Fuel System Flashcards

1
Q

Fuel Compacity

A

Total: 103 gal (51.5 per tank)
Usable 100 gal (50 per tank)

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2
Q

Slip limitation

A

No more than 30 seconds

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3
Q

Does the fuel system include crossfeeds or fuel transfer?

A

Only crossfeeds

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4
Q

How is fuel drawn?

A

Respective tanks -> Fuel Strainer -> Fuel Selector -> Check Valve -> -> Aux Fuel Pump -> Engine Driven Fuel Pump -> Carburetor -> Engine

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5
Q

What does the fuel tab in the tanks indicate?

A

Top of Tab: 51.5 gal (50 usable) - Full Tanks
Center Mark: 40 gal (38.5 usable) remaining
Bottom of Tab: 30 gal (28.5 usable) remaining

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6
Q

How many fuel drains are there?

A

8 - four on each wing. Also drains on the underside of each nacelle, on the fuel selectors and flush drains for crossfeed lines

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7
Q

Type of fuel sensors

A

Float sensors

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8
Q

Can the aux fuel pumps run the engine if the primaries fail?

A

Yes

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9
Q

Why is fuel required for cabin heating?

A

The cabin heating element is housed in the nose cone of the aircraft. Uses fuel from the RIGHT tank only. Includes a heater and heater fuel pumps.

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10
Q

What is fuel crossfeed used for?

A

Emergencies only

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11
Q

Before takeoff fuel requirement?

A

9 gallons minimum in each wing tank before takeoff

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12
Q

How much fuel does the cabin heater use?

A

2/3 gallons/hr

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13
Q

What is the output of the cabin heater?

A

45,000 Btu-per-hour

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14
Q

How does the cabin heater work?

A

A gas-powered heater in the nose cone heats fresh air from outside, routes it into the cabin and windshield defroster, then sends excess to outlets further back of the aircraft

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15
Q

Is there overheating protection for the heater?

A

Yes, the manual reset limit switch (inaccessible during flight) shuts off the heat system in case the discharge temperature reaches 300F

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16
Q
A