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Pooja Gupta
June 29, 2020
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Boeing 737 - Hydraulic System Exam MCQ

1
The engine driven hydraulic pump switch
2
The Standby hydraulic fluid
3
The standby system low quantity light is
4
Using the Standby Hydraulic power for thrust reverser deployment will cause
5
The 'B' system reservoir has
6
A leak in the hydraulic system A engine driven pump or its associated lines would be indicated by
7
The standby hydraulic pump is automatically activated on the loss of system A or B hydraulic pressure
8
Loss of the B hydraulic system will result in the complete loss of the following
9
Loss of the A hydraulic system will result in the complete loss of the following
10
The maximum hydraulic system A or B pressure is
11
Illumination of a electric hydraulic pump OVERHEAT light will
12
Illumination of a Hydraulic Electric Pump OVERHEAT light indicates
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Hydraulic system A power sources are
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The Standby hydraulic reservoir is kept topped up from
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The normal and maximum readings on the hydraulic system pressure indicator are
16
Selecting an engine driven hydraulic pump switch to OFF will
17
The A and B hydraulic reservoirs are pressurised by
18
If a total failure of both pumps supplying system B pressure occurs, which of the primary flight controls will be totally inoperative
19
Low fluid quantity in the A system reservoir can be indicated by one of the following
20
The standby hydraulic pump only supplies pressure to the
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The standby system LOW PRESSURE light is armed
22
A leak in the hydraulic system B engine driven pump or its associated lines would be indicated by
23
If an electric hydraulic pump OVERHEAT light comes on
24
Complete loss of system 'B' pressure will deactivate
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