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UNIT TWO REVIEW QUESTIONS
1.  Each wing tank holds __________ gallons and the fuselage tank holds __________
gallons for a total of __________ gallons (approx. __________ lbs JP-5).
2.  Gravity fueling is normally accomplished through overwing ports located on the
outboard section of each wing. (TRUE/FALSE)
3.
The __________ pumps provide fuel pressure to the engine driven pumps.
4.
The wing-mounted boost pump is energized whenever the __________ switch is ON.
5.  Under most conditions, the FUEL X-FEED & TANK SEL switch is left in the
__________ position.
6.  The LOW FUEL LEVEL caution fight illuminates at an indicated fuel quantity of
__________ lbs or less on either fuel quantity gauge.
7.  The fuel filter is downstream of the gear element of the engine driven pump.
(TRUE/FALSE)
8.  The motive flow for the transfer ejector in the forward section of each wing tank is
provided by __________.
9.
Suction feed is reliable to at least __________ feet regardless of fuel temperature.
10. The FUEL FILTER BLOCK caution light will illuminate with a differential of
__________ to psi. Actual bypass of the filter occurs at __________ to _________ psi.
11. Allowable fuel imbalance is __________ lbs in level flight or __________ lbs for
takeoff and landing.
12.  The __________ position of the FUEL X-FEED & TANK SEL switch is used for
single engine operation or if the FUEL LOW PRESS fight illuminates.
13. Selecting X-FEED automatically turns on __________ and opens the __________ valve
(s).
14. The LOW FUEL LEVEL caution fight operates independently of the fuel quantity
gauges. (TRUE/FALSE)
15. The digital fuel remaining indicators operate independently of the fuel quantity gauges.
(TRUE/FALSE)
2-6
FUEL SYSTEM


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