MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
MIL-R-38370 Revision B:1972
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
MIL I 27197 : C
|
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
MIL I 5949 : G
|
INSTRUMENTS, FLIGHT AND ENGINE, AIRCRAFT, FUNCTIONAL TESTS AND TOLERANCES OF |
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-5099 Revision C:2011
|
INDICATOR, CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
MIL-I-85506 Base Document:1983
|
INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
MIL-A-81852 Revision A:1986
|
ALTIMETER-ENCODER AAU-32/A |
SAE AIR 1075 : 1996
|
BAROMETRY FOR ALTIMETER CALIBRATION |
MIL-A-81851 Revision B:1986
|
ALTIMETER AAU-31/A |
MIL I 5099 : B
|
INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
MIL C 27889 : D
|
COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
MIL O 38338 : C (1)
|
OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
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-A-38140 Revision B:1977
|
ALTIMETER, PRESSURE AAU-16/A |
MIL-A-27391 Revision B:1963
|
ALTIMETER, PRESSURE AAU-2A |