Chapter 6 - Flight Characteristics Flashcards

1
Q

At aft centers of gravity, what is the pitch force required?

A

9 pounds per G

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2
Q

At forward centers of gravity, what is the pitch force required?

A

12 pounds per G

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3
Q

The trim rate of each axis changes with airspeed. (T/F)

A

False, trim rate is constant throughout the airspeed envelope of the aircraft

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4
Q

During speed break extension, what does elevator trim do? How?

A

Elevator is trimmed nose down

Due to the speed brake - elevator trim interconnect

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5
Q

What are the 3 factors that effect glide performance?

A
  1. Airspeed
  2. Configuration
  3. Coordination
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6
Q

What activates the stick shaker?

A

The AOA system

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7
Q

What is the minimum stall warning airspeed provided by the stick shaker?

A

5 knots

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8
Q

In all configurations, during power off stalls, the aircraft buffet occurs how many KIAS before stall?

A

3 KIAS

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9
Q

During an unaccelerated power-on stall, at what airspeed does the aircraft buffet occur prior to stall?

A

There is little perceptible buffer prior to the stall

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10
Q

With 100% torque, what nose attitude is possible during entry ot a wings level stall?

A

45 degrees

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11
Q

What is the defining characteristic of an upright, wings-level stall?

A

A roll-off or wing-drop, together with an increased buffet

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12
Q

During a wings-level power on stall, what is the tendency of the aircraft and why?

A

A left rolling tendency is induced at stall by engine torque before reaching full aft stick

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13
Q

Above what torque setting may it not be possible to prevent a left roll-off at a stall?

A

60%

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14
Q

What aggravates the roll-off stall tendency more, flaps or landing gear?

A

Flaps, landing gear have little effect on stall characteristics

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15
Q

Altitude loss from a wings level stall is usually less than what?

A

100 ft

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16
Q

What are the 4 independent factors that determine the amount of altitude lost during a dive recovery?

A
  1. Angle of dive
  2. Altitude at start of pullout
  3. Airspeed at star of pullout
  4. Acceleration maintained during pullout