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  • MIL-L-25467 Revision D:1977

    Current The latest, up-to-date edition.

    LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR

    Available format(s):  PDF

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    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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    Document Type Standard
    Product Note NEW CHILD NOT 1 2019 IS NOW ADDED.
    Publisher US Military Specs/Standards/Handbooks
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    MIL-I-25859 Revision C:1995 INDICATOR, THRUST AEU-2/A, SYNCHRO STYLE, PRESSURE RATIO, 1.2-3.4 UNITS, INTEGRALLY LIGHTED
    MIL-I-27674 Revision C:1994 INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE MULTIFUNCTION, MINUS 5O DEG TO PLUS 2OO DEG C
    MIL-L-85762 Revision A:1988 LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
    MIL-I-18856 Revision B:1969 INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067
    MIL-T-38034 Revision E:1970 TIMER, FIRE CONTROL, BOMBING, DUAL
    MIL-C-87979 Base Document:1987 CLOCK, AIRCRAFT, ELECTRONIC
    MIL-I-38121 Revision C:1989 INDICATOR, PRESSURE, EGU-9/A
    MIL C 38214 : B COMPASS, MAGNETIC,MOUNTED
    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
    MIL-A-38140 Revision B:1977 ALTIMETER, PRESSURE AAU-16/A
    MIL-I-81186 Base Document:1966 INDICATOR, RATE OF FUEL FLOW SYNCHRO TYPE, M590360
    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
    MIL-I-27196 Revision C:1988 INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED
    MIL I 27279 : B INDICATOR, MACH NUMBER AVU-11/A, INTEGRAL LIGHTING
    MIL-DTL-27193 Revision D:2017 INDICATOR, ATTITUDE ARU-2B/A
    MIL-DTL-25949 Revision F:1995 ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED
    SAE AS 23479 : 2012 INDICATOR, PRESSURE, 1 1/2-INCH, INTEGRALLY LIGHTED
    DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    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/A24J-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, 6O TO 65O 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-1O13(*)/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 AS 25050B : 2017 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
    MIL-STD-411 Revision F:1997 AIRCREW STATION ALERTING SYSTEMS
    MIL-I-27619 Revision G:1974 INDICATORS, ATTITUDE DIRECTOR
    MIL-C-38207 Revision A:1965 CLOCK, AIRCRAFT, MECHANICAL ABU 11/A
    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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