Flight Controls

Question 1

757/767: The three modes of stabilizer trim control are:

Answer 1

Electric (control wheel) alternate (control stand) automatic (autopilot)

Question 2

757/767: If pilots inadvertently activate aileron trim while an autopilot is engaged, the repositioning of the aileron neutral point:

Answer 2

Is not apparent until the autopilot is disengaged

Question 3

757 Selection of flaps 1 commands the

Answer 3

Slats to move to takeoff position and flaps extend to 1

Question 4

757/767 the UNSCHEDULED STAB TRIM light illuminates when

Answer 4

Stab trim movement without signal from trim switches

Question 5

When spoilers light is illuminated it indicates

Answer 5

One or more spoiler system faults detected

Question 6

767 AIL LOCK is illuminated. If this were to illuminate during low speed flight what would be the status of ailerons

Answer 6

One or more of the ailerons failed to unlock

Question 7

757/767: With the speed brake lever in the ARMED position, the ground spoilers automatically extend upon landing and the handle moves to the UP positions when three conditions are met, including:

Answer 7

Both truck tilt sensors detect a no-tilt condition on the ground

Question 8

757/767: The AUTO SPD BRK light is illuminated with the speed brake lever positioned to ARM.
indicates that:

Answer 8

Speed brakes may not extend automatically on landing or rejected takeoff or may extend in flight if additional fault occurs

Question 9

757/767: The RUDDER RATIO light is illuminated, this indicates:

Answer 9

A fault in the rudder ratio system

Question 10

The __ trim switches are inhibited if multiple autopilots are engaged in the approach mode

Answer 10

Electric

Question 11

The flap position indicator displays

Answer 11

Left and right flap and slat position

Question 12

767: The Pitch Enhancement System (PES) provides a backup source of hydraulic power to operate the horizontal stabilizer if both the left and center hydraulic systems fail. When the PES operates, trim is only available from the:

Answer 12

Control wheel trim switches

Question 13

757: It during the Before Takeoff Procedure, the stabilizer trim setting shown on FMC TAKEOFF REF page 1 is less than 3.0, what should be done?

Answer 13

Use the ALTN STAB TRIM switches

Question 14

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.

Answer 14

Left

Question 15

757: If the flaps 30 airspeed placard limit is exceeded, the flap load relief system will automatically have the flaps:

Answer 15

The flaps automatically retract to position 25 and when airspeed is reduced below the placarded limit, the flaps automatically re-extend to position 30

Question 16

757/767: If a single autopilot is engaged, ____ trimming causes the autopilot to disengage

Answer 16

Electric

Question 17

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?

Answer 17

No, the light is inhibited when autopilot or Mach/speed system is engaged

Question 18

767 Selection of flaps 1 commands the

Answer 18

Slats to move to takeoff and flaps to remain retracted

Question 19

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.

Answer 19

Speed brakes

Question 20

767: If the flaps 30 airspeed placard limit is exceeded, the flap load relief system will automatically have the flaps:

Answer 20

The flaps automatically retract to position 20. Flaps are re-extended to the selected position when the speed is reduced below the associated limit.

Question 21

757: When the TRAILING EDGE light illuminates, hydraulic power is removed from the drive unit(s) of

Answer 21

Slats and flaps

Question 22

767: In conjunction with trailing edge flap position 5 (or greater), which of the following will droop by being hydraulically driven to 50% down?

Answer 22

Inboard ailerons