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UC-12W NATOPS > Systems > Flashcards

Systems Flashcards

1
Q

Where is the pitch trim circuit breaker located

A

In the Flight group on the right circuit breaker panel

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2
Q

Can a copilots elevator trim thumb switch be overridden in

A

Yes the pilots thumb switch overrides the copilots

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3
Q

What does the bilevel trim disconnect button do at the first level

A

Disconnects the auto pilot and yaw damp and rudder boost systems

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4
Q

What does the bilevel trim disconnect switch do at the second level

A

Disconnects the electric elevator trim system

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5
Q

When can the manual trim control will be used to change the trim

A

Anytime the auto pilot is off

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6
Q

What is rudder boost

A

When system senses engine torque difference between the engines above a certain level the electric servo is actuated and deflects the rudder which assists pilot effort.
the servo contribution is proportional to the engine torque differential

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7
Q

What does prop sync button do

A

Activates propeller synchro phaser control unit

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8
Q

Where is the reversionary panel

A

Lower middle section of the instrument panel

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9
Q

What does DG switch do

A

Switches between free or manual mode and normal or slave mode which decides where the AHC gets its heading information from

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10
Q

What does the slew left or right switch do

A

Slew compass card either way

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11
Q

What does storm scope clear button do

A

Clear displayed images on the PFD or MFD and refresh to a new updated image

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12
Q

What does the pilot display switch do

A

Select the revisionary PFD or MFD display. Used if the PFD or MFD displays fail.

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13
Q

What does AHRS switch do

A

Used to select the attitude and heading source for the PFD and MFD displays

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14
Q

What does ADC switch do

A

Used to select the air data source for the PFD and MFD displays

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15
Q

What does emergency frequency switch do

A

A push-on push off switch which is used to force the number one VHF radio to tune to the emergency 121. 5 MHz frequency

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16
Q

What does the RMT tune switch do

A

Disable the auto tuning function of the CDU

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17
Q

What does GND COM ON switch to

A

Used to power the pilot side CDU and the number one VHF COMM radio when the battery switch is set to off only

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18
Q

What does cabin ALT HI warning light mean

A

Cabin pressure altitude exceeds 12,000 feet

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19
Q

What does CABIN DIFF HI warning light mean

A

Cabin differential pressure exceeds 6.9 psi

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20
Q

What do the bleed fail warning light mean

A

Melted or failed plastic bleed air failure warning line

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21
Q

What does L GEN TIE OPEN warning light mean

A

Left generator bus isolated from center bus

22
Q

What does HYD FLUID LOW light mean

A

Hydraulic fluid in the power pack is low

23
Q

What does RVS NOT READY warming light mean

A

Propeller levers are not in the high rpm low pitch position with landing gear extended

24
Q

What does R or L FUEL QTY warning light mean

A

Less than 30 min remaining at max continuous power

25
Q

What does AUTOFTHER OFF warning light mean

A

Auto feather switch is not armed and landing gear is extended

26
Q

What does OXY NOT ARMED warning light mean

A

Oxygen arming handle not pulled or system failed to charge

27
Q

What does R BL AIR OFF warning light mean

A

Right bleed air flow control valve is closed

28
Q

What does PROP GND SOL warning light mean

A

28 V is being delivered to one or both ground idle low pitch stop solenoids

29
Q

What does L IGNITION ON warning light mean

A

Left ignition and engine start switch is on or left auto ignition system is armed and left engine torque is below 17%

30
Q

What does MAN TIES CLOSE warning light mean

A

Manually closed generator bus ties

31
Q

What does R/L END ANTI ICE warning light mean

A

Engine anti ice vanes in position for icy conditions

32
Q

What does L/R PROP PITCH warning light mean

A

Propeller is below the flight idle stop

33
Q

What does CABIN ALTITUDE warning light mean

A

Cabin altitude exceeds 10,000 feet

34
Q

What does PASS OXYGEN ON warning light mean

A

Passenger oxygen system charged

35
Q

What does AIR COND N1 LOW warning light mean

A

Right engine N1 too low for air-conditioning load

36
Q

How do the rudder pedals Control nose wheel steering

A

Direct linkage

37
Q

What are the three flaps detents

A

Up
takeoff and approach
down

38
Q

How is the nose and mainly Nager assemblies retracted and extended

A

Hydraulically

39
Q

Where is the manual extension for the landing gear lever

A

Located on the floor on the pilot side of the pedestal

40
Q

What does LDG / TAXI LIGHT mean

A

Landing lights are left on with the landing gear up

41
Q

How long does it take for the hydraulic system to operate the gear either up or down

A

Approximately six seconds

42
Q

How is the landing gear held in the retracted position

A

By system pressure

43
Q

How is the landing gear held in the down position

A

Mechanically locked in place

44
Q

How long does a hydraulic system take to recharge the accumulator after landing gear attraction

A

A few minutes

45
Q

When does the landing gear warning system horn sound

A

With the flaps in either the up or approach position and either or both power leavers retarded below approximately 85% N1

46
Q

What is the landing gear manual extension procedure

A

Pull the landing gear relay circuit breaker located to the left of the landing gear control on the left side panels.
remove the alternate extension handle from the secure clip and pump up and down.
Do not lower the handle below the level of the securing clip as this will allow pressure to bleed off.
If one or more annunciators do not illuminate the handle must not be stowed leave it at the top of the upstroke.

47
Q

What type of tires on the aircraft

A

Main gear is 22x6.75 -10 10 ply tu less tires

Nose gear is 22x6.75-10 8 ply tubeless tires

48
Q

How should seats be position before takeoff and landing

A

Lateral tracking seats should be in the outboard position m, all seat backs positioned up right, and all headrests fully extended to prevent injury to passengers

49
Q

How many people can be on the air stare door stairway at any one time

A

Only one to prevent damage to door components

50
Q

How does the cabin door seal

A

Uses cabin differential pressure with no connection to a bleeder source

51
Q

What is the purpose of the disconnect safety mechanism on the flaps

A

Allows you to disconnect electrical power to flaps in the event of malfunction that causes flaps to be between 3 and 6 degrees out of phase of each other

UC-12W NATOPS (5 decks)

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