scope:

The test equipment covered by this specification shall be for flight line and shop use. The test equipment shall provide adjustable and regulated, self-generated, pneumatic pressures for simulating altitudes and airspeeds during ground testing of aircraft air data sensing equipment. The test equipment shall further provide regulation of pressure and vacuum from an external source to simulate engine bleed air to test the Air Data Computer Set, CPK-30/A24G-12 and the Angle of Attack Transmitter, TRK-48/A24G-12.

The TEST SET, PNEUMATIC PRESSURE AN/PSM-15C shall consist of the following items:

ITEM TYPE DESIGNATION APPL. PARA. Simulator, Pneumatic SM-392(*)/PSM-15C 3.4.1 Cover, Test Set CW-756(*)/PSM-15C 3.4.2 Cable Assembly, Power W1 of AN/PSM-15C 3.4.3.1 Cable Assembly Ground W2 of AN/PSM-15C 3.4.3.2 Hose Assembly, Pneumatic, 3.4.4.1 Pitot Pressure -3 Hose Assembly, Pneumatic, 3.4.4.2 Static Pressure (Corrected) -4 Hose Assembly, Pneumatic, 3.4.4.3 Engine Bleed -5 Hose Assembly, Pneumatic, 3.4.4.4 Static Pressure (Indicated) -6 Wrench, Hexagon 0.049 Flats 3.4.5.1 Wrench, Hexagon 0.187 Flats 3.4.5.2 Wrench, Hexagon 0.0615 Flats 3.4.5.3

intended Use:

The AN/PSM-150 is intended for use on the flight line or in the shop to perform checkout tests on air data sensing equipment used in aircraft.