Powerplant Flashcards

1
Q

What two identical units does the Pratt and Whitney of Canada PT6T-3B TwinPac consist of?
A. Free-shaft turbines driving the main transmission
B. Free-turbine turboshaft engines driving a combining gearbox
C. Gas producer sections driving a common power turbine
D. N1 sections driving identical N2 sections which drive the main transmission

A

B. Free-turbine turboshaft engines driving a combining gearbox

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2
Q
Which unit is the primary drive responsibility of the gas producer (N1) section?
A. The main transmission
B. The combining gearbox 
C. The power turbine (N2)
D. The N1 accessory section
A

C. The power turbine (N2)

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3
Q
The overall combining gearbox:
A. Reduces N2 rpm
B. Combines both engines' power output
C. Mounts and drives various N2 and C-box accessories
D. All the above
A

D. All the above

Reduces N2 rpm
Combines both engines’ power output
Mounts and drives various N2 and C-box accessories

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4
Q

The combining gearbox is actually:
A. One section which reduces engine RPM
B. Divided into two sections of N2 gear reduction
C. Divided into three sections - two for gear reduction and one for combining
D. Divided into four sections - two for gear reduction, one for combining, and one for torque sensing, limit- ing, and sharing

A

C. Divided into three sections - two for gear reduction and one for combining

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5
Q

N1 tachometer generator signals are used to indicate the percent of each engine’s N1 rpm on the N1 gage and to:
A. Actuate the low rpm light and audio warning systems
B. Actuate each engine’s ENGINE OUT warning light and particle separator system
C. Activate each engine’s N1 overspeed protection circuit
D. Activate torque limiting in the torque control unit

A

B. Actuate each engine’s ENGINE OUT warning light and particle separator system

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6
Q

Interturbine temperature (ITT) indications are:
A. Self-generating by means of eight thermocouples
B. Provided by probes in front of the N 1 turbine wheel
C. Self-generating and direct-reading
D. Self-generating but require correction by the ITT trim compensator unit

A

D. Self-generating but require correction by the ITT trim compensator unit

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7
Q

N2 tachometer generator signals:
A. Actuate the low rpm light and audio warning systems
B. Actuate each engine’s ENGINE OUT warning light and particle separator system
C. Provide cockpit N2 indications on the triple tachometer
D. Activate torque limiting in the torque control unit

A

C. Provide cockpit N2 indications on the triple tachometer

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8
Q

Engine torque indication is a function of ______ which operates a sensor unit in the ______.
A. Engine oil pressure, N2 gear reduction section
B. Engine oil pressure, N1 turbine wheel area
C. Engine oil pressure, combining section of the C-box
D. C-box oil pressure, combining section of the C-box

A

A. Engine oil pressure, N2 gear reduction section

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9
Q

Transmission torque is displayed on the dual torquemeter by:
A. A monopole sensor inside the main rotor mast
B. A separate torque sensor in the main transmission
C. A separate torque sensor on the combining gear in the C-box
D. Combining engine torque signals within the dual torquemeter

A

D. Combining engine torque signals within the dual torquemeter

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10
Q
Optimum compressor efficiency and anti-stall operation during engine starting and N1 acceleration are provided by:
A. A compressor bleed band
B. A compressor air bleed valve 
C. Variable inlet guide vanes 
D. The compressor speed limiter
A

B. A compressor air bleed valve

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11
Q

The engine oil-to-fuel heat exchanger regulates fuel heating by means of a thermostatic valve which is controlled by engine:
A. Oil temperature entering the heat exchanger
B. Oil temperature exiting the heat exchanger
C. Fuel temperature entering the heat exchanger
D. Fuel temperature exiting the heat exchanger

A

D. Fuel temperature exiting the heat exchanger

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12
Q

The engine fuel filter system includes:
A. A bypass in the event of clogging
B. An automatic filter backwash and drain system
C. A FUEL FILTER caution light and a bypass
D. A FUEL BYPASS caution light

A

C. A FUEL FILTER caution light and a bypass

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13
Q

The engine-driven fuel pump puts out high pressure fuel to operate the:
A. Fuel bypass system of the fuel filter
B. Fuel control unit, flow divider, and dump valve
C. Manual portion of the fuel control
D. Flow divider and dump valve

A

B. Fuel control unit, flow divider, and dump valve

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14
Q

The fuel control unit on each PT6T-3B engine is:
A. Hydropneumatic with automatic or manual operation
B. Hydroelectric with automatic or manual operation
C. Pneumatic-electric with automatic or manual operation
D. Hydropneumatic, controlled only by the twist-grip throttle

A

A. Hydropneumatic with automatic or manual operation

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15
Q

The flow divider and dump valve:
A. Drain fuel after engine shutdown
B. Separate fuel flow between the N1 and N2 burner sections
C. Separate fuel flow between the manual and automatic fuel control units and drain fuel from them after engine shutdown
D. Separate fuel flow between the primary and secondary fuel manifolds and nozzles and drain fuel from them after engine shutdown

A

D. Separate fuel flow between the primary and secondary fuel manifolds and nozzles and drain fuel from them after engine shutdown

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16
Q

Engine ignition occurs:
A. Any time the starter switch is activated
B. Only if the fuel switch is in ON and the starter is activated
C. Continuously if the fuel switch is in ON
D. Only if the ignition and starter switches are in ON

A

B. Only if the fuel switch is in ON and the starter is activated

17
Q

Powerplant lubrication systems all function similarly since they all follow the same procedure of the oil.
A. Pressurizing, cooling, filtering, and using
B. Pressurizing, using, cooling, and filtering
C. Cooling, filtering, pressurizing, and using
D. Pressurizing, filtering, cooling, and using

A

A. Pressurizing, cooling, filtering, and using

18
Q

There are ______ engine oil pumps, _______.
A. Two, one for pressure and one for scavenge
B. Three, one for pressure and two for scavenge
C. Four, one for pressure and three for scavenge
D. Four, two for pressure and two for scavenge

A

C. Four, one for pressure and three for scavenge

19
Q
The primary indication of low engine oil pressure is the engine's:
A. OIL PRESSURE caution light
B. Oil pressure gage
C. OIL TEMP caution light
D. Oil temperature gage
A

B. Oil pressure gage

20
Q

A loss of engine oil pressure results in:
A. A loss of the C-box lubrication
B. A loss of the engine’s chip detector system
C. A loss of engine torque indication
D. Excessive heating of engine fuel

A

C. A loss of engine torque indication

21
Q
Excessive engine oil temperature should be treated in the same manner as:
A. A loss of the C-box lubrication
B. A loss of engine oil pressure
C. An engine chip
D. An engine fire
A

B. A loss of engine oil pressure

22
Q

The engine chip detector system includes:
A. One chip detector and an engine CHIP caution light
B. Two chip detectors and an engine CHIP caution light
C. Two chip detectors and two engine CHIP caution lights
D. Two chip detectors, one CHIP light, and two remote indicators

A

B. Two chip detectors and an engine CHIP caution light

23
Q

Overfilling the C-box oil system results in:
A. Excess oil being vented from the filler cap
B. Lower than normal C-box oil temperature
C. A popped red button on the remote indicator
D. Excess oil vented to the engine oil system

A

A. Excess oil being vented from the filler cap

24
Q
A remote indicator for the C-box oil system indicates:
A. Overfilling of the C-box oil system
B. Overpressure of the C-box oil cooler
C. The C-box oil filter is bypassed.
D. The C-box oil cooler is clogged.
A

C. The C-box oil filter is bypassed.

25
Q

Loss of C-box oil pressure results in:
A. Erroneous hourmeter readings
B. A popped red button on the remote indicator
C. Loss of transmission torque indication
D. Erroneous engine torque indication

A

A. Erroneous hourmeter readings

26
Q

The C-box oil system includes:
A. CHIP C BOX, C BOX OIL PRESS, and C BOX OIL TEMP warning lights
B. A CHIP C BOX caution light and C BOX OIL PRESS and C BOX OIL TEMP warning lights
C. CHIP C BOX, C BOX OIL PRESS, and C BOX OIL TEMP caution lights
D. C BOX OIL PRESS, C BOX OIL TEMP, and two CHIP C BOX warning lights

A

B. A CHIP C BOX caution light and C BOX OIL PRESS and C BOX OIL TEMP warning lights

27
Q

Excessive C-box oil temperature:
A. Is the same as excessive engine oil temperature
B. Requires an immediate landing
C. Is not a major concern and should be corrected prior to the next flight
D. Requires landing as soon as possible

A

D. Requires landing as soon as possible

28
Q
The type of FCU malfunction should be determined from the:
A. N1 and ITT gages
B. Dual torquemeter
C. Helicopter reaction
D. Triple tachometer
A

D. Triple tachometer

29
Q
The engine affected with an FCU malfunction can be determined from the:
A. N1 and ITT gages
B. Dual torquemeter
C. The degree of over- or under-speed
D. Triple tachometer
A

B. Dual torquemeter

30
Q
Low side FCU malfunctions require:
A. Throttle adjustment only
B. Throttle adjustment in manual mode
C. Engine shutdown and landing as soon as possible
D. No action other than engine shutdown
A

B. Throttle adjustment in manual mode

31
Q

High side FCU malfunctions:
A. May be controlled by reducing throttle from full open
B. May require entering manual FCU mode of operation
C. Require engine shutdown and land- ing as soon as possible
D. Either A or B above may be required

A

D. Either A or B above may be required

May be controlled by reducing throttle from full open
May require entering manual FCU mode of operation