Fuel System Flashcards

(25 cards)

1
Q

Pressure refuel quantity?

A

14,150 lbs

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2
Q

Gravity/overwing refuel quantity?

A

13,000 lbs

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3
Q

Fuel tanks are divided into how many sections?

A

3 sections - main tank, collector tank, and surge tank

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4
Q

What ways are there to laterally transfer fuel between wing tanks?

A

Transfer(XFER) – via DC boost pumps

Gravity XFlow

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5
Q

How do you transfer fuel from the left wing to the right wing?

A
  1. Left DC boost pump on

2. xfer open

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6
Q

How do you transfer fuel from the left to right on the ground with engines off and APU running?

A
  1. Left DC pump on
  2. xfer open
  3. Rt. pump off.

(Not documented as an approved procedure by Bombardier)

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7
Q

How is the fuel heated?

A

Fuel / Oil Heat Exchanger

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8
Q

Do you need battery power to fuel the aircraft?

A

Yes.

Fuel / Defuel SOV are powered by the Rt. Battery bus.

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9
Q

Is mixing of fuel types approved?

A

Yes

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10
Q

What part of the fuel tank supplies fuel to the engines?

A

Collector Tank

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11
Q

What is the function of the surge tank at the tip of the fuel tanks?

A

To provide additional expansion volume for the vent system

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12
Q

What operates the Main Ejector and Scavenge Ejectors?

A

Motive flow from the engine driven pumps

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13
Q

Minimum wing fuel for go-around?

A

500 lbs per side

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14
Q

Do we need fuel anti-icing additive as long as the minimum oil temperature is achieved?

A

No, Fuel is heated thru the fuel/oil heat exchangers

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15
Q

How many water drains are in the fuel tanks?

A

6

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16
Q

When do we drain the fuel tanks?

A

When contamination is suspected

17
Q

How many fuel pumps are on the CL350/300?

A
9 TOTAL
engine driven pumps(2), 
electric boost pumps(2), 
main ejectors(2), 
scavenge ejectors(2)
APU mechanical pump(1)
18
Q

The powered fuel transfer valve fails to open, what is the backup way of moving fuel between the wing tanks?

A

Gravity transfer

19
Q

In “AUTO” when do the electric fuel pumps come on?

A

Run switch to “RUN” - for engine start

Low fuel pressure indication

Right pump for APU operation when right engine is not running

20
Q

How many fuel quantity probes are there?

21
Q

FUEL QTY LOW CAS occurs when?

A

300 lbs or less in a wing.

22
Q

Single point refuel pressure is limited to?

23
Q

The fuel/oil heat exchanger is where?

24
Q

The Hydraulic/fuel heat exchanger is where?

25
When the fuel temp is approaching 45 to 50 degrees what consideration should be made?
Limitations regarding maximum fuel temp and minimum fuel level in order to cool hydraulic fluid through the hydraulic/fuel heat exchanger.