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|  STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
CHAPTER EIGHT
11. What is the length of the manual deice cycle?
a.
15 seconds
b.
20 seconds
c.
25 seconds
d.
30 seconds
12.
Why is there a limitation on operating the flaps while using manual deice?
13. Manual deice may be used for deicing on the ground. (T/F)
14. List the engine components which continuously receive anti-icing.
15. Engine anti-ice must not be operated on the ground above ________ degrees C.
a.
8
b.
10
c.
12
d.
14
16. What is indicated by the illumination of L or R ENG ICE TEMP LO annunciator on the
main annunciator panel?
17. The pitot, static, and AOA systems are protected from ice by ____________.
a.
electrical heating elements
b.
bleed air
c.
both a and b
d.
neither a or b
18. The windshield itself does/does not incorporate an anti-ice or deice system.
ANIT-ICE AND DEFOG SYSTEMS
8-7
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