191-200 Flashcards

(10 cards)

1
Q

Can the Forward Thrust Lever be advanced if the reverse thrust lever is in the deployed position?
a)
Yes
b)
No

A

NO

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2
Q

Engine start in ambient temperatures below -35°C requires an idle engine _____ minute(s) before changing thrust lever position.
a)
1
b)
2
c)
3

A

2

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3
Q

On the B737-800, moving the APU switch to the OFF position trips the APU generator, closes the APU bleed air valve and extinguished the APU GEN OFF BUS light. Shutdown occurs:
a)
immediately
b)
after a 10 second delay
c)
automatically after a 60 second delay

A

automatically after a 60 second delay

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4
Q

To extend the service life of the APU on the NG, operate the APU for ________ before using it as a bleed air source.
a)
30 seconds
b)
one minute
c)
120 seconds

A

one minute

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5
Q

On the B737-800, can the APU be operated with the blue Maintenance (MAINT) light illuminated?
a)
Yes
b)
No
c)
No, unless the aircraft is at a maintenance station

A

YES

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6
Q

Secondary Engine Indications are displayed on the:
a)
Lower Display Unit
b)
Upper Display Unit
c)
FMC

A

Lower Display Unit

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7
Q

On the Engine Display Control Panel, pushing the MFD Engine (ENG) switch:
a)
displays primary engine indications on the lower DU
b)
displays secondary engine indications on lower DU
c)
displays hydraulic system indications

A

displays secondary engine indications on lower DU

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8
Q

The Fuel Flow Readout on the upper display unit displays fuel flow to engine with the FUEL FLOW switch in the RATE position:
a)
in pounds per hour X 1000
b)
in gallons per hour X 100
c)
kilograms per hour X 100

A

in pounds per hour X 1000

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9
Q

An illuminated APU Fire Warning Switch, in the down position, indicates a fire in the APU, and:
a)
unlocks the APU fire warning switch
b)
arms the APU squib
c)
all answers are correct

A

unlocks the APU fire warning switch

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10
Q

With the OVHT DET switch in normal, what does an illuminated amber FAULT light on the overheat fire protection panel indicate?
a)
The wheel well fire detection system has failed
b)
Both detector loops for an engine have failed
c)
One detector loop for an engine has failed

A

Both detector loops for an engine have failed

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