2A353N Practice Test

Listed below are sample questions for 2A353N from our database. Register now to start taking tests for this AFSC! We have 508 questions currently in the database for this category.

The version of this CDC we have in the database is 2A353N 01 0703, 02/03/04/05 0704, Edit Code 02

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  • 1 . The F–16’s emergency power unit provides a self-contained backup source of
    aircraft electrical and hydraulic power
  • 2 . How many controlling servo valves are contained in each F–117 integrated servo actuator?
    Three
  • 3 . The F–16’s hydraulic linear actuator receives hydraulic pressure from
    hydraulic system B only
  • 4 . The bolt used where heavy tension or lengthwise stress must be sustained is a(n)
    hexhead
  • 5 . To tighten cannon plugs, do not use
    channel lock pliers
  • 6 . The F–22 system that dehumidifies the pre-cooled air utilizing a boot strapped compressor, turbine, and water collector is the
    refrigeration system
  • 7 . The main landing gear strut on the U–2 is constructed of
    titanium
  • 8 . The unit capable of providing AC and DC electrical power, in addition to pneumatic power, for ground maintenance is the
    A/M32A–60
  • 9 . The U–2 exhaust system consists of the tail pipe and
    fan flow adapter diverter
  • 10 . The F–117’s emergency power unit can be manually operated from the control switches in the
    left main landing gear (MLG)wheel well