LEARJET 45 PILOT TRAINING MANUAL
5-24
FOR TRAINING PURPOSES ONLY
FlightSafety
international
1. The approximate maximum usable fuel
capacities of each fuel tank are:
A. Each wing - 1,600 pounds,
fuselage - 2,800 pounds
B. Each wing - 1,680 pounds,
fuselage - 2,700 pounds
C. Each wing - 1,400 pounds,
fuselage - 2,400 pounds
D. Each wing - 1,630 pounds,
fuselage - 2,340 pounds
2. The standby fuel pumps are used for all
of the following functions except:
A. Engine start.
B. As a backup to the main jet pumps.
C. Wing-to-wing fuel transfer.
D. Wing-to-fuselage transfer.
3. A white “L or R FUEL BAY LOW” CAS
message indicates the corresponding col-
lector tank is:
A. Empty.
B. Less than 20% full.
C. Less than 50% full.
D. 80% or less full.
4. Emergency fuel operation includes usage
of AVGAS, but not to exceed 500 gal-
lons per
hours of operation.
A. 100
B. 300
C. 500
D. AVGAS is not an approved fuel.
5. A FUEL IMBALANCE caution message
will display on the EICAS whenever:
A. The flaps are down and the quantity
difference between wing tanks is more
than 200 pounds.
B. The flaps are up and the quantity dif-
ference between wing tanks is more
than 350 pounds.
C. Any time the difference is greater than
200 pounds between wing tanks.
D. Both a. and b. are correct.
6. When operating with dual generator fail-
ure, wing-to-wing transfer of fuel:
A. Is not possible, as the XFLOW valve
will not open.
B. Will occur at a much slower rate if the
XFLOW valve is opened.
C. Is not possible, as the standby pumps
will not operate.
D. May be accomplished as in normal
conditions.
7. In flight, fuselage fuel is transfered to
the wings with:
A. Fuselage boost pumps.
B. Gravity.
C. Standby pumps.
D. Gravity or jet pumps located in the
fuselage transfer lines.
8. If both of the inboard display units fail in-
flight, fuel flow and fuel quantity can be
displayed on the:
A. RMUs.
B. Pilot’s multifunctional display.
C. Clearance delivery radio display.
D. Copilot’s primary flight display.
REVIEW QUESTIONS
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