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 . On the F–22, what performs the BIT on the hydraulic components?
  • 2 . On the F–15 aircraft, how long does utility system non-reservoir level-sensing maintain pressure if the aircraft develops a leak in the utility hydraulic system?
    As long as there is hydraulic fluid left in the utility reservoir
  • 3 . How many separate fluid chambers are in the F–16’s hydraulic system A reservoir?
  • 4 . The F–22 cockpit distribution and defog system provides air for the canopy seal, cockpit pressurization, canopy defog, and the
    pilots thermal cooling garment
  • 5 . The delivery rating of one of the F–16 accessory drive gearbox-mounted hydraulic pumps is
    42.5 GPM at 3,100 psi
  • 6 . On the F–100 engine, what reduces the fuel flow during engine start?
    Fuel derichment valve
  • 7 . The symbol entered on the forms if an aircraft exceeds the PDM cycle by 90 days and an extension is not granted is a
    red X
  • 8 . The correct way to detect broken wires on a cable is to
    pass a cloth along the length of cable
  • 9 . On the ignition test set, what monitors the output of energy?
    Stored energy meter
  • 10 . The interface between the electrical power system generators and the electrical power subsystem on the F–22 is the
    generator distribution center