01-379-3503
Turn And Slip Indicator
01-379-5004
Pitot-static Tube
Used on a hercules helicopter
01-379-5475
Pitot-static Tube
Used on C-17A. aerodynamically compensated; fuselage mounted
01-379-6750
Altitude Computer
01-379-8524
Indicator Housing
Used on 6610-00-887-9301.
01-380-2087
Air Speed Indicator
01-380-5627
Indicator Housing
01-380-6374
Altitude Computer
01-381-3181
Angle Indicator
01-381-8898
Air Data Computer
01-382-1461
Turn And Slip Indicator
Used on aircraft model av-8b.
01-382-1472
Turn And Slip Indicator
Used on aircraft model av-8b.
01-382-4974
Pressure Altimeter
Used on h1 helo. 2.360" overall width
01-382-7894
Pressure Altimeter
01-383-1697
Turn And Slip Indicator
01-383-1730
Pressure Altimeter
01-383-1731
Mechanical Accelerometer
01-383-1830
Air Speed Indicator
01-383-3750
Angle Of Attack Transmitter
Used on pacer dawn. 7.125" overall length operating temp based on thermostat opening
01-383-3780
Angle Of Attack Transmitter
Used on pacer dawn. 7.125" overall length operating temp based on thermostat opening
01-383-4458
Pitot-static Tube
Used on pacer dawn. 14.750" overall length
01-383-6963
Attitude Indicator
Used on dynamic control loading chassis assy.
01-383-6982
Flight Director Computer
Used on dynamic control loading chassis assy.
01-383-7240
Position Indicator
Used on dynamic control loading chassis assy.
01-383-7248
Flight Director Computer
Used on dynamic control loading chassis assy.
01-383-7393
Pitot-static Tube
Used on pacerdawn. static pressure: 9/16-18 unjf-3a thread, fitting per MS33656-6; pitot pressure: 7/16-20 unjf-3a thread
01-383-7419
Aircraft Instruments Manifold
Used on pacer special. 10.750" overall length 1.248" overall width one elec. connection: 10.75 in. l, 2 pitot connections: both 9.75 in. l, 2 static connections: 9.0 & 10.5 in. l
01-384-0112
Attitude Indicator
Used on oh-58a and oh-58c rotary wing aircraft.
01-384-0601
Indicator Housing
Used on attitude indicator (25583) p/n 501-1509-01; c-17a airlifter. inclinometer housing
01-384-0636
Venturi Tube
Used on apu heating. 7.220" overall length 1) venturi p/n 1221484-101, (1) fitting p/n 1221485-103, (1) fitting p/n 1221485-101, fittings tig arc welded to venturi
01-384-1032
Air Data Computer
Used on pacer dawn. electrostatic discharge sensitive
01-384-1400
Flight Data Recorder Memory Unit
Used on pacer dawn. 4.300" overall length 5.500" overall width crash survivable memory unit
01-384-1462
Position Indicator
Used on aircraft model f-14d. transmitter, indictor set, wing sweep a/A37j-6
01-384-6109
Angle Indicator
Used on dynamic control landing chassis assy.
01-384-7512
Position Transmitter
Used on pacer special. 12.930" overall length 9.230" overall width nuclear hardness critical
01-385-0691
Mechanical Accelerometer
01-385-1764
Air Speed Indicator
Used on mc-130e combat talon 1.
01-385-1766
Angle Indicator
Used on mc-130e combat talon 1. dual indicators -1. angle of attack-indicated by pointer, 2. pitch angle-rotates inside indicator on card
01-385-1771
Servo Controlled Autom Altimeter
Used on mc-130e combat talon 1.
01-385-8527
Position Indicator
Used on mc-130e combat talon 1.
01-386-4582
Instrument Landing Air Indicator
01-386-7542
Attitude Indicator
01-387-0676
Pressure Altimeter
01-387-3648
Angle Of Attack Transmitter
01-388-0276
Indicator Housing
Used on 6610-01-286-2306. air-speed indicator. 2) 5 volt lamps w/ solder lead connectors, screen filter insert w/ rubber 0-ring
01-388-5249
Angle Indicator
01-388-6661
Attitude Indicator
Used on C-17. the lighting spectral distribution is anvis green; indicator will incorporate a vertical gyroscope mounted on a pitch gimbal/mounted on a roll gimbal; lighting 5vac; wt. 4.5 lbs. max; temp.range minus 65.0 deg. to positive 160..0 deg. f; altitude: minus 1, 800 to 50, 000 ft.; includes a time totalizing meter
01-388-8313
Servo Controlled Autom Altimeter
Maau-34b/a aviation red
01-389-0620
Servo Controlled Autom Altimeter
Aau-34c/a night vision green
01-389-2935
Stabilization Data Indicator
Lower indicator box assy
