S Document) |
| 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/A241-8 |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-A-25915 Revision A:1980 | Accelerometer, Aircraft, Pilot\'s Warning, Type MA-2 (No S/S Document) |
| 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 (No S/S Document) |
| 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, 0-4,000 PSI, Integrally Lighted |
| MIL-DTL-7627 Revision G:2010 | Indicator, Turn and Slip, 28V 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-1 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-C-8412 Revision B:1969 | Compass, Magnetic, Slaved Gyro, Type J-4 (No S/S Document) |
| 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) (No S/S Document) |
| 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 (No S/S Document) |
| MIL-I-81400 Base Document:1966 | Instruments, Aircraft, General Specification for (No S/S Document) |
| 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 (No S/S Document) |
| 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 Hear, 0 Degrees C to 300 Degrees C |
| MIL-I-27672 Revision B:1987 | Indicator, Position ALU-4/A, Horizontal Stabilizer (No S/S Document) |
| MIL-A-27670 Revision D:1994 | Amplifier-Indicator Group Indicated Airspeed A/A24G-10 (No S/S Document) |
| MIL-A-83212 Revision A:1976 | Altimeter, Pressure AAU-27/A (No S/S Document) |
| MIL-A-81605 Revision D:1984 | Altimeter Set, Electronic AN/APN194(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 (No S/S Document) |
| MIL-I-27680 Revision C:1973 | Indicator, Altitude ARU-12/A, Remote (No S/S Document) |
| SAE AS22145A | 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 (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-I-5415 Revision C:1987 | Indicator: Air Speed, Pitot-Static Pressure, General Specification for (No S/S Document) |
| MIL-A-27671 Revision B:1965 | Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-11 (No S/S Document) |
| MIL-I-38258 Base Document:1965 | Indicator, Attitude ARU-18/A, Director (No S/S Document) |
| 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 (No S/S Document) |
| 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 | Indicator, 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 (No S/S Document) |
| 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, MS28088, 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 (NO S/S DOCUMENT) |
| 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 and ID-798/ARN (No S/S Document) |
| MIL-DTL-27193 Revision D:2017 | Indicator, Attitude ARU-2B/A |
| MIL-A-27391 Revision B:1963 | Altimeter, Pressure AAU-2/A (No S/S Document) |
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