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Sys LOD Jan 2021 > Flight Controls > Flashcards

Flight Controls Flashcards

1
Q

Explain the meaning of the SPEED BRAKES EXTENDED light.

In-flight

On the ground

A

In flight –
-SPEED BRAKE lever is beyond the ARMED position, and

  • TE flaps extended more than flaps 10, or
  • Radio altitude less than 800 feet.

On the ground –
- SPEED BRAKE lever is in the DOWN detent, and Ground spoilers are not stowed.

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2
Q

Explain the meaning of an amber LE FLAPS TRANSIT light. (4)

A
  • any LE device in transit.
  • any LE device not in programmed position with respect to TE flaps.
  • a LE slat skew condition exists.
  • illuminated during alternate flap extension until LE devices are fully extended and TE flaps reach flaps 10.

Note: Light is inhibited during autoslat operation in flight.

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3
Q

Explain the meaning of an illuminated Flight Control LOW PRESSURE light.

A
  • Indicates low hydraulic system (A or B) pressure to ailerons, elevator and rudder.
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4
Q

Explain the meaning of the FEEL DIFF PRESS light.

A

-Indicates excessive differential pressure in the elevator feel computer.

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5
Q

Explain the meaning of the SPEED TRIM FAIL light. (2)

A
  • Indicates failure of the speed trim system.
  • Indicates failure of a single FCC channel when MASTER CAUTION recall is activated.
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6
Q

Explain the meaning of the MACH TRIM FAIL light. (2)

A
  • Indicates failure of the mach trim system.
  • Indicates failure of a single FCC channel when MASTER CAUTION light recall is activated.
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7
Q

Explain the meaning of the AUTO SLAT FAIL light. (2)

A
  • Indicates failure of the auto slat system.
  • Indicates failure of the auto slat function in one of the SMYD computers when MASTER CAUTION light recall is activated.
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8
Q

Explain the meaning of the YAW DAMPER light.

A

Yaw damper is not engaged.

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9
Q

Explain the meaning of the SPEED BRAKE DO NOT ARM light.

A

When armed, Indicates abnormal condition or test inputs to the automatic speed brake system.

Light deactivated when SPEED BRAKE lever is in the DOWN position.

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10
Q

Explain the function of the FLT CONTROL switches located on the Forward Overhead panel.

ON

OFF

STBY RUD

A

STBY RUD – activates standby hydraulic system pump and opens standby rudder shutoff valve to pressurize standby rudder power control unit.

OFF – closes flight control shutoff valve, isolating ailerons, elevators and rudder from associated hydraulic system pressure.

ON (guarded position) – normal operating position.

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11
Q

Explain the function of the Control Column Stabilizer cutout switches.

A

Control column actuated stabilizer trim cutout switches stop operation of the main electric and autopilot trim when the control column movement opposes trim direction.

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12
Q

Explain how the Flap Load Relief system operates.

Flaps 40

Flaps 30

A

When the flaps are set at 40, the TE flaps:

  • retract to 30 if airspeed for flaps 40 is exceeded.
  • re-extend when airspeed is reduced below flaps 40 speed.

When the flaps are set at 30, the TE flaps:

  • retract to 25 if the airspeed for flaps 30 is exceeded.
  • re-extend when airspeed is reduced below flaps 30 speed.
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13
Q

Explain how primary flight controls are powered.

A

The flight controls are powered by redundant hydraulic sources; system A and system B. Either hydraulic system can operate all primary flight controls. The ailerons and elevators may be operated manually if required. The rudder may be operated by the standby hydraulic system if system A and system B pressure is not available.

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14
Q

Recall that flight spoilers assist the ailerons in roll control.

A

The flight spoilers rise on the wing with up aileron and remain faired on the wing with down aileron. When control wheel is displaced more than approximately 10 degrees, spoiler deflection is initiated.

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15
Q

Explain the function of the ALTERNATE FLAPS Master Switch.

OFF

ARM

A

OFF (guarded position) – normal operating position.

ARM – closes TE flap bypass valve, activates standby pump, and arms the ALTERNATE FLAPS Position Switch.

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16
Q

Explain the positions of the Speed Brake Lever.

DOWN

ARMED

FLT

UP

50%

A

DOWN (detent) – all flight and ground spoiler panels in faired position.

ARMED – - automatic speed brake system armed (illuminates SPEEDBRAKE ARMED light.) - upon touchdown, the SPEED BRAKE lever moves to the UP position, and all flight and ground spoilers extend.

FLIGHT DETENT – all flight spoilers are extended to their maximum position for inflight use.

UP – all flight and ground spoilers are extended to their maximum position for ground use.

50% (as modified) – if the speed brakes are deployed beyond the 50% position and the speedbrake load alleviation feature is activated: - the speed brake lever moves to the 50% position. - all flight spoilers retract to one-half of their maximum position for inflight use.

17
Q

Explain the function of the Speedbrake Load Alleviation Feature.

A

The automatic speed brake load alleviation feature limits the deployment of the speed brakes under certain high gross weight/airspeed combinations. Under these conditions, if the speed brakes are deployed to the FLIGHT DETENT, they automatically retract to 50 percent of the FLIGHT DETENT. The SPEED BRAKE lever moves to reflect the position of the speed brakes. Manual override is available. Increased force is needed to move the SPEED BRAKE lever beyond the 50 percent position with load alleviation active. The SPEED BRAKE lever must be held in place when manual override is used between 50 percent and the FLIGHT DETENT.

18
Q

Describe the Speed Brake system during ground operations.

when armed

A

During landing, the auto speed brake system operates when these conditions occur:

  • SPEED BRAKE lever is in the ARMED position.
  • SPEED BRAKE ARMED light is illuminated.
  • radio altitude is less than 10 feet.
  • landing gear strut compresses on touchdown.
  • both thrust levers are retarded to IDLE.
  • main landing gear wheels spin up. (more than 60 kts)

The SPEED BRAKE lever automatically moves to the UP position and the spoilers deploy.

Note: After an RTO or landing, if either thrust lever is advanced, the SPEED BRAKE lever automatically moves to the DOWN detent and all spoiler panels retract. The spoiler panels may also be retracted by manually moving the SPEED BRAKE lever to the DOWN detent.

19
Q

Recall the phase of flight that the Speed Trim System operates most frequently.

A

-STS operates most frequently during takeoffs, climb and go-arounds.

20
Q

Explain the function of the Control Column Stabilizer cutout switches.

A

Control column actuated stabilizer trim cutout switches stop the operation of the main electric and autopilot trim when the control column movement opposes trim direction.

Note: This mechanism is inside the control column near the floor. It senses excessive pressure on the yoke that opposes trim direction.

21
Q

Understand the purpose of the STAB TRIM OVERIDE switch on the AFT Electronic Panel.

A

OVERIDE- bypasses the control column actuated stabilizer cutout switches (FCTRL_014) to restore power to the Stabilizer Trim switches on the Control Wheel. NORM (guarded position) - normal operating position.

22
Q

Describe the Speed Brake system during ground operations.

If the SPEED BRAKE lever is in the DOWN position during landing or rejected takeoff,

A

If the SPEED BRAKE lever is in the DOWN position during landing or rejected takeoff, the auto speed brake system operates when these conditions occur:

  • main landing gear wheels spin up. (more than 60 kts)
  • both thrust levers are retarded to IDLE.
  • reverse thrust levers are positioned for reverse thrust.

The SPEED BRAKE lever automatically moves to the UP position and spoilers deploy.

Note: After an RTO or landing, if either thrust lever is advanced, the SPEED BRAKE lever automatically moves to the DOWN detent and all spoiler panels retract. The spoiler panels may also be retracted by manually moving the SPEED BRAKE lever to the DOWN detent.

Sys LOD Jan 2021 (15 decks)

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