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BH206L > Crew Compartment > Flashcards

Crew Compartment Flashcards

1
Q

Turning on the PITOT HEATER switch will activate the heater element for the pitot tube and the static ports.

a) True.

b) False.

A

B) False.

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2
Q

The static ports are not heated.

a) True.

b) False.

A

A) True.

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3
Q

Maximum autorotation speed of 100 kts is indicated by a __________ line on the airspeed indicator.

a) Red.

b) Yellow.

c) Blue.

A

C) Blue

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4
Q

Vne of 130 kts is indicated by a __________ line on the airspeed indicator.

a) Red.

b) Yellow.

c) Blue.

A

A) Red.

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5
Q

Main rotor rpm is indicated on the __________ on the dual tachometer.

a) Digital readout.

b) Inner scale.

c) Outer scale.

A

B) Inner scale.

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6
Q

Engine rpm is indicated on the __________ on the dual tachometer.

a) Digital readout.

b) Inner scale.

c) Outer scale.

A

C) Outer scale.

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7
Q

The gas producer (N1) indicator will operate without electrical bus power.

a) True.

b) False.

A

A) True.

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8
Q

On the Diamond J torquemeter; a condition greater that 110% results in

a) An inspection exceedance count (IEC).

b) A rebuild and overhaul exceedance count (REC).

c) A operational exceedance count (EOC)

A

A) An inspection exceedance count (IEC).

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9
Q

The yellow arc on the Diamond J torquemeter represents

a) Maximum continuous.

b) Five minute takeoff power.

c) Five second transient limit.

A

B) Five minute takeoff power

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10
Q

After turning the battery on during preflight, you notice the torquemeter digital readout flashing twice per second. What does this mean?

a) There an exceedance from a past flight.

c) It is conducting a self-test, do not start the aircraft.

d) Data limit is full, maintenance needs to download the data and clear it for further use.

A

A) There an exceedance from a past flight.

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11
Q

On the Diamond J torquemeter; a condition greater that 120% results in

a) An inspection exceedance count (IEC).

b) A rebuild and overhaul exceedance count (REC).

c) A operational exceedance count (EOC)

A

B) A rebuild and overhaul exceedance count (REC).

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12
Q

The red dot on the Diamond J TOT gauge indicates

a) Maximum continuous operation.

b) Maximum transient temperature.

c) Maximum temperature for start.

A

C) Maximum temperature for start.

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13
Q

After power up, the Diamond J TOT gauge digital readout is flashing twice per second. What does this mean?

a) It is conducting a self-test, do not start the aircraft.

b) Data limit is full, maintenance needs to download the data and clear it for further use.

c) There is a stored exceedance from a past operations

A

C) There is a stored exceedance from a past operations

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14
Q

What two exceedances does the Diamond J TOT gauge record?

a) Start and shutdown.

b) Start and takeoff.

c) Start and flight operation.

A

C) Start and flight operation.

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15
Q

The engine oil pressure gauge is a wet oil gauge and operates without electrical bus power.

a) True.

b) False.

A

A) True.

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16
Q

The transmission oil pressure gauge is a wet oil gauge and operates without electrical bus power.

a) True.

b) False.

A

A) True.

17
Q

Warning lights are colored __________ and caution lights are colored __________.

a) Red; green.

b) Red; amber.

c) Amber; red.

A

B) Red; amber.

18
Q

The engine out audio (horn) is a/an

a) Continuous sound.

b) Doorbell type chime.

c) Intermittent sound.

A

C) Intermittent sound.

19
Q

The rotor low rpm audio (horn) is a/an

a) Continuous sound.

b) Doorbell type chime.

c) Intermittent sound.

A

A) Continuous sound.

20
Q

In addition to controlling the fuel valve, the fuel valve switch also control the operation of the left fuel boost pump.

a) True.

b) False.

A

A) True.

21
Q

In addition to controlling the fuel valve, the fuel valve switch also control the operation of the right fuel boost pump.

a) True.

b) False.

A

B) False.

22
Q

Regarding the engine anti-icing switch

a) Power is only provided to the solenoid when the switch is positioned to OFF.

b) In the event of total electrical failure, the system is fail-safe ON (no electrical power = engine anti-icing ON).

c) All are correct.

A

C) All are correct.

23
Q

The generator switch has the following positions:

a) OFF, GEN (ON), and RESET.

b) OFF and ON.

c) OFF, GEN, and FIELD.

A

A) OFF, GEN (ON), and RESET.

24
Q

The left position light is

a) White.

b) Red.

c) Green.

A

B) Red.

25
Q

The GOV RPM switch on the collective controls

a) The N1 governor linear actuator allowing for increasing or decreasing the N1 rpm

b) The droop compensator allowing for increasing or decreasing the rotor rpm.

c) The N2 governor linear actuator allowing for increasing or decreasing the N2 rpm.

A

C) The N2 governor linear actuator allowing for increasing or decreasing the N2 rpm.

26
Q

When using the defog blower, it is recommended that both VENT control knobs be pulled to full open.

a) True.

b) False.

A

A) True.

27
Q

It is recommended that the heating system not be used during takeoffs or landings.

a) True.

b) False.

A

A) True.

28
Q

The air conditioning system shall be turned off for the following emergencies:

a) Engine failure or engine overtemperature.

b) Generator failure or insufficient power.

c) All are correct.

A

C) All are correct.

29
Q

The fire extinguisher is located

a) To the left of the pilot on the forward side of the vertical control tube tunnel.

b) On the cabin floor to the right of the pilot seat.

c) No fire extinguisher installed.

A

A) To the left of the pilot on the forward side of the vertical control tube tunnel.

BH206L (14 decks)

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