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CAE Ground School > Written Test > Flashcards

Written Test Flashcards

1
Q

King air is what category under what FAA part

A

Commuter under part 23

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2
Q

Standard emergency equipment

A

Portable fire extinguisher

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3
Q

Without battery, emergency exit lights are powered by what

A

Four C cell alkaline batteries

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4
Q

What does single GEN TIE OPEN light mean

A

Respective generator bus has been isolated from the center bus

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5
Q

Which bus powers the cockpit emergency lights

A

Dual fed

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6
Q

Normal generator voltage output

A

28.25 plus or minus .25

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7
Q

Generator load is limited to what on ground below 70% N1

A

75%

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8
Q

What will battery bus voltage read with battery switch off and battery bus emergency switch off

A

0 volts

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9
Q

Triple fed bus receives voltage from what the sources

A

Battery and left and right buses

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10
Q

Why do you reset right generator during start checklist and look for GEN TIE OPEN annunciators

A

Other generator voltage can be verified good while first generator is offline

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11
Q

If you leave start switch in ignition position what can’t be activated

A

Generator

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12
Q

The instrument emergency lights switch is where

A

Overhead instrument panel

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13
Q

Cockpit instrument emergency lights provide lighting through

A

Instrument sub panel

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14
Q

What does LDG/TAXI advisory light mean

A

One of the landing gear light switches is on and nose gear lock switch is engaged

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15
Q

Describe engine on king air

A

Reverse flow free turbine

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16
Q

Compressor bleed valve is close above what N1

A

98%

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17
Q

Where is ITT derived

A

Between compressor turbine and first stage power turbine stator vain rings

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18
Q

What provides initial spark for combustion

A

Igniters

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19
Q

When are igniters on

A

When starter switch is on or N1 drops below 17%

20
Q

Hot exhaust provides continuous Anti ice protection to what part

A

Engine inlet lips

21
Q

Best time to check engine oil

A

10 to 20 minutes after shutdown

22
Q

Max ITT for engine start with no inspection required

A

850 to 1000 for 5 seconds

23
Q

Describe engine oil system

A

Integral tank between engine air intake and accessory case

24
Q

What is between fuel tank and high pressure pump

A

Firewall valve, engine driven boost pump, strainer, heat exchanger

25
Q

What do you see if you put test switch in DET position

A

Corresponding ENG FIRE annunciator

26
Q

Where are portable fire extinguishers

A

One under Co pilot seat and one by door

27
Q

Describe engine fire protection system

A

Pneumatic system

28
Q

What is used as variable force to counter act spring force to adjust propeller blade angle

A

Governor boosted engine oil

29
Q

How many governors can adjust blade angle

A

Two

30
Q

What happens with primary Governor oil pump failure

A

Propeller feathers

31
Q

What controls propeller speed if propeller is forced pitch

A

Fuel topping Governor

32
Q

Auto feather is armed above what power lever setting

A

90%N1

33
Q

Prop sync will capture when props are within what RPM

A

23 to 27

34
Q

What does L/R FUEL QTY light mean

A

Approximately 300 lbs or less than 30 minutes of fuel left at max continuous power

35
Q

Where do jet transfer pumps receive motive flow fuel from

A

Engine driven boost pumps

36
Q

When does CROSSFEED light illuminate

A

When cross feed valve is open

37
Q

Which bus powers the fuel quantity gauges

A

Triple fed

38
Q

Describe the king air landing gear system

A

Electro hydraulic

39
Q

What is un augmented nose wheel deflection from rudder pedals

A

13 degrees from center

40
Q

Which pilots master cylinder can be used to set the parking brake

A

Either pilots

41
Q

When is power normally removed from the power pack gear retraction

A

When hydraulic pressure reaches 2775 psi

42
Q

First detente of the flap lever provides how much flap extension

A

40% or 14 degrees

43
Q

What happens when flaps are extended past 40% with the gear up

A

Landing gear warning both can’t be silenced

44
Q

How does rudder boost system detect engine power loss

A

Torque meter oil pressure is completed and rudder boost is initiated after difference in torques exceeds a preset level

45
Q

Yaw ramp must be operative for operations at or above

A

5000 ft single strake and 19000 ft dual aft strakes

46
Q

What is the function of the fuel topping Governor

A

Used to control reverse RPM during landing

CAE Ground School (5 decks)

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