POH 4.8 Fuel System Flashcards

1
Q

POH.4.8.1 Fuel Tanks

A
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2
Q

Where is fuel stored?

A

Fuel is stored in fuel tanks located in each wing.

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3
Q

How are tanks interconnected in each wing?

A

The tanks in each wing are interconnected to function as a single tank.

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4
Q

How are tanks filled?

A

All tanks on each side are filled through a single filler in the outboard tank, and as fuel is consumed from the inboard tank, it is replenished by fuel from outboard.

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5
Q

What’s the unusable fuel?

A

2.5 Gallons

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6
Q

How much is it usable?

A

93 gallons with standard fuel tanks

123 gallons with the optional fuel tanks installed

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7
Q

What’s the minimum fuel grade?

A

100 or 100LL Aviation Grade

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8
Q

What about Flyschool’s tanks?

A

FlySchool have optional tanks installed. The usable fuel is 123 gallons.

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9
Q

What are the fuel tank vents?

A

one installed under each wing, feature an anti-icing design to prevent ice formation from blocking the fuel tank vent lines

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10
Q

POH.4.8.2 Fuel Injection System

A
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11
Q

What type of fuel injection does the Seneca II use?

A

Continuous flow type that utilizes a vapor return line leading back to the fuel tanks.

This line provides a route back to the tanks for vapor laden fuel that has been separated in the injector pump swirl chamber.

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12
Q

How many pumps does each engine have?

A

Each engine has an engine-driven fuel pump that is a part of the fuel injection system.

An auxiliary fuel system is provided. The purpose of the electrically powered auxiliary fuel system is to supply fuel to the engine in case of engine-driven fuel pump shaft failure or malfunction, for ground and inflight engine starting, and for vapor suppression.

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13
Q

Where are the two auxiliary fuel pump switches located?

A

The two auxiliary fuel pump switches are located on the lower left side of the instrument panel and are three-position rocker switches: LO, HI and OFF.

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14
Q

What happens when the HI auxiliary fuel pump is activated?

A

When the HI auxiliary fuel pump is activated, an amber light in the annunciation panel is illuminated for each pump. These lights dim whenever the pump pressure reduces automatically, and manifold pressure is below approximately 21 inches.

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15
Q

POH.4.8.3 Electric Primer System

A
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16
Q

What does the primer switch do?

A

Separate spring loaded OFF primer button switches, located adjacent to the starter switches, are used to select HI auxiliary fuel pump operation for priming, regardless of other switch positions. These primer buttons may be used for both hot or cold engine starts.

17
Q

POH.4.8.4 Fuel Drains

A
18
Q

Why are fuel drains carried out and when?

A

Before each flight, fuel must be drained from low points in the fuel System to ensure that any accumulation of moisture or sediment is removed from the system and to check for proper fuel. Fuel drains are provided for each fuel filter (2). each fuel tank (4), and each crossfeed line (2).

19
Q

POH.4.8.5 Fuel Controls

A
20
Q

Where are fuel controls located?

A

Fuel management controls are located on the console between the front seats.

21
Q

How do the fuel controls work?

A

There is a control lever for each of the engines, and each is placarded ON - OFF - X FEED. During normal operation, the levers are in the ON position, and each engine draws fuel from the tanks on the same side as the engine. The two fuel systems are interconnected by crossfeed lines. When the X FEED position is selected, the engine will draw fuel from the tanks on the opposite side in order to extend range and keep fuel weight balanced during single-engine operation. The OFF position shuts off the fuel flow to that engine.

22
Q

What must you note about the fuel control when one engine is inoperative?

A

When one engine is inoperative and the fuel selector for the operating engine is on X FEED, the selector for the inoperative engine must be in the OFF position.

23
Q

What musn’t you do?

A

Do not operate with both selectors on X FEED. Do not take off with a selector on X FEED. Fuel and vapor are always returned to the tank on the same side as the operating engine