MIL I 5949 : G
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
INSTRUMENTS, FLIGHT AND ENGINE, AIRCRAFT, FUNCTIONAL TESTS AND TOLERANCES OF
Withdrawn date
23-07-2013
Publisher
Outlines tolerances and functional tests of Government-furnished engine and flight aircraft instruments.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL F 26685 : B NOTICE 1 | FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF |
| MS28005 Revision J:1990 | TRANSMITTER, PRESSURE, SYNCHRO, AIRCRAFT |
| MS24378 Revision G:2015 | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| MIL-T-27200 Revision C:1975 | TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
| MIL-I-27196 Revision C:1988 | INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED |
| MS28004 Revision B:1966 | INDICATOR TEMPERATURE, ELECTRICAL RESISTANCE, CYLINDER HEAD, 0-300 DEGREES C |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| MS28034 Revision B:2007 | BULBS, TEMPERATURE, ELECTRICAL RESISTANCE (-70 DEGREES C TO +300 DEGREES C) |
| MS28010 Revision D:1992 | INDICATOR, PRESSURE SYNCHRO, SINGLE, 2 INCH SIZE |
| MIL T 27/330 : B | TRANSFORMER, POWER 100 VA TO 140 VA 60 HZ TF4S03JA |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
| MS28063 Revision A:1959 | GAGE, PRESSURE, ENGINE AND UTILITY, 2 INCH, FLANGE OR PORT MOUNTED, BOTTOM PORT |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU 60A |
| MS24478 Revision C:2006 | GAGE, SINGLE 1 INCH DIAL, PNEUMATIC PRESSURE |
| MS24569 Revision D:1966 | INDICATOR TEMPERATURE, THERMOCOUPLE, SELF BALANCING POTENTIOMETER TYPE (ASG) |
| MIL-G-25597 Revision D:1973 | GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
| MIL-STD-1524 Base Document:1972 | TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL |
| MIL-C-26485 Revision D:1968 | CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
| MIL-G-25591 Revision E:1981 | GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
| MS3106 Revision D:1992 | CONNECTOR, PLUG, ELECTRIC, STRAIGHT, SOLDER CONTACTS, AN TYPE |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| MIL-C-38418 Revision E:1981 | CONTROL ASSEMBLY, GYROSCOPE, ATTITUDE A/A24G-39 |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-D-38134 Revision A:1971 | DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
| MS28061 Revision D:1979 | GAGE, PRESSURE, ENGINE, AND UTILITY, 2 INCH, FLANGE MOUNTED, BACK PORTS |
| MS28024 Revision H:1988 | INDICATOR, TURN AND SLIP, 4 MINUTE TURN, 2 3/4 INCH DIAL |
| MS24482 Revision A:1958 | TRANSMITTER, TEMPERATURE, ELECTRICAL RESISTANCE, ARMORED, BAYONET LOCKING TYPE, (50 DEGREE, TO 300 DEGREE, C) |
| MIL-STD-859 Revision B:2015 | STANDARD CALIBRATION TABLE FOR AERONAUTICAL PRESSURE MEASURING EQUIPMENT |
| MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
| MS28008 Revision B:1971 | INDICATOR TEMPERATURE, MULTI FUNCTION, ELECTRICAL RESISTANCE, SINGLE, CLAMP MOUNTED, MINUS 50 TO PLUS 50 DEGREES C, 2 INCH SIZE |
| MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL-I-38121 Revision C:1989 | INDICATOR, PRESSURE, EGU-9/A |
| MS28009 Revision B:1963 | INDICATOR - TEMPERATURE, ELECTRICAL RESISTANCE MULTI-FUNCTION, -70 TO +150 C, 2-INCH SIZE |
| MIL-I-27709 Revision A:1962 | INDICATOR, ATTITUDE ARU-14/A, REMOTE |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MS28018 Revision C:1971 | GAGE-PRESSURE, MANIFOLD, DIRECT INDICATING, 2 IN. SIZE, 10-75 IN. MERCURY |
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