A
What is the maximum rotation of the control wheel to the left or right?
a. 14 degrees
b. 30 degrees
c. 57 degrees
d. 87 degrees
d. 87 degrees
The maximum travel of the Left Aileron Trim Tab (up or down) is:
a. 1.5 degrees
b. 5 degrees
c. 6.7 degrees
d. 14 degrees
c. 6.7 degrees
How long does it take (approximately) to achieve full roll trim travel using the aileron trim switches?
a. 15 seconds
b. 30 seconds
c. 60 seconds
d. 8 seconds
b. 30 seconds
The elevator automatic tab will travel approximately what percentage of the associated elevator movement?
a. 25%
b. 50%
c. 75%
d. 100%
b. 50%
The control columns can travel a maximum of how many degrees in the UP direction?
a. 6.75 degrees
b. 11.25 degrees
c. 13 degrees
d. 23 degrees
b. 11.25 degrees
What is the maximum deflection angle of the spoiler panels?
a. 14 degrees
b. 30 degrees
c. 57 degrees
d. 87 degrees
c. 57 degrees
In the event one elevator channel is jammed, what is the required force to disconnect the pitch uncoupling mechanism?
a. 150 N (approx. 15 kg)
b. 230 N (approx. 23 kg)
c. 520 N (approx. 52 kg)
d. 1020 N (approx. 104 kg)
c. 520 N (approx. 52 kg)
The control columns can travel a maximum of how many degrees in the DOWN direction?
a. 6.75 degrees
b. 11.25 degrees
c. 13 degrees
d. 23 degrees
a. 6.75 degrees
The maximum elevator travel in the NOSE UP direction is:
a. 6.75 degrees
b. 11.25 degrees
c. 13 degrees
d. 23 degrees
d. 23 degrees
The maximum elevator travel in the NOSE DOWN direction is:
a. 6.75 degrees
b. 11.25 degrees
c. 13 degrees
d. 23 degrees
c. 13 degrees
What is the maximum deflection of the pitch trim tabs (in the UP direction) while they are being trimmed?
a. 1.5 degrees
b. 5 degrees
c. 6.7 degrees
d. 23 degrees
b. 5 degrees
Spoiler panel deflection begins when the associated aileron deflects upward by what amount?
a. 1 degree
b. 2.5 degrees
c. 5 degrees
d. 14 degrees
b. 2.5 degrees
What is the maximum deflection of the pitch trim tabs (in the DOWN direction) while they are being trimmed?
a. 1.5 degrees
b. 5 degrees
c. 6.7 degrees
d. 23 degrees
a. 1.5 degrees
An AURAL ALERT will sound if the Normal Pitch Trim switches are held down in either direction for more than:
a. Half a second
b. One second
c. Three Seconds
d. Five Seconds
b. One second
Reconnecting the Pitch System after a pitch system disconnect is classified as an operation that requires approximately how long?
a. 30 minutes
b. 1 hour
c. 6 hours
d. 12 hours
c. 6 hours
In the Automatic TLU mode, the rudder travel limitation is activated when the aircraft accelerates through what speed?
a. 150 knots
b. 180 knots
c. 185 knots
d. 250 knots
c. 185 knots
The ATR 72 variants utilize which flap settings?
a. 0, 15, 25, and 35 degrees
b. 0, 15, and 30 degrees
c. 0, 15, 20, and 25 degrees
d. 0, 10, 20, and 30 degrees
b. 0, 15, and 30 degrees
The MFC will stop the flaps if the position difference between the left and right inboard flaps exceeds what limit?
a. 3.0 degrees
b. 5.0 degrees
c. 6.7 degrees
d. 10.0 degrees
c. 6.7 degrees
In the event of an Aileron Locking Actuator disagreement, the MFC triggers a FLT CTL caution with AIL LOCK illuminated after approximately how many seconds?
a. 1 second
b. 3 seconds
c. 8 seconds
d. 15 seconds
c. 8 seconds
Which electrical bus powers the Rudder Trim control system?
a. DC BUS 1
b. DC BUS 2
c. AC BUS 1
d. DC EMER BUS
d. DC EMER BUS
A FLAP UNLK light and warning will illuminate if the extended flaps retract uncommanded by more than what amount?
a. 1 degree
b. 3 degrees
c. 5 degrees
d. 6.7 degrees
What is the difference in degrees between flap command and actual position that results in the Flaps position being displayed in green on the EWD (except at 0°)?
a. Lower than 0.5 degrees
b. Lower than 1 degree
c. Lower than 3 degrees
d. Lower than 6.7 degrees
b. 3 degrees
b. Lower than 1 degree
The MFC (Multi-Function Computer) triggers a FLT CTL caution light along with the AIL LOCK light on the glareshield in the event of what disagreement?
a. Rudder Trim position vs. Yaw Trim Handle position.
b. Elevator position vs. Pitch Trim setting.
c. Aileron Locking Actuator position disagreement.
d. Flap Handle position vs. Actual Flap position.
In the event of a failure in the Stick Pusher or Stick Shaker systems, what is the resulting cockpit indication?
a. PITCH FAIL light.
b. STICK FAIL message on the EWD
c. The FAULT light illuminates on the stick shaker/pusher pushbutton.
d. A continuous horn sounds.
c. Aileron Locking Actuator position disagreement.
c. The FAULT light illuminates on the stick shaker/pusher pushbutton.
What is the main visual indication used by the pilots to monitor the flap position?
a. The Flap Control Handle position only.
b. The Flap Position Indication on the EWD.
c. The hydraulic pressure gauge.
d. The Flap Actuator FAULT light.
If the TLU FAULT light illuminates, how is the rudder travel limit manually adjusted?
a. By rotating the Yaw Trim Handle.
b. By moving the TLU switch to the HI SPD or LO SPD position.
c. By cycling the blue hydraulic system.
d. By engaging the Gust Lock.
b. The Flap Position Indication on the EWD.
b. By moving the TLU switch to the HI SPD or LO SPD position.
The Rudder Travel Limitation is removed when the aircraft slows below what speed?
a. 150 knots
b. 180 knots
c. 185 knots
d. 250 knots
Full Rudder Trim travel takes approximately how long?
a. 8 seconds
b. 15 seconds
c. 30 seconds
d. 60 seconds
b. 180 knots
b. 15 seconds
How long does it take (approximately) for full pitch trim travel using either the Normal or Standby systems?
a. 8 seconds
b. 15 seconds
c. 30 seconds
d. 60 seconds
The green band on the Pitch Trim Indicator, representing the normal pitch trim position for takeoff, ranges from 0 degrees up to:
a. 1.5 degrees
b. 2.5 degrees
c. 5 degrees
d. 6.7 degrees
c. 30 seconds
b. 2.5 degrees