AFCS Flashcards

(34 cards)

1
Q

What is the purpose of the Wildcat Automatic Flight Control System (AFCS)?

A

To incorporate the autostabilisation and in addition detect and correct for long-term errors in the aircraft’s flight path

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2
Q

What is the purpose of the series actuators within the Main Rotor Actuators (MRA)?

A

They are used to provide autostabilisation

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3
Q

What is the purpose of the parallel actuators?

A

They operate in parallel with the pilot’s controls as a result of the output of the Automatic Flight Control System (AFCS) computer

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4
Q

What allows a parallel actuator to be physically overridden when the Automatic Flight Control System (AFCS) autopilot is engaged?

A

A slipping clutch mechanism

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5
Q

Where is the Automatic Flight Control System (AFCS) controller located?

A

In the interseat console

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6
Q

How are the Automatic Flight Control System (AFCS) controller push buttons and display indication illumination levels set?

A

Utilising the AFCS controller dimmer

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7
Q

What is the function of the Computer Acceleration Control (CAC)?

A

Enhances pitch stability and reduces sideslip in turns above 60 kt

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8
Q

The Automatic Flight Control System (AFCS) actuators are configured in series with the main actuators and operate over what percentage of the available range?

A

10%

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9
Q

Why are the Main Rotor Actuators (MRA) internally split?

A

Permits continued operation of the unit if a failure of hydraulic pressure occurs in one system, or one lane of the Automatic Flight Control System (AFCS) is unserviceable

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10
Q

The Tail Rotor Actuator (TRA) is ………. powered, dual tandem design with a common piston rod

A

A hydraulically

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11
Q

What permits yaw pedal movement after a Tail Rotor Actuator (TRA) failure lock up?

A

A shear pin mounted on the actuator arm

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12
Q

What is a yaw parallel actuator?

A

It is a slow acting, electromechanical rotary actuator that operates over the full range of control run movement

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13
Q

What is the purpose of the electrical signals from the fore and aft and lateral Control Position Transmitters (CPT) to the Automatic Flight Control System (AFCS) computer?

A

To back off the error signals from the Attitude and Heading Reference System (AHRS) during pilot initiated cyclic manoeuvres

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14
Q

Which of the following captions illuminate when the Automatic Stabilisation Equipment (ASE) button on the Automatic Flight Control System (AFCS) controller is depressed?

A

ASE, P1 and P2, R1 and R2, Y1 and Y2

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15
Q

What condition does the Automatic Flight Control System (AFCS) need to be in before the Computer Acceleration Control (CAC) becomes operational?

A

At least one collective channel lane needs to be engaged

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16
Q

What is a precondition for selecting height hold on the Automatic Flight Control System (AFCS)?

A

At least one collective lane is engaged

17
Q

How is a manual height change with the Automatic Flight Control System (AFCS) height hold engaged normally achieved?

A

By selecting the COL REL button on the collective stick

18
Q

What is the effect of pushing the trim switch on the Automatic Flight Control System (AFCS) controller vertically downwards?

A

The pitch and roll AFCS actuators in the Main Rotor Actuator (MRA) are centralised

19
Q

What reason would the pitch and roll channels on the Automatic Flight Control System (AFCS) be trimmed?

A

To maintain the Centre of Gravity (CG) within the operating limits

20
Q

What will be the Automatic Flight Control System (AFCS) output if the aircrew momentarily displace the heading trim switch?

A

The aircraft heading will trim in 1° steps

21
Q

What information can the Automatic Flight Control System (AFCS) controller null indicators display?

A

Series actuator position and computer demand signals in lanes 1 and 2 of either the pitch/roll or yaw/collective channels

22
Q

Where is the CAC CUTOUT switch located?

A

On the cyclic stick grip

23
Q

What is the purpose of the CAC CUTOUT switch on the cyclic grip?

A

To disengage the Computer Acceleration Control (CAC) for fault diagnosis purposes

24
Q

What is the function of the COL REL button on the collective lever handgrip?

A

To disengage either Radar Altimeter (RadAlt) or barometric height hold

25
Where are the RAD ALT FLT/TEST and ADU FLT/TEST switches associated with the Automatic Flight Control System (AFCS) located?
Overhead console and panel KJ
26
Where are the RAD ALT FLT/TEST and ADU FLT/TEST switches associated with the Automatic Flight Control System (AFCS) located?
Overhead console and panel beneath the right side collective lever
27
What are the cockpit indications when a pitch actuator runaway condition is detected by the Pitch Actuator Runaway Protection System (PARPS)?
[AFCS] caution illuminated and audio alert, faulty lane light on Automatic Flight Control System (AFCS) controller extinguished, null indicator shows lane split
28
What happens on the Automatic Flight Control System (AFCS) roll channel when an aircraft banks at greater than 7°?
A computed roll rate signal predominates
29
What function is retained on the Automatic Flight Control System (AFCS) yaw channel when a yaw pedal is depressed to manoeuvre the aircraft?
Yaw stabilisation
30
What is the operational range of barometric height hold mode?
400-12,000 ft
31
What is the operational range of the radar altitude height hold?
100 to 500 ft (restricted by the Release To Service (RTS))
32
Which Automatic Flight Control System (AFCS) malfunction produces a no disturbance to aircraft attitude response?
Passive failures
33
How is an Automatic Flight Control System (AFCS) hardover failure in pitch detected?
The Pitch Actuator Runaway Protection System (PARPS) detects the onset of the failure and automatically disconnects the affected lane
34
What failure may cause the Automatic Flight Control System (AFCS) caution indicator to momentarily flash?
Oscillatory failure