BBD-700 Flight Controls Flashcards

1
Q

How are the primary flight controls controlled and actuated?

A

Mechanically controlled

Hydraulically actuated

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2
Q

Which hydraulic systems power the aileron PCUs?

A

Left aileron – systems 1 and 3

Right aileron – systems 2 and 3

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3
Q

How are the aileron control circuits separated in response to a jammed control system?

A

Via a roll disconnect mechanism in the torque tube

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4
Q

If the aileron/rudder/stabilizer trim is outside the allowable range during throttle advancement for takeoff, what will occur?

A

CONFIG AIL / RUD / STAB TRIM red warning message

NO TAKEOFF voice message

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5
Q

When is initial yaw damper engagement controlled by the flight guidance computer?

A

First engine start

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6
Q

Which hydraulic systems power the rudder PCUs?

A

Hydraulic systems 1, 2 and 3

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7
Q

Which hydraulic systems power the elevator PCUs?

A

Left elevator – systems 1 and 3

Right elevator – systems 2 and 3

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8
Q

Which 3 trim modes activate the horizontal stabilizer and their priority?

A
Manual trim (pilot then copilot)
Auto trim (autopilot 1 or 2)
Mach trim (autopilot off)
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9
Q

What functions does the Master Disconnect Switch on the yoke provide?

A

AFCS disconnect – momentarily selected
Pitch trim disconnect – held
Stall pusher - held

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10
Q

When will the stabilizer in motion aural clacker sound?

A

Stabilizer runaway

Stabilizer trim switch is held for an extended period

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11
Q

How is operation of the slats and flaps controlled?

A

By two independent slat/flap control units (SFCUs)

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12
Q

What is the purpose of the “Flap Override Switch”?

A

Used to cancel the flap aural warning if the flaps cannot be configured for an OUT/30 landing

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13
Q

How many spoiler panels are located on each wing?

A

4 multifunctional spoilers (MFS)
and
2 ground spoilers (GS)

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14
Q

With flaps extended, which MFS are available?

A

Only the two inboard pairs of MFS

MAX selection on the FSCL has no effect

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15
Q

The MFS are used for what purpose?

A

Roll assist
Proportional lift dumping
Ground lift dumping
Combination roll assist and proportional lift dumping

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16
Q

How is symmetrical lift dumping ensured when an MFS panel failure is detected?

A

The opposite panel is automatically disabled

17
Q

Ground spoilers when “armed” will deploy on landing with?

A

Engine throttles at idle or below and two of the following three conditions:
RA below 7 feet
One main landing gear WOW
One wheel speed greater than 16 knots

18
Q

How may pilot stop the stick pusher?

A

Pressing and holding the autopilot/stick pusher disconnect (AP/SP DISC) button
N/A for JAA certified aircraft