2A353 (Legacy) Practice Test
Listed below are sample questions for 2A353 (Legacy) from our database. Register now to start taking tests for this AFSC! We have 395 questions currently in the database for this category.
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The version of this CDC we have in the database is 2A353 0703, Edit Code 02
1 . On the F-15 aircraft, the directional feel trim actuator connects to the
torque tube assembly forward of the rudder pedals
2 . What prevents fluid loss when the filter bowl and element are removed from the F-16's hydraulic system A pressure manifold?
Internal shutoff valve
3 . Special bolts are identified by
the bolt head marked with the letter S
4 . The F-100 engine exhaust nozzle position transmitter is driven by
the convergent exhaust nozzle control
5 . The U-2 exhaust system consists of the tail pipe and
fan flow adapter diverter
6 . The internal fuel storage system on the F-16 consists of
seven fuel tanks
7 . Radiation hazards are affected by
strength of emission, time of exposure, and weather
8 . To disable ignition power box 1 when performing a test of ignition power box 2 in the RQ-1's ignition test circuit, ignition test relay
1 must be energized
9 . The external power monitor on the A-10 measures the frequency, voltage, and phase sequence of external AC power applied to the aircraft and
determines whether the power is compatible with the aircraft electrical system
10 . The type of TO improvement issued for all TCTO deficiencies is
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