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MS33638 Revision C:1969

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Cases, Instrument, Flange Mounted, Aircraft (No S/S Document)

Available format(s)

PDF

Published date

04-15-1969

Withdrawn date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Withdrawn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