
777 Tech Paper 12B, 13, 14
Authored by Maxus Maxis
Other
Professional Development
Used 1+ times

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48 questions
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1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The aircraft is on the ground and only one power source is available. Both Centre fuel pumps are selected to ON and fuel is available in the Centre tank but PRESS illuminates in one pump switch. Why?
On the ground, system logic allows only one pump at a time to operate.
The pump has failed and due to system logic the OFF light is inhibited.
Automatic load shedding takes place on the ground with only one power source and as a consequence one pump is OFF.
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What mode is the jettison system operating in with the FUEL-TO-REMAIN knob pulled?
Automatic Mode
Manual Mode
MLW Mode
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
When the airplane is heavy and loaded near the forward CG, fuel is jettisoned
From the wings and centre tanks simultaneously
From the wing tanks first
From the centre tank first
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The jettison system can jettison fuel up to:
Up to 5200 kg of fuel in each wing and centre tank.
Up to 5200 kg of fuel in each main tank.
Up to 5200 kg of fuel minimum.
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What does the primary L ENG hydraulic pump FAULT light indicate?
Engine EGT is high or engine speed is low
The left Engine Primary fuel pump is inoperative
Hydraulic Pump pressure is low or temperature is high
The Left Engine is faulty
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What does the Demand L ELEC hydraulic pump FAULT light indicate?
Hydraulic Pump pressure is low or hydraulic pump temperature is high
The left Engine Primary fuel pump is inoperative
Automatic systems using the Left System are faulty
The Autobrake System is faulty
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
How many hydraulic systems are needed to power enough of the flight Controls for safe flight?
One system
Two systems
Three systems
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