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STUDENT GUIDE T-39N/G NATOPS
UNIT SIX REVIEW QUESTIONS
1.
Anti-icing systems shall be turned on when operating in _______________ with a temperature
range of _______________ to _______________C.
2.
A minimum of _______________ EPR is required to operate the engine anti-ice system.
3.
The engine ignition switch should be placed in NORMAL when the anti-ice systems are turned
on. (TRUE/FALSE)
Placing -the ENGINE & RAM AIR INLETS switch ON opens the bleed air shut-off valves for
4.
engine anti-icing and provides power to electrically heat the __________ and __________.
5.
With weight off the wheels, electrical anti-icing is, automatically provided to the
_____________and_____________.
6.
The stall warning vanes will be heated in flight as long as power is available to the bus.
(TRUE/FALSE)
7.
The AOA heater will operate in flight with only one generator on line. (TRUE/FALSE)
8.
Electrical power to anti-ice and bird proof the forward windshields is controlled by
the__________switches and the _______________ switch.
9.
The SIDE WINDSHIELD switch sends DC secondary bus power to heat the _______________
and _______________ and both _______________.
10.  The temperature of all heated windows except the _______________ is monitored for the
WINDSHIELD HOT caution light.
11.  While taxiing for takeoff, you get a LH AC GEN OFF caution light. No corrective action is
necessary, since output is limited below 58% rpm. (TRUE/FALSE)
12.
If either windscreen is unheated, airspeed is limited to ___________ KIAS below 10000 feet.
13.  The airfoil de-icing system is designed to be used BEFORE ice has accumulated on the leading
edges of the wing and empennage. (TRUE/FALSE)
14.  When the PNEU BOOTS switch is selected to HVY, the dwell time between boot inflation is
_______________ seconds.
15.
Operation of the de-icing system can be monitored by _______________.
16.
If manual inflation of the de-ice boots is desired, it can be accomplished by _______________.
ANTI-ICE/DE-ICE SYSTEMS
6-5


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