CAE Flight Controls Flashcards

1
Q

What is the max altitude with the YD inop?

A

31,000’

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2
Q

What conditions exist while a pilot is depressing the MSW?

A

AP disengage, all trims inop, stall pusher inop (except on EASA aircraft)

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3
Q

At what altitude will the half bank mode automatically engage?

A

31,600’

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4
Q

Can the pilot override the YD command?

A

No

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5
Q

Normal flap extension from 0 to 30 should not exceed what time limit?

A

20 seconds

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6
Q

To what degree can the multifunction spoilers extend with control wheel input?

A

45 degrees

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7
Q

What spoiler panels move on the ground?

A

All of them

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8
Q

What are the selectable flap positions?

A

0, 10, 20, 30

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9
Q

How does manual reversion work?

A

Automatically, with cables through the PCUs

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10
Q

Why are balance tabs installed?

A

To reduce the pilot effort needed to move the ailerons

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11
Q

Do both ailerons have trim tabs?

A

No, just the left aileron

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11
Q

PCU is an acronym for what term?

A

Power Control Unit

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12
Q

Can spoilers and flaps be used at the same time?

A

Yes

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13
Q

Which trim, primary or secondary, trims faster at cruise?

A

Secondary trim

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14
Q

What functions does the primary trim have that the secondary trim doesn’t?

A

Autopilot, configuration trim, variable speed trim and Mach trim

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15
Q

If a seriies of defective components causes the available hydraulic pressure to decrease to 0, can the rudder be controlled?

A

Yes, through cables by mechanical input only (manual reversion)

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16
Q

Is the travel time the same using ALT flaps compared with using normal flaps?

A

No. Using ALT flaps, the flpas run more slowly at FLAPS RATE LOW

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17
Q

If primary trim is inoperable, is configuration trim still available?

18
Q

The YD system is mechanically limited to how many degrees of rudder deflection?

19
Q

Where are the spoiler RVDTs located?

A

Inside both yokes

20
Q

Which flight computer controls the outboard flight spoilers?

21
Q

Can the YD be engaged independently from the AP?

22
Q

What are the limitations with flight spoiler use

A

Not below 500’ AGL
Min speed Vref+8
No emergency spolers unless in emergency conditions or directed by procedure

23
Q

Which flight computer controls inboard flight spoilers

24
Q

What computer commands the roll spoilers to move?

A

Spoiler electronic control unit (SECU) computer

25
Q

Which flight control surface does the left yoke operate after the pitch disconnect handle was pulled?

A

The left yoke controls the left elevator

26
Q

Which spoilers are used for lift dumping?

A

Panel 1 and 8 in MAX and 2 and 7 in EMER

27
Q

When can flight spoilers be extended to EMER

A

Only in an emergency condition or as required by a procedure

28
Q

Flight spoilers must not be extended in flight below which approach speed?

29
Q

The rudder travel limit confines the rudder contol surface movement as a function of what?

30
Q

The CL30/35 has how many stick shaker(s) in what location?

A

Two, one attached to each yoke

31
Q

The CL30/35 has how many stick pusher(s) in what location?

A

One, in the left yoke

32
Q

Which flight control surfaces does the left yoke operate after the roll disconnect has been pulled?

A

The left yoke contols the multifunction spoilers only.

33
Q

What are the max Flap Extended airspeeds for Flaps 10 / 20 / 30

A

10: 210
20: 210
30: 175

34
Q

Which flight contol surfaces does the right yoke operate after the pitch disconnect handle has been pulled?

A

The right yoke controls the right elevator

35
Q

With the spoilers in the MAX position and the flaps extending to WHAT position, the aircraft may exhibit a slight wing dip that is easily controllable by either pilot or by the autopilot.

A

20 degrees

36
Q

Name the primary flight controls

A

Elevators, rudders, ailerons and roll spoilers

37
Q

When extended, the ground spoilers extend to xxx degrees; the multifunction spoilers extend to yyy degrees

A

Ground spoilers extend to 60 degrees, multifunction spoilers to a max of 45 degrees.

38
Q

What are bent tabs

A

Bent tabs are positioned on the trailing edge of the aileron surface to keep the survace upfloat to a minimum at high speeds

39
Q

What functions of PRI stab trim are lost when selecting SEC trim?

A

Autopilot, Mach and configuration trim, speed dependent trim rate

40
Q

On TO roll, when the aircraft accelerates above HOW MANY kts, the YD function is smoothly disabled until weight is off the wheels

41
Q

Name the secondary flight controls

A

Aileron and rudder trims, horizontal stabilizer, flaps, spoilers

42
Q

Is there an artifical feel to the rudder?

43
Q

What primary flight controls are hydraulically powered?

A

All of the except the ailerons