MS33639 Revision D:1988
Current
Current
The latest, up-to-date edition.
CASE, INSTRUMENT, CLAMP MOUNTED AIRCRAFT (ASG)
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Publisher
| Committee |
FSC 66GP
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| DevelopmentNote |
D Notice 2 - Notice of Validation but remains Inactive for New Design (06/2004)
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| DocumentType |
Standard
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| Pages |
3
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| ProductNote |
NEW CHILD NOT 3 2019 IS NOW ADDED
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-I-27674 Revision C:1994 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE MULTIFUNCTION, MINUS 5O DEG TO PLUS 2OO DEG C |
| MIL-I-8580 Revision B:1965 | INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
| MIL I 25688 : A | INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE |
| MIL-I-83262-1 Revision A:1987 | INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-31A/A |
| 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-27202 Revision A:1980 | INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
| ARINC 408A : 1976 | AIR TRANSPORT INDICATOR CASES AND MOUNTING |
| MIL-DTL-25026 Revision C:2011 | INDICATOR, TEMPERATURE, THERMOCOUPLE, ENGINE EXHAUST, TYPE MJ-4 |
| MIL-C-6818 Revision D:1973 | CLAMP, INSTRUMENT MOUNTING AIRCRAFT |
| MIL I 38120 : A (3) | INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A |
| MIL-I-9443 Revision D:1972 | Indicator, Temperature, Thermocouple, Engine Exhaust, Type MJ-2 |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL I 7077 : B | INDICATOR, TEMPERATURE ELECTRICAL RESISTANCE, MULTIFUNCTION -70 DEG TO PLUS 150 DEG. C 2 INCH SIZE |
| MIL-DTL-5184 Revision C:2016 | Indicator, Position |
| MIL I 25689 : A NOTICE 1 | INDICATOR, ELECTRICAL TACHOMETER |
| SAE AS50571B | Lights, Instrument, Individual, General Specification For |
| MIL-I-25852 Revision B:1981 | Indicator, Temperature, Thermocouple EHU-4/A |
| MIL-I-9343 Revision C:1985 | Indicator, Temperature, Thermocouple, Engine Exhaust, Type MJ-1 |
| MIL-PRF-38120 Revision B:1997 | Indicator, Rate of Flow and Transfer EFU-20/A |
| 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-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-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 I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MIL-DTL-25308 Revision C:2010 | GAGE, PRESSURE, DIAL INDICATING, HYDRAULIC, TYPE ME-1 |
| 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-DTL-83361 Revision B:2007 | INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
| MIL I 25725 : A | INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
| MIL-C-6390 Revision B:1959 | CLAMPS AND INSTRUMENTS, AIRCRAFT, INSTALLATION OF |
| MIL-L-5057 Revision F:1981 | LIGHT, INSTRUMENT, INDIVIDUAL, GENERAL SPECIFICATION FOR |
| MIL-I-25861 Revision D:1967 | Indicator, Pressure, Hydraulic, 0-4,000 PSI, Integrally Lighted |
| MIL-P-38027 Revision A:1973 | PRESSURE INDICATING SYSTEM, HYDRAULIC A/A27 J-1 |
| 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-27665 Revision B:1984 | Indicator, Temperature, Electrical Resistance, Minus 50 Degrees to Plus 50 Degrees C |
| MIL-I-27203 Revision B:1987 | Indicator, Position, Wing Flap |
| MIL I 6856 : C | INDICATOR, PRESSURE SYNCHRO 1 1/2 INCH |
| MIL-I-27247 Revision C:1985 | Indicator, Temperature, Synchro |
| MIL-DTL-27189 Revision E:2008 | Indicator, Pressure, Oil |
| 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-F-8378 Revision B:1975 | FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
| MIL-T-27-233 Base Document:1978 | TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
| MIL-I-25130 Revision B:1974 | INDICATOR, PRESSURE, OIL, 0-300PSI, TYPE MO-1 |
| 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-83245 Revision A:1994 | INDICATOR SET, OIL PRESSURE A/A24J-17 |
| MIL I 27189 : D | INDICATOR, PRESSURE OIL |
| 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-25645 Revision D:1970 | Indicator, Liquid Oxygen Quantity, Capacitance Type, General Specification for |
| MIL-I-83262-3 Base Document:1977 | INDICATOR, TEMPERATURE, THERMOCOUPLE, EHU-43/A |
| MIL-DTL-7077 Revision D:2011 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION, -70 DEGREES C TO 150 DEGREES C, 2-INCH SIZE |
| 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-I-27667 Revision C:1990 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, EHU-16/A MULTIFUNCTION -70 DEGREES TO +150 DEGREES C |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL-V-85603 Base Document:1989 | Voltmeter, DC, Aircraft, Digital Display General Specification for |
| MIL-DTL-27190 Revision C:2006 | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-DTL-6856 Revision D:2006 | INDICATOR, PRESSURE, SYNCHRO, 1-1/2 INCH |
| 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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