Flight Controls and Hydraulics Flashcards

1
Q

Where is the pedal adjust handle located?

A

On the outside of the instrument panel.

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2
Q

Which cockpit control has a telescoping (extend/retract) feature?

A

Co-pilot’s collective

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3
Q

Outputs from cockpit controls are carried by mechanical linkage through the pilot assist servos to the ____________________.

A

Mechanical Mixing Unit (MMU)

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4
Q

The MMU is designed to reduce __________________________.

A

Inherent Control Coupling.

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5
Q

Name the four mechanical mixes provided by the MMU.

A

Collective to Pitch, Collective to Roll, Collective to Yaw, and Yaw to Pitch.

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6
Q

How does the MMU minimize inherent control coupling?

A

By combining, summing, and coupling collective, pitch, and yaw inputs.

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7
Q

Why is Collective/Airspeed to Yaw mixing completely phased out when the airspeed is above 100 kts?

A

Due to the efficiency of the tail rotor and cambered fin.

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8
Q

What has happened if we get the TAIL ROTOR QUAD FAIL caution?

A

One or both of the tail rotor cables has failed.

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9
Q

If only one of the cables breaks, what kind of aircraft control do the pilots have?

A

Full aircraft control.

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10
Q

If both cables break how do the pilots control the yaw axis?

A

Airspeed dependent on the aircraft gross weight.

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11
Q

Moving the SERVO OFF switch from NORM to 1ST STG or 2ND STG will _________________________________.

A

Turn off that stage (1st or 2nd) of the three primary servos.

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12
Q

What prevents the two stages of the primary servos from being turned off simultaneously?

A

Electrical interlock

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13
Q

On which panel can you find both the TAIL SERVO and BACKUP HYD PUMP switches?

A

MISC SWITCH panel

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14
Q

What system will automatically shut off components if a leak is detected?

A

LDI

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15
Q

The fluid quantity switch on the hydraulic pump module activates the appropriate RSVR LOW caution which indicates ________________.

A

A loss of hydraulic fluid for that system (Leak) less than 60% of fluid remaining in the pump.

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16
Q

What are the #1 and #2 hydraulic pumps mounted to and driven by?

A

The Accessory Modules.

17
Q

What is the Backup Pump driven by?

A

An electric motor

18
Q

What five things will activate the backup pump

A

HYD PUMP 1 FAIL
RSVR 1 LOW
T/R SERVO 1 FAIL
HYD PUMP 2 FAIL
APU ACCUM LOW

19
Q

What is the purpose of the APU Accumulator?

A

Provide a hydraulic charge to the APU start motor.

20
Q

In flight, the backup pump mode automatically sets to?

A

The AUTO mode even if the switch is in the Off or ON position.

21
Q

What does the backup pump supply pressure to?

A

No. 1 and/or No. 2 hydraulic systems, 2nd stage tail rotor servo and APU accumulator.

22
Q

What component located in the utility module will isolate a leak that occurs in the APU Accumulator?

A

The Velocity Fuse

23
Q

The No. 2 hydraulic system supplies pressure through the transfer module to what servos?

A

The second stage primary servos and the pilot-assist servos.

24
Q

The failure of the No. 2 hydraulic system illuminates what cautions / advisories if the backup pump fails to come on?

A

HYD PUMP 2 FAIL, PRI SERVO 2 FAIL, BOOST SERVO OFF, SAS OFF, TRIM FAIL and FPS FAIL.