MIL-L-27160 Revision C:1972
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Current
The latest, up-to-date edition.
Lighting, Instrument, Integral, White, General Specification for
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Published date
03-03-1972
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€16.67
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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.
| 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 |
17
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the general requirements for a 5.OV illuminating system for integrally white-lighted aircraft instruments using incandescent lamps as the light source.
| MIL-I-27674 Revision C:1994 | Indicator, Temperature, Electrical Resistance (No S/S Document) |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL (NO S/S DOCUMENT) |
| MIL-I-18856 Revision B:1969 | Indicator, Angle of Attack, 28V DC MS28062 and MS28067 |
| MIL-C-87979 Base Document:1987 | Clock, Aircraft, Electronic (No S/S Document) |
| 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-9A (No S/S Document) |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-I-27677 Revision E:1990 | Indicator, Liquid Quantity Oxygen (No S/S Document) |
| 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 (No S/S Document) |
| MIL-A-38140 Revision B:1977 | Altimeter, Pressure AAU-16/A (No S/S Document) |
| 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 (S/S by NASM28728) |
| 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) (No S/S Document) |
| 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 ARP798B | 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 (No S/S Document) |
| MIL-I-25931 Revision B:1964 | Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted (No S/S Document) |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-25861 Revision D:1967 | Indicator, Pressure, Hydraulic, 0-4,000 PSI, Integrally Lighted |
| MIL-P-38027 Revision A:1973 | PRESSURE INDICATING SYSTEM, HYDRAULIC A/A27J-1 (S/S BY MIL-I-27190 AND MS28005) |
| 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, Minus 50 Degrees to Plus 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 (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| MIL-A-27261 Revision A:1966 | Accelerometer, Aircraft |
| MIL-A-81403 Base Document:1967 | Altimeter-Encoder, AAU-21/A (No S/S Document) |
| 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/A, Horizontal Stabilizer (No S/S Document) |
| MIL-A-27670 Revision D:1994 | Amplifier-Indicator Group Indicated Airspeed A/A24G-10 (No S/S Document) |
| MIL-A-83212 Revision A:1976 | Altimeter, Pressure AAU-27/A (No S/S Document) |
| MIL-G-26988 Revision C:1971 | Gage, Liquid Quantity, Capacitor Type Transistorized, General Specification for (No S/S Document) |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-A-81605 Revision D:1984 | Altimeter Set, Electronic AN/APN194(V) |
| MIL-I-83262 Revision B:1977 | Indicator, Temperature, Thermocouple Hermetically Sealed, General Specification for (No S/S Document) |
| MIL-I-83245 Revision A:1994 | Indicator Set, Oil Pressure A/A24J-17 (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-I-27848 Revision B:1994 | Indicator, Horizontal Situation AQU-4/A |
| MIL-I-38258 Base Document:1965 | Indicator, Attitude ARU-18/A, Director (No S/S Document) |
| MIL-C-87975 Base Document:1985 | Clock, Aircraft, Mechanical ABU-32/A (No S/S Document) |
| MIL-A-27671 Revision B:1965 | Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-11 (No S/S Document) |
| 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 |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-I-26299 Revision G:1990 | Indicator, Rate of Flow, 0-5,000 PPH, Integrally Lighted (No S/S Document) |
| 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 (No S/S Document) |
| 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 (NO S/S DOCUMENT) |
| MS27570 Base Document:1967 | LAMP, INCANDESCENT MINIATURE INTEGRAL LIGHTING, T-1 1/4 SIZE (NO S/S DOCUMENT) |
| MS25237 Revision D:1978 | Lamp, Incandescent, Single Contact Midget Flanged Base (T-1-3/4 Bulb) (S/Sby MIL-L-6363/8) |
| MS24367 Revision C:1971 | LAMP, INCANDESCENT - MINIATURE INTEGRAL LIGHTING (NO S/S DOCUMENT) |
| 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 (NO S/S DOCUMENT) |
| MS27571 Base Document:1967 | LAMP, INCANDESCENT - MINIATURE INTEGRAL LIGHTING, T-1 SIZE (NO S/S DOCUMENT) |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MS27569 Base Document:1967 | LAMP, INCANDESCENT-MINIATURE INTEGRAL LIGHTING, T-1 3/4 SIZE (NO S/S DOCUMENT) |
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