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|  CHAPTER EIGHT
STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
CHAPTER EIGHT REVIEW
1.
List the areas protected by the icing protection systems:
2.
The leading edges of the wings are protected from ice formation using ___________.
a.
electrical heating elements
b.
engine bleed air
c.
both a and b
d.
neither a or b
3.
Engine bleed air is regulated at _________ psi.
a.
36 to 42
b.
28 to 34
c.
35 to 40
d.
38 to 44
4.
What is the warning associated with activating the wing anti-ice system in flight?
5.
The wing anti-ice system may be operated on the ground at any time. (T/F)
6.
How many overtemperature switches are installed in each wing?
a.
2
b.
3
c.
4
d.
5
7.
The ice protection system for the horizontal stabilizer utilizes __________________.
a.
bleed air
b.
electrical heating elements
c.
both a and b
d.
neither a or b
8.
The anti-ice and deice systems should not be operated simultaneously. (T/F)
9.
What is indicated by the illumination of the STB ANTI-ICE FAIL light on the main
annunciator panel?
10. What is indicated by the illumination of the white operation lights above the anti-ice and
deice switches on the overhead panel?
8-6 ANTI-ICE AND DEFOG SYSTEMS
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