MIL C 38214 : B
|
COMPASS, MAGNETIC,MOUNTED |
MIL-T-27305 Revision C:1987
|
TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
MIL-I-85506 Base Document:1983
|
INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
MIL-T-38049 Revision A:1972
|
TRANSMITTER, PRESSURE TRU 60A |
MIL-I-5133 Revision C:1953
|
INDICATOR, ATTITUDE TYPE J 8 |
MIL I 25689 : A NOTICE 1
|
INDICATOR, ELECTRICAL TACHOMETER |
MIL-I-27304 Revision E:1977
|
INDICATOR, RATE OF FLOW |
MIL T 5882 : D
|
TRANSMITTER, PRESSURE, MULTIPURPOSE, 0-50 PSI, MS28005-1 |
MIL-A-81852 Revision A:1986
|
ALTIMETER-ENCODER AAU-32/A |
MIL-A-81851 Revision B:1986
|
ALTIMETER AAU-31/A |
MIL-DTL-25308 Revision C:2010
|
GAGE, PRESSURE, DIAL INDICATING, HYDRAULIC, TYPE ME-1 |
MIL-DTL-5882 Revision E:2013
|
TRANSMITTER, PRESSURE, MULTIPURPOSE, 0-50 PSI, MS28005-1 |
MIL C 27889 : D
|
COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
MIL-I-22126 Revision B:1972
|
INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
MIL I 83452 : LATEST
|
INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
MIL-C-6499 Revision E:1970
|
CLOCK, AIRCRAFT MECHANICAL TYPE A 13A |
MIL I 8136 : A
|
INDICATOR, FUEL FLOW RATE, SYNCHRO STYLE, SINGLE CLAMP MOUNTED 2 INCH SIZE 300 TO 3,000 PPH TYPE A 12 |
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
MIL-A-81403 Base Document:1967
|
ALTIMETER-ENCODER, AAU-21/A |
MIL-I-81400 Base Document:1966
|
INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
MIL-F-8378 Revision B:1975
|
FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
MIL-I-25482 Revision D:1993
|
INDICATOR, ENGINE TESTING |
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-I-25859 Revision C:1995
|
INDICATOR, THRUST AEU-2/A, SYNCHRO STYLE, PRESSURE RATIO, 1.2-3.4 UNITS, INTEGRALLY LIGHTED |
MIL-I-83262 Revision B:1977
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
MIL-I-7087 Revision A:1968
|
INDICATOR, PRESSURE OIL, 0-200 PSI |
MIL-I-7071 Revision B:1972
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
MIL-I-83117 Revision B:1975
|
INDICATOR, ANGLE OF ATTACK |
MIL-T-25485 Revision C:1974
|
TRANSMITTER, THRUST, SINGLE SYNCHRO STYLE, PRESSURE RATIO, TYPE MK-2 |
MIL-I-7084 Revision A:1988
|
INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
MIL-C-87975 Base Document:1985
|
CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
MIL-C-38207 Revision A:1965
|
CLOCK, AIRCRAFT, MECHANICAL ABU 11/A |
MIL-T-25307 Revision D:1985
|
TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
MIL-I-7075 Revision A:1965
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION -50 DEGREES TO +50 DEGREES C 2 INCH SIZE |
MIL-I-27667 Revision C:1990
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, EHU-16/A MULTIFUNCTION -70 DEGREES TO +150 DEGREES C |
MIL-I-26299 Revision G:1990
|
INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |