VMC Factors Flashcards

1
Q

Weight Increase

A

Vmc Decrease - Larger weight
component in horizontal
direction.

Performance Decrease

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2
Q

Aft CG

A

Vmc Increase - Rudder becomes less effective.

Performance Increase - Lower stall speed and higher cruise
speed.

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3
Q

Power Increase

A

Vmc Increase - Creates a greater rolling and yawing moment.

Performance Increase

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4
Q

Flaps Extended in Landing
Configuration

A

Vmc Decrease - Operating
engine creates more induced
airflow over the wing which
creates more lift, resulting in
more induced drag that
counteracts turning tendency.

Performance Decrease - Flaps increase drag.

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5
Q

Gear Extended

A

Vmc Decrease - Creates stabilizing effect.

Performance Decrease - Increases drag.

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6
Q

Windmilling Prop

A

Vmc Increase - Increases drag
due to propeller’s higher pitch
when feathered.

Performance Decrease - Increases drag.

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7
Q

Density Altitude Increase

A

Vmc Decrease - Engine produces less power resulting in less rudder required.

Performance Decrease - Less power available.

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8
Q

Sideslip

A

Vmc Increase - Airflow strikes
the rudder at a smaller angle,
vertical stabilizer blocks some
airflow. Relative wind strikes
vertical stabilizer from the side
pushing towards dead engine.

Performance Decrease - Increases drag.

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9
Q

Temperature Increase

A

Vmc Decrease - Engine produces less power resulting in less rudder required.

Performance Decrease- Less power available.

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10
Q

Cowl Flaps Open

A

Vmc Decrease - Small stabilizing effect.

Performance Decrease - Increases drag.

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11
Q

Critical Engine Inoperative

A

Vmc Increase - See critical
engine factors (PAST)

Performance Decrease - More drag due to greater rudder
deflection required.

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12
Q

Flaps in Takeoff Configuration

A

Vmc Increase - Operating engine
creates more induced airflow,
which creates more lift causing
the airplane to roll to the dead
engine.

Performance Increase?

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13
Q

List the VMC factors (12)

A

Weight
CG
Cowl Flaps
Gear
Takeoff Flaps
Landing Flaps

Windmilling Prop
Power
Critical Engine Failed

Density Altitude
Temperature

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