MS33638 Revision C:1969
Withdrawn
Withdrawn
Cases, Instrument, Flange Mounted, Aircraft (No S/S Document)
Available format(s)
PDF
Published date
04-15-1969
Publisher
Withdrawn date
04-07-2015
US$20.00
Excluding Tax where applicable
| DevelopmentNote |
C NOTICE 1 - Notice of Inactivation for New Design. C NOTICE 2 - Notice of Validation but remains Inactive for New Design. (11/2008) C NOTICE 3 - Notice of Cancellation without Replacement. (05/2015)
|
| DocumentType |
Standard
|
| Pages |
4
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL I 7231 : B | INDICATOR, TRUE AIRSPEED, SYNCHRO REPEATER TYPE N 1 |
| MIL M 7584 : A | METER, FUEL FLOW SYNCHRO STYLE TYPE B 3A |
| MIL-DTL-5099 Revision C:2011 | Indicator, Cabin Air Pressure, 1-7/8 Inch Dial, Type MA-1 |
| 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-I-9443 Revision D:1972 | Indicator, Temperature, Thermocouple, Engine Exhaust, Type MJ-2 |
| MIL-A-27195 Revision A:1989 | Accelerometer, Aircraft, Mechanical ABU-6/A |
| MIL I 5356 : A | INDICATOR AIRSPEED, PITOT STATIC TYPE L 7 |
| MIL-I-5170 Revision C:1987 | Indicator, Position, Horizontal Stabilizer (No S/S Document) |
| SAE AS50571B | Lights, Instrument, Individual, General Specification For |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MIL I 5099 : B | INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| MIL-A-25915 Revision A:1980 | Accelerometer, Aircraft, Pilot\'s Warning, Type MA-2 (No S/S Document) |
| MIL-L-5057 Revision F:1981 | Lights, Instrument, Individual, General Specification for (S/S by SAE-AS50571) |
| MIL-I-27280 Revision A:1960 | Indicator, Indicated Airspeed AVU-10/A (No S/S Document) |
| MIL-DTL-7627 Revision G:2010 | Indicator, Turn and Slip, 28V DC |
| MIL-C-9075 Revision A:1968 | Computer and Transmitter, True Airspeed, Pitot-Static, 150-900 Knots, Type MA-1 (No S/S Document) |
| MIL-F-8378 Revision B:1975 | Frequency Meters, Aircraft 380 to 420 Hertz and 350 to 450 Hertz (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-7112 Revision B:1985 | Indicator, Temperature, Electrical Resistance, Cylinder Hear, 0 Degrees C to 300 Degrees C |
| MIL-I-27673 Revision C:1993 | Indicator, True Airspeed AVU-15/A |
| MIL-DTL-6019 Revision E:2011 | Gages, Pressure, Dial Indicating, Low-Pressure Oxygen |
| MIL-A-38140 Revision B:1977 | Altimeter, Pressure AAU-16/A (No S/S Document) |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL-I-25437 Revision B:1984 | Indicator, Aircraft, Pressure, Voltage Ratio Type, General Specification for |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
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US$20.00
Excluding Tax where applicable
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