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|  CHAPTER FOUR
STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
CHAPTER FOUR REVIEW
1. The fuel supply system is designed to operate between ____________ and
_____________, within the temperature range _______ and __________ degrees C.
2.
Discuss the fuel flow throughout the fuel supply system.
3. During normal operation, the ____________________________ provides fuel feed to each
engine.
4.
The boost pump is used during:
_________________________
_________________________
_________________________
_________________________
5.
After engine starting, the boost pump must be manually shut off. (T/F)
6.
How many fuel tanks comprise the fuel storage subsystem?
a.
4
b.
5
c.
6
d.
7
7.
Which of the following is not a purpose of the boost pump?
a.
Crossfeed
b.
Backup for the primary jet pumps
c.
Engine starting
d.
Transfer fuel from the mid-fuselage tanks into the wing tanks
8. In the automatic mode, the boost pump will operate when the fuel feed line pressure drops
below _______ psi.
9. Transfer pumps must be manually shut off once all fuel has been pumped from the mid-
fuselage tanks to the wings. (T/F)
10. ___________________________ are used to maintain fuel quantity in each feed chamber.
4-6
FUEL SUPPLY SYSTEM
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