LIGHTING, INSTRUMENT, INTEGRAL, WHITE GENERAL SPECIFICATION FOR

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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
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)
DocumentType	Standard
Pages	16
PublisherName	US Military Specs/Standards/Handbooks
Status	Current

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, 6O TO 65O 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