B767 FLIGHT CONTROLS

When are the flight control shut off switches used? (FCOM, 9.10.6). A.- In case of a hydraulic leak inflight. B.- In the event of a flight control failure. C.- Ground use only.

What the lights mean in the Flight (FLT) CONTROL SHUTOFF Switches? (9.10.6). A.- ON – the flight control valve is commanded open. B.- Off (ON not visible) – the flight control valve is commanded open. C.- Off (visible) – the flight control valve is commanded open.

Which is the correct display on EICAS status when the control column is pushed to the forward stop? (FCOM, 9.10.5). A.- Both elevator position pointers full scale deflection up. B.- Both elevator position pointers full scale deflection down. C.- Both elevator position pointers 3/4 scale deflection down.

The AUTO SPDBRK light illuminates and the EICAS advisory message AUTO SPEEDBRAKE displays to indicate: (FCOM, 9.20.9). A.- A fault is detected in the automatic speed brake system which may result in the loss of automatic speed brake extension. B.- The pilot must be alert. C.- A fault is detected in the automatic speed brake system.

IF the stabilizer moves in a direction opposing autopilot elevator control inputs, Unscheduled Stabilizer Trim (UNSCHED STAB TRIM) Light illuminates. (FCOM, 9.20.5). A.- TRUE. B.- FALSE.

What is the stabilizer trim rate during autopilot operation? (FCOM, 9.20.5). A.- Normal (full rate). B.- 1/2 full rate. C.- 1/4 full rate.

Where is the aileron trim indicator located? (FCOM, 9.10.3). A.- Aft control stand. B.- Center pilots panel. C.- Pilots control column. C.- Pilots control column.

When using the alternate flaps system, the flaps raise at what speed compared to hydraulic operation? (FCOM, 9.20.10). A.- Faster. B.- Slower. C.- The same.

Why should the speed brake lever be moved from armed to the down detent when the auto SPDBRK light illuminates? (FCOM, 9.20.9). A.- To prevent possible inflight speedbrake deployment. B.- To prevent asymmetric speedbrake deployment. C.- To restore operation of roll spoilers.

What is indicated when the right YAW DAMPER Switch has an ON indication and INOP light in view? (FCOM, 9.10.5). A.- The right yaw damper is inoperative. B.- No yaw damping capability exists. C.- The system has been turned off manually.

What is indicated by the Stabilizer Trim (STAB TRIM) Light, Illuminated (amber)? (FCOM, 9.10.3). A.- Stabilizer trim is operating normally. B.- Stabilizer trim rate is one–half the normal control wheel stabilizer trim switch rate. C.- Autopilot stabilizer trimming.

What is indicated by a FLAP LD RELIEF advisory message (EICAS)? (FCOM, 9.30.1). A.- System is retracting flaps to 25 position. B.- The flap load relief system fails to operate when required. C.- Flaps 30 airspeed is exceeded and pilot should slow down or retract flaps.

What happens when flaps 1 is selected? (FCOM, 9.20.9). A.- Only the trailing edge flaps are extended. B.- Both leading edge slat and trailing edge flaps are extended. C.- Commands the slats to move to the midrange position.

What functions do the yaw damper systems provide? (FCOM, 9.20.8). A.- Turn coordination and rudder load relief. B.- The yaw damper systems improve turn coordination and Dutch roll damping. C.- Rudder load relief and improved dutch roll characteristics.

What EICAS page displays the rudder, aileron and elevator positions? (FCOM, 9.10.5). A.- Maintenance. B.- Status Display. C.- Engine secondary.

What does the rudder trim indicator display? (FCOM, 9.10.4). A.- Trim input in units. B.- Rudder displacement in degrees. C.- Rudder displacement in percent of max. available.

What does the SPOILERS Light indicate when illuminated (Amber)? (FCOM, 9.10.8). A.- The spoilers are armed for deployment. B.- One or more spoiler pairs are inoperative. C.- The spoilers are deployed.

What is the purpose of the Flap Load Relief system? (FCOM, 9.20.10). A.- If the flap airspeed placard limit is exceeded with the flaps in the 25 or 30 positions, the flaps automatically retract to position 20. B.- Relieves "c" hydraulic system pressure to flap actuators when pressure is too high. C.- Ensures that trailing edge flaps extend before the leading edge flaps.

What is indicated when the left yaw damper switch is off and the indp light is illuminated? (FCOM, 9.10.5). A.- The system has been turned off manually. B.- A fault exists in the system. B.- A fault exists in the system. C.- No yaw damping capability exists.

What is indicated when the Aileron Lockout (AIL LOCK) Light comes Illuminated (amber)? (FCOM, 9.10.8). A.- All ailerons locked out. B.- One on both of the outboard ailerons may not have unlocked. C.- Aileron lockout actuator disagrees with the commanded position.

What is cutoff by Stabilizer (STAB) Cutout Switches? (FCOM, 9.10.2). A.- Manual trim signals. B.- Hydraulic power. C.- Electric trim signals.

How many hydraulic rudder actuators are depressurized when the rudder ratio light is illuminated? (FCOM, 9.20.8). A.- 1. B.- 2. C.- 3.

What is indicated by the flap position indicator at flaps 5? (FCOM, 9.10.11). A.- Trailing edge position. B.- Leading edge position. C.- Flap lever position.

What does the rudder ratio light illuminated inflight mean? (FCOM, 9.10.6). A.- One control system electronic unit is out. B.- Rudder displacement is no longer limited. C.- The rudder ratio changer is inop.

What system prevents structural damage due to large rudder displacement at high airspeed? (FCOM, 9.20.7). A.- Rudder ratio changer. B.- Feel unit. C.- Mechanical stop.

What does the aileron trim indicator display? (FCOM, 9.10.3). A.- Units of trim. B.- Degrees of trim. C.- Percent of max. trim.

What are the normal landing flap settings? (FCOM, 9.20.9). A.- 15 and 20. B.- 20 and 25. C.- 25 and 30.

What are the functions of the dual aileron trim switches? (FCOM, 9.10.4). A.- Both switches provide the same function. the second switch is a redundant backup. B.- One switch controls the hydraulic trim system and the other switch controls the electric backup system. C.- Moves the control wheel, ailerons, and spoilers in the desired direction.

How many actuators on each aileron panel position the ailerons? (FCOM, 9.20.4). A.- 1. B.- 2. C.- 3.

How many spoilers are there on each wing? (FCOM, 9.20.8). A.- 5. B.- 6. C.- 7.

How do the stabilizer trim switches located on the control columns actuate the trim control modules? (FCOM, 9.20.5). A.- Hydraulically. B.- Electrically. B.- Electrically. C.- Mechanically. C.- Mechanically.

How can stabilizer movement be stopped? (FCOM, 9.20.6). A.- Move the trim switches in the same direction. B.- Center the manual trim levers. C.- Use force on the control column in opposition to the runaway trim.

How are the flaps hydraulically powered under normal conditions? (FCOM, 13.20.2). A.- Left system. B.- Center and left system. C.- Center system.

From where is airspeed data for the Rudder ratio changer received? (FCOM, 9.20.7). A.- Pitot static system. B.- Air data computer. C.- Captain’s airspeed indicador.

Automatic operation of the ground speedbrakes may be affected by a partial or gear up landing. (FCOM, 9.20.8). A.- TRUE. B.- FALSE.

At what flap position are the leading edge slats fully extended in primary hydraulic drive. (FCOM, 9.20.9). A.- 1. B.- 20. C.- 25.

Hydraulic power for the elevators is provided by which hydraulic system(s). (FCOM, 9.20.4). A.- LEFT. B.- CENTER. C.- LEFT, CENTER, RIGHT.

How many hydraulic system(s) normally provide hydraulic power for rudder displacement? (FCOM, 9.20.4). A.- 1. B.- 2. C.- 3.

How many hydraulic power actuators are used for elevator movement under normal conditions? (FCOM, 9.20.4). A.- 1. B.- 2. C.- 3.

What systems must be available to the yaw dampers to pass a yaw damper test?. A.- EFIS, air data computer. B.- Hydraulic, air data computer. C.- Hydraulic, IRS.