FUEL SYSTEM Flashcards

(36 cards)

1
Q

Parts of fuel system

A

1) Storage

2) Distribution

3) Fuel Indication

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2
Q

Wing tanks

A

2 x INTEGRAL (9496 (4748 per tank))
2 x SURGE
1 x COLLECTOR

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3
Q

How are engines supplied?

A

From integral tanks through collector tanks

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4
Q

Which tank is used by APU?

A

Right tank

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5
Q

How are engines fed?

A

By the means of EJECTIVE PUMP

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6
Q

How is APU fed?

A

By the means of ELECTRICAL PUMPS (AC/DC) when engines are not running

By EJECTORS when engines are running

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7
Q

Role of AC pumps

A

1) Redundancy for case of EJECTOR PUMP failure

2) Fuel pressure for engine&APU start on the ground

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8
Q

2 types of refueling

A

1) via refueling adapter (RHW) only pressure refueling

2) 2x gravity refuel ports on the top of the wing

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9
Q

How does the fuel flow inside the tanks?

A

Toward the fuselage into collector tank

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10
Q

Baffle and flapper check valves

A

Baffle and flapper check valves
1) prevent fuel from escaping of collector tank
2) prevent fuel from entering the surge tank

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11
Q

Purpose of tank vent system

A

To keep differential pressure between tank and ambient air within operational limits

To prevent fuel spillage during maneuvers and hard breaking

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12
Q

How is fuel drain provided?

A

Each tank has its own independent line into a surge tank

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13
Q

Where is water drain valves are located?

A

1) Next to AC auxiliary fuel pump (on the bottom of collector tank)

2) Close to the wing stub to wing junction

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14
Q

Fuel quantity measurement system consists of

A

1) 13 x ELECTRICAL FUEL QUALITY (PROBES)

2) 3 x MECHANICAL FUEL QUANTITY (MAGNETIC LEVEL INDICATOR)

3) Fuel temperature

4) Low level indication (independent probe (not one of the fuel indication probe)

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15
Q

Type of fuel measurement probes

A

AC capacitance-type

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16
Q

Which system of measurement is backup

A

Mechanical (floater)

17
Q

When fuel temperature is indicated in amber

18
Q

How pump failure is indicated

A

By amber dashes

19
Q

Where is temperature sensor installed?

A

In the left tank only

20
Q

When LOW LEVEL warning is indicated?

A

If fuel quantity is below 300 kg

21
Q

Where are magnetic sensors are mounted

A

3 indicators per wing mounted into fuel tank access panels

22
Q

How to measure fuel quantity with a mechanical indicator

A

Turn it out, pull, take the value from the scale and determine the quantity with the chart from operation manual

23
Q

Parts of fuel distribution system

A

1) Engine feed

2) APU feed

3) Refuel defuel

24
Q

Means of fuel supply to the engines

A

1) Ejectors

2) AC pumps

25
Crossfeed function
Allows fuel supply to both engines from either of fuel tanks
26
Source of fuel supply to APU
Right tank by DC pump
27
Which pump is used for fuel supply to start the engine on the ground (in flight)
DC pump is used for engine start when AC power or AC fuel pump is unavailable
28
Mean of initial fuel supply during start
When APU is working — AC pump After start — ejector
29
Low fuel pressure in engine detected
Ejector — OFF AC PUMP (if in AUTO) — automatically starting
30
Mean of initial fuel supply: NO AC GPU, NO APU
DC pump
31
EICAS: FUEL IMBALANCE
360 kg Disappear — 45 kg “FUEL EQUAL — XFEED OPEN”
32
Priority of AC PUMP selector
AC PUMP selector command overrides XFEED selector command
33
XFEED operation limitations
Prohibit during takeoff and landing
34
APU fuel supply
1) Initial supply — DC PUMP 2) AC power available — AC PUMP 3) Engine is running — EJECTOR
35
How to provide APU fuel supply from the left tank?
Set LOW 2
36
When there may appear FUEL LO LEVEL indication, if fuel quantity is adequate?
In case of scavenge pumps failure, fuel flows out from the collector tank and Fuel Low Level sensor triggers