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 |