Fuel Sys Flashcards

1
Q

The APU is supplied by what tank?

A

2 main

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2
Q

FLCVs in tanks 2/3

A

1

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3
Q

What fuel tank does the SPR drain into?

A

3 main

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4
Q

Usable fuel in Ext Tank

A

8,900lbs

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5
Q

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

A

6, 4 main tanks and 2 aux tanks.

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6
Q

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

A

500-1000lbs

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7
Q

Symetric tanks should be w/in ________lbs

A

1,000

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8
Q

Transfer pumps are ______ driven

A

Electricly

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9
Q

Undumpable fuel in main tanks.

A

1,520lbs

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10
Q

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.

A

7060, 6407lbs

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11
Q

How are Boost Pumps energized?

A

ENGINE START sw to Run

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12
Q

Number of FLCVs in each external tank

A

1

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13
Q

Low Fuel

A

Projected Landing with less than 6,000lbs of fuel

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14
Q

Transfer Pumps in each Tank

A

1

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15
Q

PSI of Fuel Boost Pumps

A

15-24psi

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16
Q

PSI of Fuel Transfer Pumps

A

28-40psi

17
Q

Undumpable fuel in Aux and Ext tanks

A

0 lbs

18
Q

Transfer pumps in ea Aux tank?

A

1

19
Q

Transfer pumps in each main fuel tank

A

1

20
Q

What is required for the Water removal system to work?

A

Boost Pump

21
Q

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

A

Empty, 500lbs

22
Q

The APU requires _____ lbs of fuel to Start and Run

A

2000lbs