MIL-L-27160 Revision C:1972
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The latest, up-to-date edition.
LIGHTING, INSTRUMENT, INTEGRAL, WHITE GENERAL SPECIFICATION FOR
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Important note : Users cannot be edited or removed once added to your Multi user PDF.Details general requirements for a 5.0V illuminating system for integrally white-lighted aircraft instruments with incandescent lamps as the light source.
| Committee |
FSC 6620
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| DevelopmentNote |
C NOTICE 1 - Notice of Validation. C NOTICE 2 - Notice of Cancellation without Replacement. C NOTICE 3 - Notice of Reinstatement. C NOTICE 4 - Notice of Inactivation for New Design. C NOTICE 5 - Notice of Validation but remains Inactive for New Design. (09/2008) C NOTICE 6 - Notice of Validation but remains Inactive for New Design. (02/2015)
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| DocumentType |
Standard
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| Pages |
16
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-I-27674 Revision C:1994 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE MULTIFUNCTION, MINUS 5O DEG TO PLUS 2OO DEG C |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL |
| MIL-I-18856 Revision B:1969 | INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
| MIL-C-87979 Base Document:1987 | CLOCK, AIRCRAFT, ELECTRONIC |
| MIL-I-27191 Revision C:1995 | INDICATOR, POSITION, VARIABLE NOZZLE |
| MIL-I-83152 Revision B:1974 | INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
| MIL-I-38121 Revision C:1989 | INDICATOR, PRESSURE, EGU-9/A |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-I-27677 Revision E:1990 | INDICATOR, LIQUID OXYGEN QUANTITY |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-DTL-27188 Revision C:2006 | INDICATOR, PRESSURE EGU-2/A, OIL, 0-100 PSI |
| 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 27220 : B | INDICATOR SET, LIQUID OXYGEN QUANTITY A/A24J-8 |
| MIL-I-83449 Base Document:1974 | INDICATOR SET, LIQUID OXYGEN QUANTITY, A/A24J-21 |
| 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-27202 Revision A:1980 | INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-DTL-27193 Revision D:2017 | INDICATOR, ATTITUDE ARU-2B/A |
| JSSG-2010-5 Base Document:1998 | Crew Systems Aircraft Lighting Handbook |
| MIL-DTL-25949 Revision F:1995 | ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, 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)/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 |
| 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)/12(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)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-D-28728 Revision B:1986 | DIAL, CONTROL, MULTI-TURN COUNTERS, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-I-85506 Base Document:1983 | INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
| 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-R-81876 Revision B:1988 | RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
| MIL-I-27304 Revision E:1977 | INDICATOR, RATE OF FLOW |
| 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-I-27882 Revision A:1963 | INDICATOR, LIQUID OXYGEN, QUANTITY GMU-37/A |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| SAE ARP 798 : 2017 | DESIGN CRITERIA FOR WHITE INCANDESCENT LIGHTED AEROSPACE INSTRUMENTS |
| NASA STD 3000 VOL 2 : 1995 | MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 2 |
| MIL-DTL-83361 Revision B:2007 | INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
| MIL-I-21735 Revision A:1969 | Indicator, Airspeed and Mach Number, Pitot Static, 60 to 650 Knots |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| MIL-I-26689 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
| MIL-I-25931 Revision B:1964 | INDICATOR, POSITION, LANDING GEAR, SYMBOL-INDICATING, INTEGRALLY LIGHTED |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-25861 Revision D:1967 | INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
| MIL-P-38027 Revision A:1973 | PRESSURE INDICATING SYSTEM, HYDRAULIC A/A27 J-1 |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL I 7069 : A NOTICE 1 | INDICATORS, TACHOMETER, ELECTRIC, PERCENT SPEED TYPE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-27665 Revision B:1984 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE ABU-1O/A, -50 DEGREES TO +50 DEGREES C |
| MIL-I-27203 Revision B:1987 | Indicator, Position, Wing Flap |
| MIL-STD-35-109 Base Document:1976 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, INDICATORS, POINTER |
| MIL-I-27247 Revision C:1985 | INDICATOR, TEMPERATURE, SYNCHRO |
| MIL-A-27198 Revision B:1987 | ALTIMETER, PRESSURE AAU-7/A |
| MIL-DTL-27189 Revision E:2008 | INDICATOR, PRESSURE, OIL |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-I-83262-2 Base Document:1977 | INDICATOR, TEMPERATURE, THERMOCOUPLE, EHU-38/A |
| MIL-A-27261 Revision A:1966 | Accelerometer, Aircraft |
| MIL-A-81403 Base Document:1967 | ALTIMETER-ENCODER, AAU-21/A |
| MIL-I-38468 Revision A:1983 | INDICATOR, LIQUID OXYGEN QUANTITY GMU-59/A |
| MIL-A-25933 Revision B:1985 | ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
| MIL-I-38021 Revision A:1963 | INDICATOR, LIQUID OXYGEN QUANTITY GMU 39/A |
| MIL-I-27552 Revision C:1995 | INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-15A/A, POTENTIOMETER TYPE, WHITE LIGHTED |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-I-27672 Revision B:1987 | INDICATOR, POSITION ALU-4/1, HORIZONTAL STABILIZER |
| MIL-A-27670 Revision D:1994 | AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
| 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-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| 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-83245 Revision A:1994 | INDICATOR SET, OIL PRESSURE A/A24J-17 |
| MIL-I-27673 Revision C:1993 | INDICATOR, TRUE AIRSPEED AVU-15/A |
| MIL I 27189 : D | INDICATOR, PRESSURE OIL |
| 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-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
| MIL-I-25941 Revision D:1986 | INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
| 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-C-87975 Base Document:1985 | CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
| MIL-A-27671 Revision B:1965 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-C-38207 Revision A:1965 | CLOCK, AIRCRAFT, MECHANICAL ABU 11/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 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL-L-5667 Revision B:1964 | LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
| MIL-DTL-27190 Revision C:2006 | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-STD-1293 Base Document:1979 | ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT |
| 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-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 |
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