Flight Controls Flashcards

1
Q

How are the primary flight controls controlled and actuated?

A

Electronically controlled by the fly-by-wire (FBW) system
Hydraulically actuated by power control units (PCUs)

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2
Q

What are the FBW normal mode tactile pitch protections?

A

Progressive increase in required sidestick force as sidestick deflection is increased
Soft stop in the pitch axis at the operational flight envelope
Hard stop at the sidestick travel limit in the pitch axis at the airplane structural limit
Stick shaker

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3
Q

What is the normal mode nose-up pitch attitude limit in flight?

A

30º

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4
Q

What is the normal mode nose-up pitch attitude limit during takeoff?

A

17.5⁰ to assist in preventing a tail strike on takeoff

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5
Q

What is the normal mode nose-down pitch attitude limit in flight?

A

20º

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6
Q

Is the airplane aerodynamically stalled, in the normal mode, while maintaining VAOA HARD (Hard Stop)?

A

No; In smooth air, the hard stop maintains an AOA value for activating the stick shaker

Note: Environmental factors such as turbulence or gusts can cause airspeed to decrease
below VAOA HARD. In this case, the airplane may stall in FBW normal mode momentarily as the
airplane pitch is adjusted to regain VAOA HARD.

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7
Q

In FBW normal mode, what is the maximum bank angle limit?

A

80º

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8
Q

Passed what bank angle in the normal mode will FBW return to?

A

30°

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9
Q

To what degree is pitch compensation in turns provided?

A

33⁰

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10
Q

What are the 3 FBW direct modes?

A

PFCC (primary flight control computer) direct
REU (remote electronic unit) direct
AFCU (alternate flight control unit) direct

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11
Q

What causes PFCC direct mode?

A

Loss on input to the PFCC; IRS, ADC etc

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12
Q

What causes REU direct mode?

A

Loss of all three PFCC

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13
Q

What causes AFCU direct mode?

A

Loss of all REU to a single flight control surface

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14
Q

Is the autopilot available in FBW direct modes?

A

No

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15
Q

How do you regain FBW normal mode after a complete PFCC failure?

A

All PFCCs must be reset by pressing the PBAs to OFF then ON
Note: this is not a memorized event. There is a checklist for this!

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16
Q

What will occur if the rudder or stab trim is outside the allowable takeoff range during thrust lever
advancement?

A

Red CONFIG RUDDER TRIM or CONFIG STAB TRIM CAS will appear
“No Takeoff” aural alert

17
Q

What functions does the AP/PTY switch on the sidestick provide when pressed momentarily?

A

Disconnects the autopilot if engaged
Selects sidestick momentary priority if the autopilot is not engaged

18
Q

What is the function of the ALTN FLAP PBA?

A

Will extend the slats and flaps to position 2

Note: The slats and flaps begin movement only if the airspeed is at or below 200kt. This
control is a work around for a failed flap handle. There is only an alternate control and not an
alternate operating system.

19
Q

Will failure of the flaps prevent operation of the slats?

A

No; the slats and flaps have independent dual-motor power drive units (PDUs)

20
Q

What is the purpose of the FLAPS OFF PBA on the TAWS panel?

A

Used to cancel the flap aural warning if the flaps are not set at 4 with the gear down, airspeed
below 159kt, and altitude below 245ft (75m) for landing

21
Q

How many pairs of spoiler panels are located on each wing?

A

3 multi-functional spoilers (MFS)
1 ground spoiler (GS)

22
Q

How are the spoilers controlled and actuated?

A

Electrically controlled
Hydraulically actuated

23
Q

What do the MFS panels provide?

A

Roll
Drag
Ground lift dumping

24
Q

Which hydraulic system powers the ground spoilers?

A

HYD system 1

25
Q

What is the activation logic for the ground spoilers?

A

Either MLG is weight-on-wheels, and
Either MLG wheel speed is greater than 16kt, and one of the following
RAD ALT below 7ft, or
Both MLG are weight-on-wheels and airplane pitch angle less than 2º

26
Q

When in AFCU direct mode, what spoilers are available?

A

None

27
Q

What happens if both sidesticks are operated simultaneously?

A

Red DUAL annunciation is shown on both PFDs
“DUAL INPUT” aural warning message
The total summed input signal of both sidesticks is limited to the maximum deflection of a single sidestick

28
Q

What happens when the AP/PTY pushbutton is pressed and held?

A

The autopilot, if engaged, disconnects
The opposite sidestick and its pitch trim switch are deactivated
The PTY legend on the onside glareshield SIDESTICK guarded PBA flashes
A red arrow illuminates on the opposite SIDESTICK guarded PBA
A “PRIORITY LEFT” or “PRIORITY RIGHT” aural message is annunciated once
Note: when both AP/PTY pushbuttons are pressed, the last one pressed has priority. If the
AP/PTY pushbuttons are pressed simultaneously, the left sidestick has priority

29
Q

What happens when the guarded SIDESTICK PBA on the glareshield is pressed?

A

The autopilot, if engaged, does not disconnect
The PTY legend on the onside glareshield SIDESTICK PBA remains on without flashing
The AP/PTY pushbutton on the disabled sidestick has no effect
Note: Pressing the guarded SIDESTICK PBA on the disabled side transfers sidestick priority