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.

The version of this CDC we have in the database is 2A353 0703, Edit Code 02

« Return to AFSC List
  • 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