241-250

Question 1

Why are there mechanical Flap Gates positioned at 1 and 15?
a)
for single engine and normal go-around
b)
for takeoff flap settings
c)
for standardization among fleets

Answer 1

for single engine and normal go-around

Question 2

Where would a TE flaps asymmetry or skew indication be seen?
a)
The Flap Position Indicator
b)
The Aft Overhead Panel
c)
all answers are correct

Answer 2

The Flap Position Indicator

Question 3

Leading edge devices _______ be retracted by the standby hydraulic system.
a)
can
b)
cannot

Answer 3

cannot

Question 4

On the Leading Edge Devices (LE DEVICES) Annunciator Panel, located on the aft overhead panel, an extinguished LE light indicates:
a)
the related LE device is retracted
b)
the related LE device is extended
c)
the related LE device has been manually extended

Answer 4

the related LE device is retracted

Question 5

On the Leading Edge Devices (LE DEVICES) Annunciator Panel, located on the aft overhead panel, pressing the Leading Edge Annunciator Panel TEST switch:
a)
tests the FSEU
b)
tests all trailing edge flap positions
c)
tests all annunciator panel lights

Answer 5

tests all annunciator panel lights

Question 6

An illuminated green Leading Edge Devices Extended (LE FLAPS EXT) Light indicates:
a)
all leading edge devices are retracted
b)
all leading flaps are extended
c)
all trailing edge devices are retracted

Answer 6

all leading flaps are extended

Question 7

An illuminated amber YAW DAMPER Light indicates:
a)
the yaw damper is being operated by the standby hydraulic system
b)
the yaw damper is not engaged
c)
the yaw damper switch needs to be positioned to OFF

Answer 7

the yaw damper is not engaged

Question 8

An illuminated amber Speed Trim Failure (SPEED TRIM FAIL) Light indicates:
a)
a failure of the speed trim system
b)
a failure of the mach trim system
c)
a failure of the autopilot

Answer 8

a failure of the speed trim system

Question 9

On the Integrated Standby Flight Display (ISFD), airspeed and altitude are computed from the pneumatic pressure data provided by direct connections to the:
a)
auxiliary pitot and alternate static ports
b)
Captain’s pitot and static ports
c)
First Officer’s pitot and static ports

Answer 9

auxiliary pitot and alternate static ports

Question 10

On the PFD Airspeed Indicator, the bottom of the Maximum Speed (red and black) bar indicates the maximum speed as limited by:
a)
Landing Gear or Flap Placard speed
b)
VMO/MMO
c)
All answers are correct

Answer 10

All answers are correct