{Flight Safety's General PC-12 Questions} Flashcards

1
Q

What is the first step taken after a CAWS warning ENG FIRE and voice callout is received on the ground?

A

PCL idle

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2
Q

What action should be taken to prevent smoke or fumes from entering the cockpit as a result of an engine fire in flight?

A

ECS emergency shutoff - pull

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3
Q

Due to the composite construction of the engine cowling and possibility of toxic gases during a fire, what must be shut off when a fire condition is suspected?

A

ECS emergency shutoff - pull

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4
Q

What indication can be expected if the engine fire detection system fails?

A

A master caution CAWS - FIRE DETECT

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5
Q

True or False: The type of flight control system in the PC12 is electrically actuated, hydraulically boosted?

A

False

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6
Q

In pusher ice mode, when will the shaker and pusher activation occur?

A

8 degrees lower Angle of Attack, or approximately 10 degrees faster

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7
Q

When will the Pusher Ice Mode advisory CAWS illuminate?

A

Inertial Separator OPEN & Prop Heat ON

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8
Q

How will the stick pusher function in pusher safe mode?

A

Stick pusher will activate based on the lower flap when asymmetrical flap deflection happens.

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9
Q

Stick pusher is inhibited for how long after takeoff?

A

5 Seconds

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10
Q

What is required for stick shaker and pusher to operate?

A

One AoA computer activates the shaker, Two AoA computers activate the pusher

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11
Q

What are the indications in the cockpit when approaching a stall?

A

Shaking, beeping with mushy controls

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12
Q

What effect will stick pusher / shaker activation have on the Autopilot?

A

Autopilot disengages

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13
Q

True or False: The flaps on the PC12 are electrically actuated, single piece fowler.

A

True

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14
Q

Which flap positions are available?

A

0 - 15 - 30 - 40

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15
Q

What action must be taken if you get PUSHER on the ground and persist after completing the test?

A

No FLY

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16
Q

What action must be taken if the PUSHER CAWS illuminates when the aircraft is in flight and remains on after testing?

A

The aircraft is no longer stall protected - Follow the QRH

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17
Q

Which conditions could result in FLAPS illuminating in flight?

A

Asymmetrical flap deflection

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18
Q

After a FLAPS CAWS message appears what is the first step to take?

A

Check the Flaps CB - follow the QRH

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19
Q

FLAPS and PUSHER CAWS illuminated together means:

A

Flaps are asymmetrically deployed

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20
Q

What does a Green PUSHER ICE MODE CAWS mean?

A

Pusher computer set to ice mode

21
Q

If the flaps CB trips due to an overheat of the PDU, how long must you wait to reset the CB?

22
Q

How many times can a pilot reset the flaps CB?

23
Q

If the pilot pushes the FLAP INTERRUPT switch to INTERRUPT in flight and then switches it back to NORMAL will the flaps function?

24
Q

What indications will the pilot receive when the flaps are deployed above Vfe?

A

Red A/S in the flight indicator and a high pitch tone at 1600 Hz interrupted at 5 Hz intervals

25
In flight what is the only flap failure that can be reset?
PDU or CB overheat
26
True or False: Pitch Trim is accomplished by means of an electrically actuated trim tab mounted on the LH elevator
FALSE
27
What is the procedure to activate the pitch or aileron trim on the yoke?
Pull the trip, push the hat in the desired direction
28
During runaway trim operations what is the way the pilot can stop all trim operations?
Trim interrupt button above the PCL
29
What is the total usable fuel?
402 gallons
30
What are the approved fuel types?
Jet A, Jet A-1, Jet B, JP-4 and any fuel under SB 14004
31
What is the maximum fuel imbalance permitted for departure in pounds?
178#
32
What is the maximum fuel imbalance permitted for departure on the EIS fuel tape?
3 segments
33
The fuel reset button is used to reset what values?
The fuel used to zero and fuel contents after refueling.
34
When pulled what does the red fuel emergency shutoff handle in the cockpit do?
Fuel is prevented from entering the engine
35
When is PRIST required?
Any time a flight is conducted in temperatures below 0 degrees Celsius ***Guardian requires it for ALL flights***
36
Under normal conditions, when is the hydraulic power pack powered?
Under normal conditions: On the ground when the engine is running and always in the air
37
If the hydraulic power pack fails or a loss of electrical power occurs what keeps the gear up in flight?
A nitrogen charge can hold the gear up for approximately 200 minutes
38
What conditions will cause the HYDR CAWS caution light to appear?
In flight: Power pack is on for more than 10 minutes or if the PSI is less than 1800 On ground: The power pack cycled on more than 6 times in the past hour
39
Maximum cargo capacity?
3300#
40
Maximum luggage behind the luggage net?
400#
41
What type of engine does the PC-12 have?
PT6A-67B, or newer/upgraded aircraft: PT6A-67P
42
Where is the fire extinguisher?
Behind the co-pilot's seat
43
What position is the ELT kept in?
Armed
44
EFIS receives information from what sources?
AHRS 1/2, AOA, Navigation systems, pitot/static system
45
What navigation information can be displayed by bearing #1?
VOR 1, GPS 1, ADF 1
46
What does the 1|2 button do?
Switches between navigation radio 1 and navigation radio 2
47
During takeoff and landing what functions of the AP and Yaw damper system may be used?
None
48
What does SOFT RIDE mode do on the AP?
Turns down the gains, making smoother slower corrections. Disengages in approach and BC mode.