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.
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The version of this CDC we have in the database is 2A353N 01 0703, 02/03/04/05 0704, Edit Code 02
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?
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)
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
7 . The main landing gear strut on the U–2 is constructed of
8 . The unit capable of providing AC and DC electrical power, in addition to pneumatic power, for ground maintenance is the
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
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