MS33639 Revision D:1988
Current
Current
The latest, up-to-date edition.
Cases, Instrument, Clamp - Mounted, Aircraft
Available format(s)
PDF
Published date
01-03-1988
Publisher
£14.68
Excluding VAT
| DevelopmentNote |
D Notice 2 - Notice of Validation but remains Inactive for New Design (06/2004)
|
| DocumentType |
Standard
|
| Pages |
4
|
| ProductNote |
NEW CHILD NOT 3 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| MIL-I-27674 Revision C:1994 | Indicator, Temperature, Electrical Resistance (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 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 (No S/S Document) |
| 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 (S/S by NASM6818) |
| 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 | Gages, 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 (S/S by AFGS-87216) |
| 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 (No S/S Document) |
| 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 | Lights, Instrument, Individual, General Specification for (S/S by SAE-AS50571) |
| 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/A27J-1 (S/S BY MIL-I-27190 AND MS28005) |
| 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) (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-F-8378 Revision B:1975 | Frequency Meters, Aircraft 380 to 420 Hertz and 350 to 450 Hertz (No S/S Document) |
| MIL-T-27-233 Base Document:1978 | TRANSFORMERS AND INDUCTORS (AUDIO, POWER AND HIGH-POWER PULSE), INDUCTOR, CHARGING, TF5S37ZZ (NO S/S DOCUMENT) |
| MIL-I-25130 Revision B:1974 | Indicator, Pressure, Oil, 0-300 PSI, Type MO-1 (No S/S Document) |
| 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-83245 Revision A:1994 | Indicator Set, Oil Pressure A/A24J-17 (No S/S Document) |
| 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 (No S/S Document) |
| 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 (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-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 |
| 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 | Indicator, Rate of Flow, 0-5,000 PPH, Integrally Lighted (No S/S Document) |
| 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, Pressure, Dial Indicating (No S/S Document) |
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