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-L-25467 Revision D:1977
|
LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR |
MIL-I-83152 Revision B:1974
|
INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
MIL I 27197 : C
|
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
MIL C 38214 : B
|
COMPASS, MAGNETIC,MOUNTED |
MIL-T-38473 Revision A:1972
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TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
MIL-A-38140 Revision B:1977
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ALTIMETER, PRESSURE AAU-16/A |
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-DTL-25949 Revision F:1995
|
ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED |
MIL-PRF-27197 Revision F:2017
|
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
MIL-PRF-38135 Revision D:2014
|
INDICATOR, INDICATED AIRSPEED AVU-19A, STANDBY |
SAE ARP 6161 : 2011
|
FLIGHT COMPARTMENT GLARE |
MIL-I-27304 Revision E:1977
|
INDICATOR, RATE OF FLOW |
MIL-D-81641 Base Document:1972
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
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-A-81851 Revision B:1986
|
ALTIMETER AAU-31/A |
SAE ARP 798 : 2017
|
DESIGN CRITERIA FOR WHITE INCANDESCENT LIGHTED AEROSPACE INSTRUMENTS |
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-58067 Revision A:1977
|
INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
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 O 38338 : C (1)
|
OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
MIL-L-27160 Revision C:1972
|
LIGHTING, INSTRUMENT, INTEGRAL, WHITE GENERAL SPECIFICATION FOR |
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
MIL-C-81774 Revision A:1973
|
CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
MIL-G-23081 Revision C:1972
|
GYROSCOPE INDICATOR SYSTEM VERTICAL. |
MIL A 87211 : NOTICE 1
|
AIR DATA SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD ENES, WRIGHT PATTERSON, AFB OH 45433 6503 |
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-83245 Revision A:1994
|
INDICATOR SET, OIL PRESSURE A/A24J-17 |
MIL-I-83262 Revision B:1977
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
MIL-I-27673 Revision C:1993
|
INDICATOR, TRUE AIRSPEED AVU-15/A |
MIL-I-27623 Revision C:1972
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
MIL-I-83117 Revision B:1975
|
INDICATOR, ANGLE OF ATTACK |
MIL-I-5415 Revision C:1987
|
INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
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-23832 Revision A:1980
|
INDICATOR, TACHOMETER, TRIPLE POINTER, HELICOPTER |
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-V-85603 Base Document:1989
|
VOLTMETER, DC, AIRCRAFT, DIGITAL DISPLAY GENERAL SPECIFICATION FOR |
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 |
RE.AERO 79030 : 1991
|
GUIDE FOR RECONFIGURATING KEYBOARD DESIGN |