Fuel System

Question 1

Single Point Pressure Refueling pressure is ( ) to ( ) psi, or ( ) to ( ) psi (for aircraft modified by SB 45-28-2).

Answer 1

(20 to 40) or (20 to 55). PTM Pg. 5-23

Question 2

During the SPPR refueling pre-check, the fuel flow from the fuel truck must shut off within ( ) seconds.

Answer 2

20 seconds. PTM Pg. 5-24

Question 3

Once the engines are running, the Lear 45 fuel system can operate on ( ) and suction feed.

Answer 3

Gravity. PTM Pg. 5-16

Question 4

Fuel can gravity feed between the wing tanks with the ( ) open.

Answer 4

Crossflow valve open. PTM Pg. 5-12

Question 5

The amber ( ) CAS message displays when the wing tanks have greater than a 200 lb. difference.

Answer 5

FUEL IMBALANCE. PTM Pg. 5-17

Question 6

To correct a right wing heavy fuel imbalance, the pilot should open the cross flow valve and turn on the ( ) standby fuel pump.

Answer 6

Right. PTM Pg. 5-12

Question 7

Prior to gravity refueling, if the wing tanks are not full, the pilot should drain the:

Answer 7

Vent expansion lines. PTM Pg. 5-26

Question 8

The Fuel Used value on the Fuel pages of the EICAS does not include fuel used by the ( ).

Answer 8

APU. PTM Pg. 6-6

Question 9

The FMS fuel quantity does not register fuel used by the ( ).

Answer 9

APU. PTM Pg. 16-91

Question 10

The Lear 45 holds approximately ( ) lbs. of fuel.

Answer 10

6,060 lbs. of fuel. PTM Pg. 5-2

Question 11

The Lear 40 (unmodified) holds approximately ( ) lbs. of fuel.

Answer 11

5,375 lbs. of fuel. PTM Pg. 5-2