Flight Controls

Question 1

An illuminated FEEL DIFF PRESS light indicates
A the elevator trim system is in operative
B an emergency situation exist due to the complete hydraulic failure
C excessive differential hydraulic pressure is sensed in the elevator feel computer

Answer 1

C excessive differential hydraulic pressure is sensed in the elevator feel Computer

Question 2

Engagement and disengagement of the Mach trim system
A is accomplished automatically as a function of the pressure altitude
B is accomplished automatically as a function of airspeed
C is accomplished manually by use of the trim cut out switch

Answer 2

B is accomplished automatically as a function of airspeed

Question 3

The stabilizer trim MAIN ELECT and a AUTOPILOT cut out switches are provided to allow the main electrical or auto pilot trim inputs to be
A disconnected from the respective stabilizer trim motor
B disconnected from the single stabilizer trim motor
C over written by the opposite stabilizer trim motor

Answer 3

B disconnected from the single stabilizer trim motor

Question 4

Switching these STAB TRIM override switch to OVERIDE
A deactivates the main STAB TRIM system
B deactivates the auto pilot STAB TRIM system
C electric trim can be used regardless of control composition

Answer 4

C electric trim can be used, regardless of control, position

Question 5

The Rudder trim control switch electrically repositions the
A Rudder pedals
B Rudder feel and centering unit
C Rudder trim tabs

Answer 5

B Rudder feel and centering unit

Question 6

The 737 flap lever
A selects the position of the LE devices by determining the TE flat position
B at flat positions, 30 and 40 arms, the flap load relief system
C all answers are correct

Answer 6

C all answers are correct

Question 7

Why are there mechanical flap gates positioned at the flap 1 and flap 15 detect?
A for single engine and normal go around
B for takeoff flat setting
C for standardization across fats

Answer 7

A for single engine and normal go around

Question 8

Where would the TE flap asymmetry air or skew indication issue be seen
A the LE DEVICES indicator on the act overhead panel
B the flap position indicator
C all answers are correct

Answer 8

B the flap position indicator

Question 9

On the LE DEVICES annunciator panel and extinguished LE light indicates
A the related LE device is extended
B the related LE device is retracted
C the LE device is not responding

Answer 9

B the LE device is retracted

Question 10

Rotating the Rudder trim control job
A pneumatically trims the rudder
B electrically trims the rudder
C hydraulically trims the Rudder

Answer 10

B electrically trims the rudder