Fuel Sys

Question 1

The APU is supplied by what tank?

Answer 1

2 main

Question 2

FLCVs in tanks 2/3

Answer 2

1

Question 3

What fuel tank does the SPR drain into?

Answer 3

3 main

Question 4

Usable fuel in Ext Tank

Answer 4

8,900lbs

Question 5

How many fuel tanks are in the KC-130J?

Answer 5

6, 4 main tanks and 2 aux tanks.

Question 6

T/O Fuel Managment: Tanks 1/4 should contain _______lbs more than tanks 2/3.

Answer 6

500-1000lbs

Question 7

Symetric tanks should be w/in ________lbs

Answer 7

1,000

Question 8

Transfer pumps are ______ driven

Answer 8

Electricly

Question 9

Undumpable fuel in main tanks.

Answer 9

1,520lbs

Question 10

For takeoff and landing fuel management, the main tanks are full, except for fuel used for taxi, takeoff, and climb, but not less ________ lbs in tanks No. 1 and No. 4, and not less than ________ lbs in tanks No. 2 and No.3 when the EXT tanks contain usable fuel.

Answer 10

7060, 6407lbs

Question 11

How are Boost Pumps energized?

Answer 11

ENGINE START sw to Run

Question 12

Number of FLCVs in each external tank

Answer 12

1

Question 13

Low Fuel

Answer 13

Projected Landing with less than 6,000lbs of fuel

Question 14

Transfer Pumps in each Tank

Answer 14

1

Question 15

PSI of Fuel Boost Pumps

Answer 15

15-24psi

Question 16

PSI of Fuel Transfer Pumps

Answer 16

28-40psi

Question 17

Undumpable fuel in Aux and Ext tanks

Answer 17

0 lbs

Question 18

Transfer pumps in ea Aux tank?

Answer 18

1

Question 19

Transfer pumps in each main fuel tank

Answer 19

1

Question 20

What is required for the Water removal system to work?

Answer 20

Boost Pump

Question 21

For a 540 sink rate, Ext shoud be ______, not to Exceed_____lbs.

Answer 21

Empty, 500lbs

Question 22

The APU requires _____ lbs of fuel to Start and Run

Answer 22

2000lbs