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Why are mechanical gates installed on the flap selector unit?

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Elevator system feel is provided by the elevator feel computer. This computer receives inputs of:

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The number of slats located on each wing are:

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The Speed Trim System (STS) is a speed stability augmentation system designed to improve flight characteristics during operation with a low gross weight, aft center of gravity and high thrust when the autopilot is not engaged.

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The STS monitors inputs of stabilizer position, thrust lever position, airspeed and vertical speed and then trims the stabilizer using the autopilot stabilizer trim.Remember that the SPEED TRIM FAIL amber light is often illuminated when you arrive at the aircraft. It is only due to the Inertial Vertical Speed Indicator which is not powered by the ADIRUs (IRS selectors OFF): the STS receives invalid inputs.

During descent from altitude you need to decrease your aispeed by using your speed brakes. What is the correct position of the SPEED BRAKE LEVER.

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The FEEL DIFF PRESS light indicates:

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Excessive differential pressure can be caused by erroneous activation of the Elevator Feel Shift module.

Yaw damper inputs (main or standby) can be overriden:

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Landing flap 40 selected and in position. An IAS of 178kts is flown due to a highwind gust. Would you expect:

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! When the flaps are set at 40, the TE flaps:- retract to 30 if airspeed exceeds 163 knots- re-extend when airspeed is reduced below 158 knots.When the flaps are set at 30, the TE flaps:- retract to 25 if the airspeed exceeds 176 knots- re-extend when airspeed is reduced below 171 knots.

The amber SPOLIERS light is located on the bottom right of the Flight Control Panel and indicates:

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The trailing edge flaps devices consist of double slotted flaps inboard outboard of each engine.

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During a normal landing, flight spoilers & ground spoilers will always extend simultaneously.

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The Power Transfer Unit provides an alternate source of power for the Autoslat System if:

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If a failed AOA circuit is detected, what will happen?

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The speedbrake lever will move forward and all spoilers will retract if either thrust lever is advanced after landing.

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The flight control computers use Mach Information from the _____ to compute a Mach trim actuator position.

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The amber ASSIST ON light indicates:

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Dual AILERON trim switches, located on the aft electronic panel, must be pushed simultaneously to command trim changes. The trim electrically repositions the aileron feel and centering unit, which causes the control wheel to rotate and redefines the aileron neutral position.

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If the difference in AoAs exceeds 5.5 degrees, what will happen?

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To operate the Feel system, the Elevator Feel Computer uses:

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The system operates normally even with only one hydraulics system remaining

Speed Trim Failure (SPEED TRIM FAIL) Light - If illuminated (amber) this indicates a:

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Concerning Mach Trim operation, FCCs use Mach information from the ADC / ADIRU, to compute a Mach trim actuator position whih repositions the elevator feel and centering unit, which adjusts the control column neutral position (column will not move).

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The column will move

During the ALTERNATE FLAPS OPERATION procedure, the flight crew should plan a Flaps 15 landing. After arming the ALTERNATE FLAPS MASTER SWITCH (230 kt max), the flight crew set the flaps to desired flap position and extend flaps on maneuvering speed schedule. The LE FLAPS TRANSIT light will remain illuminates until the flaps approach the:

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In the event of hydraulic Systems A & B fail, ailerons, elevators, and rudder can be operated with the Standby system.

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If wheel spinup is not detected on landing with the speed brake armed the flight spoilers will deploy automatically :

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What is the maximum flap extension altitude?

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The ALTERNATE FLAPS Master Switch:

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Leading Edge devices are normally operated by ______

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If a failed AOA circuit is detected, what will happen?

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The amber LE FLAPS TRANSIT light:

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The elevator transfer mechanism allows:

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During flight with both hydraulic systems A & B inoperative:

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With the loss of hydraulic system B, (system A operating normally):

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If the flight crew selects the ALTERNATE FLAPS to the ARM position:

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With a loss of both system A & B, the elevator FEEL DIFF PRESS light will illuminate.

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In addition to Hydraulic System A & B, the rudder can also be powered by the Standby Hydraulic System through the:

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The flap load relief system is operational at:

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The trailing edge flaps are at 15 units. The correct indication on the aft overhead panel for the leading edge devices is:

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Emergency Descent Speedbrakes are armed when is above 30,000 ft and:

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The Flap/Slat Electronics Unit (FSEU) provides:

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A Mach Trim system provides speed stability at the higher Mach numbers.Mach trim is automatically accomplished above:

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Loss of Hydraulic System B pressure does not cause illumination of the amber YAW DAMPER light or yaw damper disengagement.

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Main electric trim has 2 speed modes : high & low speed.

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The SPEED BRAKE DO NOT ARM light indicates that the speedbrake is not usable.

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During a steady right-handed turn on the ground, correct indications of the Yaw Damper indicator would be?

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Roll control is provided by the ailerons, assisted by the _____

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What is the correct flap setting for a jammed stabilizer landing?

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What is the number of flight spoilers located on each wing?

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The amber FEEL DIFF PRESS light illuminates when the:

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What is number of ground spoilers on each wing?

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If the spoilers become jammed:

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Mach Trim system corrects for Mach tuck by moving stabilizer up.

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It moves elevators up (not the stabilizer)

The Autoslat system:

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Extending the flaps to flaps 15 using ALTERNATE FLAPS takes approximately _______

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The Speed Trim System (STS) operates most frequently during takeoffs & go-arounds. Conditions for speed trim operation are:

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What do the MACH TRIM FAIL, SPEED TRIM FAIL & AUTO SLAT FAIL lights have in common?

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If the flight crew activates the FLT CONTROL switch Overhead panel to STBY RUD, it activates the:

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The primary flight controls consist of rudder, ailerons and ______

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The flight spoilers rise on the wing with up aileron and remain faired on the wing with down aileron. When the control wheel is displaced more than approximately ____ degrees, spoiler deflection is initiated.

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The airspeed range for trim operation is:

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Elevator Feel provides simulated aero forces using airspeed from elevator pitot & stabilizer position.

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The feel is transmitted to the control columns by the elevator feel & centering unit.

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If the SPEEDBRAKES EXTENDED light is illuminated in flight. It indicates:

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At what flap setting(s) should the leading edge slats be in the FULL EXTEND position?

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During an ALL FLAPS UP LANDING, the speed to be maintained is:

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Boeing 737 Max - Flight controls