Trans GK Fuels Flashcards
What temperature range is the fuel system designed for?
Between -40C - 50C
During normal operation, fuel feed to each engine is provided by:
The primary jet pump
Motive flow for the primary jet pump is supplied by:
The engine-driven fuel pump through the motive flow valve
The boost pump is used during:
Engine starting
Fuel crossfeed
Wing tank to feed tank fuel transfer
As a backup for the primary jet pump
Does the boost pump energize automatically during engine start and automatically stop after the engine is started?
Yuh (on Gawd)
If a fuel filter becomes clogged, what happens?
A filter pressure switch actuates and the filter is bypassed (L F FLTR BYPASS and/or R F FLTR BYPASS annunciator illuminates )
When does the filter bypass valve open, supplying fuel to the engine? (Fuel is unfiltered)
When the pressure differential exceeds 2.3 psi
In the automatic mode, the boost pump will operate when:
Fuel feed line pressure drops below 5 PSI
Fuel feed chamber volume falls below approximately 11 gallons
Engine starting is selected
Crossfeed is selected
The fuel system has 4 electric pumps, what are they?
2 boost pumps
2 transfer pumps
One electric boost pump is located where?
In each fuel feed chamber
Transfer pumps are used to transfer fuel where?
2 transfer pumps are used to transfer fuel from the mid fuselage tanks into the wing tanks
When does the fuel transfer pump automatically shut off (when in AUTO position)
When the fuel level within the tank reaches a level slightly above empty and the line pressure drops to 5.0 +/-0.5 PSI
What do you do if the fuel transfer pump operation light remains illuminated with either L or R XFER PRESS LO annunciator illuminated, and the switch is in AUTO?
Pull the LH or RH TRANS PUMP C/B to avoid fuel transfer pump damage
What is a jet pump?
A low pressure device that transfers energy from a high velocity, low mass, fluid stream to induce a low velocity, high mass fluid stream (motive flow)
Transfer jet pumps are used to:
Maintain fuel quantity in each fuel feed chamber (one installed on the aft and forward side of the fuel feed chamber; 2 each wing)