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The version of this CDC we have in the database is 2A656 01 1210, 1212, 1302, Edit Code 04
1 . One purpose of the fan in the aircraft bleed air system cooling turbine and fan assembly is to prevent
turbine over speeding.
2 . For aircraft pressurization systems to operate properly, you should note that as the aircraft pressurizes, the outflow safety valve opens at the same time once the
pneumatic relay opens.
3 . While troubleshooting an inoperative taxi light in the aircraft lighting system, if you find 28-volts alternating current (VAC) on terminal A2 of the taxi light relay your next checkpoint would usually be at the
lamp terminals to ground
4 . The flow control valve control in the bleed air air-conditioning system controls flow by maintaining a constant differential pressure between the
inlet and throat of the venturi.
5 . What controls the flow of the current carriers in a transistor?
6 . All of these aircraft systems use engine bleed air except
7 . How many gallons of liquid coolant should initially be pumped into the aircraft liquid coolant system with the radar shunt hose installed?
8 . You should check this component first if one outflow safety valve opens fully when the aircraft starts to pressurize.
9 . What is the minimum personal protective equipment (PPE) you are required to wear when performing routine sealed lead-acid batteries (SLAB) maintenance?
Safety toe boots only.
10 . Prior to removing any connector plug in the nose wheel steering system, you must
disconnect the power
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