Fuel System Flashcards

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1
Q

What happens when all the fuel in an auxiliary tank is pumped to the main tank and consumed?

A

AUX pump will automatically turn off and supply CAAS with an advisory for the associated tank

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2
Q

What keeps fuel loss and post-crash fires to a minimum by breaking or shearing at predetermined locations and sealing themselves to retain fuel?

A

Breakaway self sealing fittings

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3
Q

What is installed in each tank to prevent fuel spillage from the vents should the helicopter roll over following a crash landing?

A

Roll-over Vent System

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4
Q

How is an Engine Fuel Valve opened or closed electronically?

A

Fire Pull Handles

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5
Q

If the engines are running, CAAS will activate a FUEL LVL caution at ______pounds in the event the fuel quantity low level warning system has failed (internal fuel tank sensors).

A

<360 lbs for more than 2 seconds

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6
Q

ENG 1/2 FUEL PRESS LO caution(s) activate when fuel pressure in the respective line is below what?

A

10 psi +/- 1 psi

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7
Q

The fuel flow display on the fuel page of the MFD will flash when fuel flow is equal to or greater than ___________ pounds.

A

2,995 lbs

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8
Q

What is the purpose of the jet pump system within each main fuel tank?

How are they activated?

A

Evacuate fuel from the refuel station manifold

By turning on the main tank(s) boost pumps.

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9
Q

How is the jet pump system activated?

A

By turning on the respective main tank pumps on the overhead sw panel

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10
Q

What two fuel system related switches are monitored by the Cockpit Voice and Flight Data Recorder (CVFDR) for position?

A

X-FEED and Main Fuel Pump sw’s

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11
Q

What should be avoided if both boost pumps should fail in either main fuel tank with the XFEED open and a low fuel indication?

A

Nose low attitude in excess of 5 degrees

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12
Q

What is the max capacity for fuel in the CH47F?

A

6,887.6 lbs

1028 gallons

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