Flight Director/Display Control Panel Flashcards

1
Q

What conditions does the go around buttons set?

A

Wings level
indicated AirSpeed 70 knots
vertical speed 750 ft per minute rate of climb
go around light off

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2
Q

What are the five components of the flight director set

A

Flight director display control panels (fd/dcp)
flight control computers (FCC)
multifunctional displays (MFDs)
sensors
go around and remote standby switches on the cyclic

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3
Q

What component processes and commands steering cues?

A

The fcc s

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4
Q

The FD processes signal from navigation and flight instrument sets to produce steering commands that are performed through which axes

A

Collective vertical pitch and roll

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5
Q

What are the five roll nav sources?

A

Fms VOR TCN loc and BC

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6
Q

Which roll nav source cannot be armed?

A

Fms

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7
Q

What navigation sources are available for bearing pointer selection?

A

Fms vor TCN and ADF

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8
Q

What are the functions of the p-sync knobs?

A

Push to sync captures current reference ie ias alt and rotate to adjust the desired FD reference value

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9
Q

If the uncoupled FD basic aircraft mode references (RALT ALT-P ALT IAS HDG VS) are changed, will the coupled FD references change?

A

Yes, changes to these references on either FD will change the reference on both fds coupled or uncoupled

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10
Q

To engage the level attitude recovery. The___z-axis must be pressed in above___kias

A

Cyclic trim beeper
60 kias

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11
Q

When the cyclic trim beeper is pressed above 60 kias what collective axis will couple?

A

Barometric alt

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12
Q

When coupled to the flight director, the pilot shall be in a position to override the___inputs

A

Flight controls

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13
Q

True or false when coupled the flight director can prevent exceeding engine (torque and TGT) limitations when the aircraft gross weight is less than 16,825 lb

A

False. There is no limiting in the collective axis of the coupled FD

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14
Q

What are the three HVR modes?

A

HVR DECL
HVR VEL
HVR POSN

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15
Q

GO ARND is designed to level the aircraft attitude establish a___fpm rate of climb and establish___ KIAS

A

750 FPM
70 kias

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16
Q

Once GO ARND has achieved 750 fpm and 70 KIAS, __mode disengages. ___and___modes will engage

A

GO ARND
VS AND IAS

17
Q

ALTP can be ARMED ___ and captures___feet prior to selected altitude

A

Anytime

300 ft

18
Q

How VS rate adjusted

A

Collective trim beeper or collective trim release while adjusting collective position

Does not have a p-sync knob

19
Q

With IAS mode engaged, what are three ways the pilot may adjust the reference value

A

P-SYNC knob
cyclic trim beeper (fore/aft)
cyclic trim release press and adjust cyclic position

20
Q

Which NAV SRC is capture only

21
Q

How HDG mode adjusted

A

Adjusting the HDG P-SYNC knob

22
Q

The Glide slope mode has an auto level sub mode designed to level the aircraft at___ft AGL

A

50 ft if Glide slope is followed below 200 ft AGL

23
Q

In order for ILS DECL mode to function, ___mode must be engaged

24
Q

When LOC is selected as the NAV SRC, BC will display on the FD when the difference between the inbound course and aircraft heading is greater than___degrees

25
If the flight director fails, what two cautions will appear
FLT DIR FAIL, FD COUPLE FAIL
26
What is the first underlined step for an uncommanded change in normal flight conditions while coupled to the FD
RMT SBY switch - press to disengage the FD modes
27
To clear a FLT DIR FAIL or FD COUPLE FAIL caution, what must the pilot clear on the AFCS control panel?
CPTR 1 and/or CPTR 2 (FCC COMPUTER 1 AND/OR FCC COMPUTER 2)