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Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
CASE, INSTRUMENT, FLANGE MOUNTED, AIRCRAFT
Available format(s)
PDF
Withdrawn date
07-04-2015
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| Committee |
FSC 66GP
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| 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)
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| 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Withdrawn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 |
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| MIL-PRF-38135 Revision D:2014 | INDICATOR, INDICATED AIRSPEED AVU-19A, STANDBY |
| 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 |
| 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, PILOTS WARNING, TYPE MA-2 |
| MIL-L-5057 Revision F:1981 | LIGHT, INSTRUMENT, INDIVIDUAL, GENERAL SPECIFICATION FOR |
| MIL-I-27280 Revision A:1960 | INDICATOR, INDICATED AIRSPEED AVU-10/A |
| MIL-DTL-7627 Revision G:2010 | INDICATOR, TURN AND SLIP, 28 V DC |
| MIL-C-9075 Revision A:1968 | COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
| MIL-F-8378 Revision B:1975 | FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
| 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 HEAD 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 |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL-I-25437 Revision B:1984 | INDICATORS, 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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