King Air 200 Powerplants

Question 1

The PT6A engine power section consists of:
A. One compression stage and four turbine stages.
B. A two-stage power turbine.
C. A two-stage turbine and a centrifugal compressor.
D. Twin-spool, two-stage turbines.

Answer 1

A. One compression stage and four turbine stages.

Question 2

The reduction gear system provides gear reduction:
A. For the propeller
B. Between the compressor and power turbine
C. For the aircraft accessory drive section
D. Between the compressor and the compressor turbine

Answer 2

A. For the propeller

Question 3

Max RPM in reverse?
 A. 1,900
 B. 2,200
 C. 1,830
 D. 2,000

Answer 3

A. 1,900

Question 4

During a ground start of the right engine, the R IGNITION ON annunciator must illuminate:
A. At 10% N1 rpm.
B. When the CONDITION lever is positioned to LOW IDLE.
C. At a stabilized 12% N1.
D. When the IGNITION AND ENGINE START switch is positioned to IGNITION and ENGINE START.

Answer 4

D. When the IGNITION AND ENGINE START switch is positioned to IGNITION and ENGINE START.

Question 5

When the AUTO–ENG–IGN switch is positioned to ARM, ignition is:
A. Continuous.
B. Inactive but armed if torque is greater than 400 foot-pounds.
C. Controlled by the stall warning system.
D. Continuous when torque is greater than 400 foot-pounds

Answer 5

B. Inactive but armed if torque is greater than 400 foot-pounds.

Question 6

After lift-off, if an autofeather is initiated, the immediate requirement is to:
A. Continue flying the aircraft and allow the propeller to feather.
B. Position the POWER lever to IDLE
C. Position the CONDITION lever to CUTOFF.
D. Reduce electrical loads.

Answer 6

A. Continue flying the aircraft and allow the propeller to feather.

Question 7

Which of the following is the most accurate definition of engine torque readout?
A. Power developed by the gas generator
B. Thrust supplied by the propeller
C. Ratio of compressor inlet to exhaust outlet
D. Power delivered to the propeller

Answer 7

D. Power delivered to the propeller