T3 DAFC Flashcards

1
Q

With the aircraft at a hover and Translational Rate Command captured, what will occur if the DAFCS Trim Switch is beeped forward 3 times?

A

Move forward at 3 knots

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2
Q

The DAFCS stabilizes the helicopter about all axis and enhances control response. Name five features provided by DAFCS.

A

Heading Hold, Altitutde Hold, Aircrast Stability, Pitch Attitude Hold, Altitude Hold, DAFCS Trim, Bankle Angle Hold, Airspeed Hold

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3
Q

How do you momentarily disengage altitude hold when changing altitudes?

A

Thrust brake

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4
Q

When flying in known or forcast moderate or above turbulance, what are the three concerns/restrictions the pilot should be aware of?

A

Do not use BALT hold, ensure thrust brake operation, LCT in MAN

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5
Q

Will the cyclic move when the DAFCS trim switch is moved laterally?

A

No

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6
Q

Should BARO ALT hold be used in moderate turbulance or above?

A

No

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7
Q

Which actuator makes the control input for positive stick gradient, pitch attitude, and airspeed hold purposes?

A

DASH

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8
Q

What is the status of the Heading Stability feature when the Swivel Lock Switch is not in the LOCK pistion?

A

DAFCS Heading Hold is degraded

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9
Q

Will the Longitudinal Cyclic Trim Actuators function with the DAFC Switch in the off postion?

A

Yes

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10
Q

With the Translational Rate Command captured, what happens to the status of the TRC when either WOW switch engages?

A

Disengaged

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11
Q

When flying in moderate turbulance or above, should BARO ALT be engaged?

A

No

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12
Q

What is the name of the DAFCS component which the #1 Fligh Control Computer control to provide Altitude Hold?

A

Thrust CCDA

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13
Q

Which DAFCS computer controls the radar and inertial altitude hold?

A

FCC1

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14
Q

How do the flight control computers know to place the LCT actuators to the GRD position when in AUTO?

A

Both WOW switches engage

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15
Q

What should you do if the LCT actuator fails to postion to GND during taxi, water, or slope operations?

A

Place LCTs in Manual

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16
Q

When accelerating from a hover, what is the max groundspeed which can be flown to remain within the Low Speed Regime?

A

20 KGS

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17
Q

At what groundspeed does the TRC feature become active or captured?

A

Below 9 KGS

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18
Q

Name two features of DAFCS that disengage when the Centering Device Release switch is pressed?

A

Bank Angle Hold, Heading Hold

19
Q

What are the three control laws for the DAFCS?

A

Forward Flight, Low Speed, Ground

20
Q

What is the maximum aircraft bank angle with altitude hold?

A

45

21
Q

What is the maximum allowable airspeed when operating with both DAFCS OFF?

A

160 KCAS

22
Q

What is the maximum allowable airspeed when operating with a single DAFCS ON?

A

100 KCAS

23
Q

What must be monitored to prevent transmission damage when changing airspeed ot heading with ALT HOLD engaged?

A

Torque

24
Q

Which Flight Control Computer control the Pitch CCDA?

A

FCC2

25
Q

At what groundspeed will the Low Speed Regime become active when decelerating?

A

16 KGS

26
Q

If you have a hard-over with both DAFCS on, how will you know when you have the good system selected ON and the malfunctioning system OFF?

A

Reverse Hard-Over

27
Q

What action is required to release the Thrust Magnetic Brake?

A

Depress the Thrust Brake Switch

28
Q

How will the aircraft react if DAFCS is turned Off at one airspeed and back on at a different airspeed?

A

Pitch Transients, adjusting to go where it was turned off

29
Q

What visual indications will you see when the DASH Actuators are re-centering when the DAFCS is first turned on?

A

DASH Caution Lights

30
Q

Do not manually extend the LCT actuators beyond GND position on the cyclic trim indicators at airspeed below ____ KIAS

A

60

31
Q

Describe one way you can change the aircraft bank angle without moving the cyclic?

A

AFCS Trim Switch

32
Q

Which mode of LCT operation should you select during flight in moderate or above turbulance?

A

Manual

33
Q

What does the acronym CPT stand for?

A

Control Position Transducer

34
Q

What does the acronym LVDT stand for?

A

Linear Variable Differential Transducer

35
Q

What is the name of the portion of the Integrated Lower Control Actuator that is controlled by the DAFCS Flight Control Computer?

A

Extendible Link

36
Q

How accurate is the DAFCS Heading Hold feature?

A

+/- 5 degrees

37
Q

When the landing gear proximity switches are active, the DAFCS input into the Pitch ILCA is reduced by what percent?

A

50

38
Q

What 3 DAFCS features are provided by the DASH actuator?

A

Airspeed Hold, Pitch Attitude Hold, Positive Stick Gradient

39
Q

Which Flight Control Computer controls the Thrust CCDA?

A

FCC1

40
Q

At what groundspeed does the Position Hold feature become active?

A

1 KGS

41
Q

Is “Go Around” a DAFCS feature or a feature of the Flight Director?

A

Flight Director

42
Q

When can radar altitude hold be used in forward flight?

A

Over water or known flat terrain

43
Q

Does the cyclic have to be centered for the cyclic to be in detent?

A

No

44
Q

Should you allow the cyclic to move when the AFCS trim switch is moved forward or aft?

A

Yes