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|  STUDENT ACTIVITY GUIDE
TOPIC:
T2 Electrical and Instrument Systems
1.
Three sources of DC power for the T2 aircraft are _______________, _______________,
and _______________.
2.
The purpose of the emergency electrical disconnect switch is to _______________
_______________ _______________ _______________ and should be in the
_______________ position.
3.
The voltmeters will indicate _______________ _______________ _______________
voltage, while the ammeters indicate current load on the _______________
4.
The electrical control transfer switch will assume control of _______________,
_______________, _______________, and _______________ from either cockpit.
5.
Select the statement(s) below which As/are true about the control transfer system:
a.
The NFO in the AFT cockpit can transfer control to the FWD cockpit.
b.
The illumination of a green light adjacent to the transfer control switch in the FWD
cockpit indicates the FWD cockpit has control.
c.
The illumination of a green light adjacent to the transfer control switch in the FWD
cockpit indicates the AFT cockpit has control.
d.
The pilot or NFO may take control, but cannot transfer control to the other cockpit.
6.
The primary buss can receive power from:
a.
The external power source
b.
The generators
c.
The batteries
d.
All of the above
7.
The monitor busses can be powered by the _______________ or by _______________
_______________, but cannot be powered by the _______________.
8.
With a dual generator failure, the _______________ and _______________
_______________ busses will be lost.
9.
The method of regaining the secondary buss from the aft cockpit with a dual generator
failure in flight is to _______________ _______________ _______________
_______________ _______________.
1-3
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