MIL I 5949 : G
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INSTRUMENTS, FLIGHT AND ENGINE, AIRCRAFT, FUNCTIONAL TESTS AND TOLERANCES OF
Publisher
Withdrawn date
07-23-2013
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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Withdrawn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 | Transmitters, 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 (No S/S Document) |
| 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 Deg. C |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-I-27680 Revision C:1973 | Indicator, Altitude ARU-12/A, Remote (No S/S Document) |
| MS28034 Revision B:2007 | Bulbs, Temperature, Electrical Resistance (-70 Deg. C TO +300 Deg. C) |
| MS28010 Revision D:1992 | Indicators, 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 (NO S/S DOCUMENT) |
| MS28063 Revision A:1959 | Gages, Pressure, Engine and Utility, 2-Inch, Flange- or Port-Mounted, Bottom Port |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU-60-A (NO S/S DOCUMENT) |
| MS24478 Revision C:2006 | Gage, Single 1 Inch Dial, Pneumatic Pressure |
| MS24569 Revision D:1966 | Indicator, Temperature - Thermocouple, Self Balancing Potentiometer Type |
| 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 (NO S/S DOCUMENT) |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL (NO S/S DOCUMENT) |
| MIL-C-26485 Revision D:1968 | Control Assembly, Attitude Gyroscopic AF/A24G-1A (No S/S Document) |
| MIL-G-25591 Revision E:1981 | Gyroscope, Rate, Switching, Type MC-1 |
| MS3106 Revision D:1992 | Connector, Plug, Electric, Straight, Solder Contacts, AN Type (S/S by SAE-AS31061) |
| 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 (No S/S Document) |
| MS28061 Revision D:1979 | Gage, Pressure, Engine and Utility, 2-Inch, flange-Mounted, Back Ports |
| MS28024 Revision H:1988 | Indicators, Turn and Slip, 4-Minute Turn, 2 3/4 Inch Dial (No S/S Document) |
| MS24482 Revision A:1958 | Transmitter, Temperature, Electrical Resistance, Armored, Bayonet Locking Type, (-50 Degrees C to 300 Degrees C) (S/S by MIL-DTL-25446) |
| 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-1 (No S/S Document) |
| MS28008 Revision B:1971 | Indicator, Temperature, Multi-Function, Electrical Resistance, Single, Clamp Mounted, Minus 50 Degrees, 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 (No S/S Document) |
| MIL-I-38121 Revision C:1989 | Indicator, Pressure, EGU-9A (No S/S Document) |
| MS28009 Revision B:1963 | Indicator - Temperature, Electrical Resistance Multi-Function, -70 to +150 C, 2-Inch Size |
| MIL-I-27709 Revision A:1962 | Indicator, Altitude, ARU-14/A, Remote (No S/S Document) |
| 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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