Unit Two review Quetions

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)

The __________ pumps provide fuel pressure to the engine driven pumps.

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 __________.

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)

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FUEL SYSTEM