Fuel (28) Flashcards

1
Q

How many fuel tanks are there?

A

2

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2
Q

At what level is the interconnection between the 2 tanks?

A

160kg

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3
Q

What draws fuel intro the engines?

A

The engine driven fuel pumps

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4
Q

How are the fuel ventilation systems protected from flame propagation?

A

Via flame arrestors

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5
Q

How many probes are in each fuel system and where does it send data?

A

2
AMMC

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6
Q

Is there an independent low level sensor?

A

YES
optical sensor switch

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7
Q

What is the fuel capacity?

A

888Kg
(useable)

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8
Q

How much unusable fuel is there

A

8kg

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9
Q

At what level is the interconnect or and what is its purpose?

A

160kg total
To concentrate the fuel around the inlet

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10
Q

How much of the suction feed screen can be blocked when operating at Max Op Alt?

A

50%

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11
Q

How are the Fuel ShutOff valves controlled?
(2)

A

EDCU
When Fire suppression ARMED

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12
Q

What is the purpose of the fuel Snorkel?

A

Minimised fuel spillage in the event of an aircraft rollover

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13
Q

How long and what temp can the flame arrest or protect the fuel tank for?

A

800°C for 5 mins

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14
Q

When is [1(2) FUEL LOW] triggered?

A

51kg
(10 mins)

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15
Q

What does [PMS NOT OFF] signify on the EDCU Fuel page?

A

Pilot tries to close the SOV with the engine Power Management Switch (PMS) for the relevant engine in the FLIGHT or IDLE position?

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16
Q

What does [ENG 1(2) FIRE ARM] posted in the EDCU Fuel page signify?

A

Fire system ARMED

17
Q

What does [SOV DISCREPANCY] signify in the EDCU Fuel Page?

A

When the reported position of the valve does not match the commanded position of the valve

18
Q

What does [CMD NOT EXECUTED] power in the fuel management page signify?

A

The AMMC does not acknowledge the EDCU command to open or close a SOV

19
Q

What 3 conditions are needed for operation of a sample/drain valve?

A
  • ENgine SOV closed
  • WOW
  • Sample valve switch operation
20
Q

On power-up what position are the SOVs in?

A

The last known position

21
Q

What happens to the fuel quantity display on the PFD when both tanks are below 51kg?

A

Display changes to amber

22
Q

What does three amber dashes signify on the Fuel Quantity indicator on the PFD?

A

Loss of probe data.

23
Q

Under OEI, how is the fuel in the failed engine displayed?

A

Greyed out 160kg

24
Q

Are there any airframe mounted fuel filters?

A

No - The one at the suction valve is only a screen
The fuel is filtered at the engine only

25
Can you identify a failed fuel probe?
Yes - via Fuel Synopitc Page
26
How is the aircraft refuelled?
Gravity LHS of Aircraft
27
When at 160kg (collector cell level), how much flight time is available?
50 minutes AEO 35 minutes OEI
28
In level flight and when the fuel quantity equals the unusable fuel quantity, what will the fuel quantity read?
000
29
What kind of sensor is the Low Level Sensor?
Optic Based
30
Where is the Fuel Control Unit located?
On the Reduction Gearbox