MS33585 Revision B:1961
Withdrawn
Withdrawn
POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT (NO S/S DOCUMENT)
Available format(s)
PDF
Published date
06-30-1961
Publisher
Withdrawn date
08-28-1996
US$20.00
Excluding Tax where applicable
| 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Withdrawn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 (No S/S Document) |
| MIL-I-8580 Revision B:1965 | Indicator, Tachometer, Helicopter, 0-4000 RPM, Type MA-1 (No S/S Document) |
| 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-9A (No S/S Document) |
| 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 (No S/S Document) |
| MIL-T-38473 Revision A:1972 | Timer, Precision, Bombing, 0 - 30 Minutes (No S/S Document) |
| 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 (S/S by SAE-AS18012) |
| MIL I 5356 : A | INDICATOR AIRSPEED, PITOT STATIC TYPE L 7 |
| 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-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 Multi-Function, Type G-10 |
| MIL-G-23676 Base Document:1963 | Gage, Pressure, Dial Indicating Oxygen, High Pressure (No S/S Document) |
| MIL-I-5417 Revision D:1968 | Indicator, Indicated Airspeed, 40-400 Knots (No S/S Document) |
| MIL-I-5721 Revision C:1970 | Indicator, Indicated Airspeed, 20-250 Knots (No S/S Document) |
| 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 (No S/S Document) |
| 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 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-A-25915 Revision A:1980 | Accelerometer, Aircraft, Pilot\'s Warning, Type MA-2 (No S/S Document) |
| MIL-I-22126 Revision B:1972 | Indicator, Torquemeter, Engine, Turboprop |
| MIL-I-27280 Revision A:1960 | Indicator, Indicated Airspeed AVU-10/A (No S/S Document) |
| 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, 0-4,000 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, 0-600 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) (No S/S Document) |
| MIL-I-83262-2 Base Document:1977 | Indicator, Temperature, Thermocouple, EHU-38/A (No S/S Document) |
| MIL-I-8404 Revision A:1953 | Indicator, Pressure, Single, 0 to 35 PSI Fuel Pressure Type C-33 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-I-81400 Base Document:1966 | Instruments, Aircraft, General Specification for (No S/S Document) |
| 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 1.0, Type ME-5 (No S/S Document) |
| 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/A, Horizontal Stabilizer (No S/S Document) |
| MIL-G-26988 Revision C:1971 | Gage, Liquid Quantity, Capacitor Type Transistorized, General Specification for (No S/S Document) |
| 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 (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-83117 Revision B:1975 | Indicator, Angle of Attack (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| 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, Pressure, Dial Indicating (No S/S Document) |
Summarise
US$20.00
Excluding Tax where applicable
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