756 Systems Flight Controls
Aviation Systems Flight Controls Quiz
Test your knowledge on the flight control systems of the Boeing 757 and 767! This quiz covers various aspects of the aircraft's operational procedures and systems.
- Multiple-choice questions
- Detailed scenarios related to flight controls
- Assess your understanding of standard operational protocols
1) 767: The AIL LOCK light is illuminated. If this light were to illuminate during low speed flight, what would be the status of the inboard/outboard ailerons?
A) One or more ailerons failed to lock
B) The inboard ailerons failed to lock
C) One or more ailerons failed to unlock
D) The inboard ailerons failed to unlock
2) 757/767: The stabilizer is controlled automatically by the autopilot or the Mach speed trim system. When either the autopilot or mach speed trim system is trimming, can the STAB TRIM light illuminate?
A) No, the light is inhibited when autopilot or Mach/speed system is engaged
B) Yes, the light can illuminate when the Mach/speed system is using both trim modules
C) Yes, the light can illuminate during all trimming conditions
D) Yes, the light can illuminate when the autopilot is using both trim modules
3) 757/767: When the SPOILERS light is illuminated, it indicates:
A) Spoilers may not extend upon landing
B) Spoilers may extend at any time
C) The speed brake lever is aft of the armed position
D) One or more spoiler system faults detected
4) 757/767: The AUTO SPD BRK light is illuminated with the speed brake lever positioned to ARM. This indicates that:
A) Speed brakes may not extend automatically on landing or rejected takeoff or may extend in flight if additional fault occurs
B) The flaps are in a landing position above 15 feet RA
C) Radio altitude is between 800 feet and 15 feet RA
D) The load alleviation system has been activated
5) 757/767: The speed brake lever is aft of the armed position and radio altitude is between 800 feet and 15 feet RA. The ___________ light will illuminate.
A) SPEED BRAKES
B) SPOILERS
C) AUTO SPD BKS
D) ALT ALERT
6) 757/767: The rudder ratio system varies control authority from the rudder pedals and trim modules based on airspeed. The system is powered by the ______ hydraulic system.
A) Right
B) Left
C) Center
D) Left, center or right
7) 767: Selection of flaps 1 commands the:
A) Slats move to position 1 and the flaps move to the takeoff position
B) Slats move to the takeoff position and the flaps to remain retracted
C) Slats remain in the UP position and the flaps to move to position 1
D) Slats move to the takeoff position and flaps move to position 1
8) 757: Selection of flaps 1 commands the:
A) Slats move to the takeoff position and flaps remain in the UP position
B) Slats remain in the UP position and the flaps to move to position 1
C) Slats move to position 1 and the flaps move to the takeoff position
D) Slats move to takeoff position and flaps extend to 1
9) 757: If the flaps 30 airspeed placard limit is exceeded, the flap load relief system will automatically have the flaps:
A) The flaps automatically retract to position 25 and when airspeed is reduced below the placarded limit, the flaps automatically re-extend to position 30
B) The flaps automatically retract to position 25 and remain there for the landing
C) The flaps automatically retract to position 20. Flaps are re-extended to the selected position when the speed is reduced below the associated limit.
D) The flaps automatically retract to position 15 and when airspeed is reduced below the placarded limit, the flaps automatically re-extend to position 30
10) 767: If the flaps 30 airspeed placard limit is exceeded, the flap load relief system will automatically have the flaps:
A) The flaps automatically retract to position 20. Flaps are re-extended to the selected position when the speed is reduced below the associated limit.
B) The flaps automatically retract to position 25 and when airspeed is reduced, the flaps automatically re-extend
C) The flaps automatically retract to position 25 and remain there for the landing
D) The flaps automatically retract to position 15 and when airspeed is reduced, the flaps automatically re-extend
11) 757/767: The RUDDER RATIO light is illuminated, this indicates:
A) A fault in the rudder ratio system
B) Full authority of the rudder is available as long as the right hydraulic system is powered
C) The center hydraulic system is no longer available to power the rudder ratio
D) The rudder ratio changer is depressurized to a high speed/full authority control mode
12) 757/767: The flap position indicator displays:
A) Left and right flap position
B) Left and right slat position
C) Left and right flap, slat, and spoiler position
D) Left and right flap and slat position
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