Fuel

Question 1

Total Usable Fuel Quantity

Answer 1

384 gallons (2573 lbs)

Question 2

Total Usable Fuel Quantity - EACH SIDE

Answer 2

192 gallons (1286.5 lbs)

Question 3

Total Usable Fuel Quantity - EACH WING TANK SYSTEM

Answer 3

131 gallons (877.5 lbs)

Question 4

Total Usable Fuel Quantity - EACH NACELLE TANK

Answer 4

61 gallons (409 lbs)

Question 5

Maximum Allowable Fuel Imbalance

Answer 5

200 lbs

Question 6

There are _______ fuel sumps/drains per side of the aircraft.

Answer 6

Five

Question 7

If a transfer pump fails in flight, reduce the total fuel available for that engine by approximately __________ lb.

Answer 7

188 lb

Question 8

To ensure the transfer of fuel from the center wing tank to the nacelle tank, monitor the nacelle tank quantity for an approximate increase from ________ lb to ________ lb.

Answer 8

330 lb to 400 lb

Question 9

LIMITATIONS ON THE USE OF OF AVGAS
1. Operation is limited to _______ hours between engine overhauls.
2. Operation is limited to _______ feet pressure altitude or below with boost pumps inoperative.
3. Crossfeed capability is required for climbs above _______ feet pressure altitude.

Answer 9

1. 150 hours
2. 8000 feet
3. 8000 feet

Question 10

Do not take off if fuel quantity gages indicate in the _________ arc or if fuel quantity is less than ________ pounds in each wing system.

Answer 10

Yellow
265 pounds

Question 11

Crossfeeding of fuel is permitted only in the event of:

Answer 11

1. Electric boost bump failure, or
2. Engine failure

Question 12

Operation of either engine with its corresponding fuel pressure annunciator (L FUEL PRESS or R FUEL PRESS) illuminated is limited to _____ hours before overhaul or replacement of the engine-driven fuel pump.

Answer 12

10 hours

Question 13

Boost bump limit for takeoff

Answer 13

Both boost pumps must be operational prior to takeoff.