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CHAPTER TEN
STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
CHAPTER TEN REVIEW
1.
The standby instruments include:
2.  The cabin __________________, __________________, ___________________, and
_____________________, receive information from the CP's pitot static system.
3.  The standby attitude indicator can provide attitude information for approximately ___
minutes following a complete electrical failure.
4.
The standby attitude indicator can continue to supply attitude information even after all
power, including the standby battery, is lost. (T/F)
5.  The magnetic compass is unaffected by the use of windshield heat or operation of the
defog/heater blower units. (T/F)
6.
The left pitot static system is connected to:
7.
The right pitot static system is connected to:
8.
Static ports are located ___________________________________.
a.
on the left side of the fuselage only
b.
on the right side of the fuselage only
c.
on each side of the fuselage
9.
List the components of the avionics system.
10. How is the avionics system powered on?
11. There are ________ antennas mounted on and in the aircraft.
a.
15
b.
16
c.
17
d.
18
12. The ELT transmitter antenna is located __________________________.
13. The CP's EADI and EHSI receive information from _______________________.
a.
the P's systems
b.
the CP's systems
c.
both a and b
d.
neither a or b
10-14
AVIONICS


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