MIL-L-25467 Revision D:1977
Current
Current
The latest, up-to-date edition.
LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR
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Language(s)
English
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Details requirements for a 5-volt incandescent or 115 volt electroluminescent illuminating system for red integrally lighted aircraft instruments, and specifies test procedures applicable to the lighting system for aircraft instruments.
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Standard
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14
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| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-C-27298 Revision B:1980 | CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
| MIL-T-38473 Revision A:1972 | TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
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| MIL-I-21206 Revision B:1960 | Indicator, Rate of Flow, Fuel; EFU-7/A (300-5000-15000 PPH) |
| MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-I-38338 Revision D:1991 | INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
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| MIL-DTL-27193 Revision D:2017 | INDICATOR, ATTITUDE ARU-2B/A |
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| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-7788 Revision H:2011 | PANELS, INFORMATION, INTEGRALLY ILLUMINATED |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-G-19053 Revision C:1957 | GAGE - AIRCRAFT, CAPACITANCE, LIQUID OXYGEN CONVERTER, GENERAL SPECIFICATION FOR |
| MIL I 82356 : NOTICE 1 | INSTRUMENTS, SIMULATED, FOR AIRCRAFT TRAINING DEVICES; GENERAL SPECIFICATION FOR |
| MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
| MIL-C-25050 Revision A:1963 | COLORS, AERONAUTICAL LIGHTS AND LIGHTING EQUIPMENT, GENERAL REQUIREMENTS FOR |
| MIL-I-25852 Revision B:1981 | INDICATOR, TEMPERATURE, THERMO COUPLE EHU-4/A |
| MIL-G-8798 Base Document:1956 | GAGE SYSTEM, FUEL QUANTITY, CAPACITOR TYPE NONVACUUM TUBE, INTEGRALLY LIGHTED GENERAL SPECIFICATION FOR |
| MIL-I-21203 Revision A:1962 | Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro |
| SAE AS 18276 : 2014 | LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
| MIL-A-23887 Revision A:1965 | Altimeter Set, Electronic AN/APN-141(V) |
| MIL-I-27304 Revision E:1977 | INDICATOR, RATE OF FLOW |
| MIL-I-81454 Base Document:1967 | INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
| MIL-I-26382 Revision C:1994 | Indicator Set, Liquid Oxygen Quantity A/A24J-4 and A/A241-8 |
| MIL-I-25863 Revision D:1990 | INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-A-81852 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-DTL-27189 Revision E:2008 | INDICATOR, PRESSURE, OIL |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| MIL-I-5482 Revision C:1960 | INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE |
| NASA STD 3000 VOL 2 : 1995 | MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 2 |
| MIL-I-21735 Revision A:1969 | Indicator, Airspeed and Mach Number, Pitot Static, 60 to 650 Knots |
| MIL-I-18804 Revision B:1964 | INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| FAA AC 20-74 : 1971 | AIRCRAFT POSITION AND ANTICOLLISION LIGHT MEASUREMENTS |
| MIL-I-26689 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
| MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
| MIL-I-25931 Revision B:1964 | INDICATOR, POSITION, LANDING GEAR, SYMBOL-INDICATING, INTEGRALLY LIGHTED |
| MIL-PRF-38214 Revision D:2008 | COMPASS, MAGNETIC, MOUNTED |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-27280 Revision A:1960 | INDICATOR, INDICATED AIRSPEED AVU-10/A |
| MIL-I-25861 Revision D:1967 | INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
| SAE AS25050B | Colors, Aeronautical Lights and Lighting Equipment, General Requirements For |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
| MIL-S-52156 Revision D:1988 | SURVEYING INSTRUMENT, DISTANCE MEASURING, ELECTRONIC MICROWAVE |
| MIL-A-27198 Revision B:1987 | ALTIMETER, PRESSURE AAU-7/A |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-A-27261 Revision A:1966 | Accelerometer, Aircraft |
| MIL-A-81403 Base Document:1967 | ALTIMETER-ENCODER, AAU-21/A |
| MIL-I-81400 Base Document:1966 | INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-G-23081 Revision C:1972 | Gyroscope Indicator System, Vertical |
| MIL-A-49079 Revision A:1986 | ALTIMETER SET, ELECTRONIC AN/APN-209(V) (UNITS OF) |
| MIL-A-25933 Revision B:1985 | ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
| MIL-A-81605 Revision D:1984 | ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
| MIL-I-83262 Revision B:1977 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| MIL-I-25950 Revision B:1967 | INDICATOR, PRESSURE, OIL, 0-100 PSI |
| MIL-I-7071 Revision B:1972 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-A-81296 Revision D:1985 | ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
| MIL-I-25941 Revision D:1986 | INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
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| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
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| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| MIL-I-27667 Revision C:1990 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, EHU-16/A MULTIFUNCTION -70 DEGREES TO +150 DEGREES C |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL I 25860 : A | INDICATOR, RATE OF FLOW EFU-1/A, 0-6,000-24,000 PPH, 2-INCH, INTEGRALLY LIGHTED |
| MIL-L-5667 Revision B:1964 | LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
| MIL-V-85603 Base Document:1989 | VOLTMETER, DC, AIRCRAFT, DIGITAL DISPLAY GENERAL SPECIFICATION FOR |
| MIL-STD-1293 Base Document:1979 | ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT |
| MIL-I-26380 Revision B:1964 | INDICATOR, LIQUID OXYGEN QUANTITY GMU-5/A |
| MIL-I-25992 Revision A:1959 | INDICATOR, BEARING DISTANCE HEADING ID 526A ARN |
| MIL-A-27391 Revision B:1963 | ALTIMETER, PRESSURE AAU-2A |
| ARINC 575 : 68 SUPP 3 | MARK 3 SUBSONIC AIR DATA SYSTEM (DIGITAL) DADS |
| MS27570 Base Document:1967 | LAMP, INCANDESCENT MINIATURE INTEGRAL LIGHTING, T-1 1/4 SIZE |
| MS25237 Revision D:1978 | LAMP, INCANDESCENT, SINGLE CONTACT MIDGET FLANGED BASE (T-1-3/4 BULB) |
| MS24367 Revision C:1971 | LAMP, INCANDESCENT MINIATURE INTEGRAL LIGHTING |
| MIL-C-25050 Revision A:1963 | COLORS, AERONAUTICAL LIGHTS AND LIGHTING EQUIPMENT, GENERAL REQUIREMENTS FOR |
| MIL-C-14806 Revision A:1969 | COATING, REFLECTION REDUCING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES |
| MS24515 Revision F:1979 | LAMPS, INCANDESCENT, T-1, SUB-MIDGET FLANGED |
| MS27571 Base Document:1967 | LAMP, INCANDESCENT MINIATURE INTEGRAL LIGHTING, T-1 SIZE |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| MS27569 Base Document:1967 | LAMP, INCANDESCENT MINIATURE INTEGRAL LIGHTING, T-1 3/4 SIZE |
| MIL-C-81774 Revision A:1973 | CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
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