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32問 • 1年前

Via

通報

問題一覧

At which speed will increasing the pitch attitude cause an airplane to climb?

High speed.

At what speed, with reference to L/Dmax, does maximum rate-of-climb for a jet airplane occur?

A speed greater than that for L/Dmax.

What effect does an increase in airspeed have on a coordinated turn while maintaining a constant angle of bank and altitude?

The rate of turn will decrease resulting in no changes in load factor.

If no corrective action is taken by the pilot as angle of bank is increased, how is the vertical component of lift and sink rate affected?

Lift decreases and the sink rate increases.

What is the relationship of the rate of turn with the radius of turn with a constant angle of bank but increasing airspeed?

rate will decrease and radius will increase.

How can the pilot increase rate of turn and decrease the radius at the same time?

Steepen the bank and decrease airspeed.

Why must the angle of attack be increased during a turn to maintain altitude?

Compensate for loss of vertical component of lift.

Describe dynamic longitudinal stablitity.

Motion about lateral axis.

What is a characteristic of longitudinal instability?

Pitch oscillations becoming progressively greater.

Identify the type of stability if the aircraft remains in the new position after the controls have been neutralized.

Neutral longitudinal static stability.

Identify tge type of stability if the aircraft attitude tends to move farther from its original position after controls have been neutralized.

Negative static stability.

identify the type of stability if the aircraft tends to return to its original position after the controls have been neutralized.

Positive stativ stability.

What are some characteristics of an airplane loaded with the CG at the aft limit?

Lowest stall speed, highest cruise speed, and least stability.

What characteristic should exist if an airplane is loaded to the rear of its CG range?

Unstable about the lateral axis.

What effect does an uphill runway slope have upon takeoff performance?

Increases takeoff distance.

Which condition reduces the required runway takeoff?

Increased headwing component.

Which performance factor decreases as airplane gross weight increases, for a given runway?

Critical engine failure speed.

What effect does landing at high elevation airports have on groundspeed with comparable relative to temperature, wind, and airplane weight?

Higher that at low elevation.

Under which condition during the landing roll are the main wheel brakes at maximum effectiveness?

When wing lift has been reduced.

What should a pilot do to maintain "best range" airplane performance when a tailwind is encountered?

Decrease speed.

Which maximum range factor decreases as weight decreases?

Airspeed.

Which procedure produces the minimum fuel consumption for a given leg of the cruise flight?

Increase speed for a headwind.

At what speed, with reference to L/Dmax does maximum range for a jet airplane occur?

A speed greater than that for L/Dmax.

Maximum range performance of a turbojet aircraft is obtained by which procedure as aircraft weight reduces?

Increasing altitude or decreasing speed.

What is the reason for variations in geometric pitch along a propeller or rotor blade?

It permist a relatively constant angle of attack along its length when cruising flight.

Under normal operating conditions, which combination of MAP and RPM produce the most severe wear, fatigue, and damage to high performance reciprocating engines?

High RPM and low MAP.

What effect does high relative humidity have upon the maximum power output of modern aircraft engines?

Reciprocating engines will experience a significanrt loss of BHP.

Where is the critical altitude of a supercharged-reciprocating engine?

The highest altitude at which a desired manifold pressure can be obtained.

What is controlled by the waste gate of a turbocharged-reciprocating engine?

Exhaust gas discharge.

Under what condition should stalls never be practiced in a twin-engine airplane?

With one engine inoperative.

What does the blue radial line on the airspeed indicator of a light, twin-engine airplane represent?

Maximum single-engine rate of climb.

What performance should a pilot of a light, twin-engine airplane be able to maintain at Vmc?

Heading.

CPL HUMAN PERFORMANCE AND LIMITATIONS (1)

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78問 • 1年前

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CPL Radio Telephony (3)

Via · 20問 · 1年前

CPL Radio Telephony (3)

Met 1

Met 1

Met 2

Met 2

Met 3

Met 3

Met 4

Met 4

Met 5

Met 5

Met 6

Met 6

Met 7

Met 7

Met 8

Met 8

Human Performance 3

Human Performance 3

Met 9

Met 9

Met 10

Met 10

AGK 1

AGK 1

AGK 2

AGK 2

AGK 3

AGK 3

問題一覧

At which speed will increasing the pitch attitude cause an airplane to climb?

High speed.

At what speed, with reference to L/Dmax, does maximum rate-of-climb for a jet airplane occur?

A speed greater than that for L/Dmax.

What effect does an increase in airspeed have on a coordinated turn while maintaining a constant angle of bank and altitude?

The rate of turn will decrease resulting in no changes in load factor.

If no corrective action is taken by the pilot as angle of bank is increased, how is the vertical component of lift and sink rate affected?

Lift decreases and the sink rate increases.

What is the relationship of the rate of turn with the radius of turn with a constant angle of bank but increasing airspeed?

rate will decrease and radius will increase.

How can the pilot increase rate of turn and decrease the radius at the same time?

Steepen the bank and decrease airspeed.

Why must the angle of attack be increased during a turn to maintain altitude?

Compensate for loss of vertical component of lift.

Describe dynamic longitudinal stablitity.

Motion about lateral axis.

What is a characteristic of longitudinal instability?

Pitch oscillations becoming progressively greater.

Identify the type of stability if the aircraft remains in the new position after the controls have been neutralized.

Neutral longitudinal static stability.

Identify tge type of stability if the aircraft attitude tends to move farther from its original position after controls have been neutralized.

Negative static stability.

identify the type of stability if the aircraft tends to return to its original position after the controls have been neutralized.

Positive stativ stability.

What are some characteristics of an airplane loaded with the CG at the aft limit?

Lowest stall speed, highest cruise speed, and least stability.

What characteristic should exist if an airplane is loaded to the rear of its CG range?

Unstable about the lateral axis.

What effect does an uphill runway slope have upon takeoff performance?

Increases takeoff distance.

Which condition reduces the required runway takeoff?

Increased headwing component.

Which performance factor decreases as airplane gross weight increases, for a given runway?

Critical engine failure speed.

What effect does landing at high elevation airports have on groundspeed with comparable relative to temperature, wind, and airplane weight?

Higher that at low elevation.

Under which condition during the landing roll are the main wheel brakes at maximum effectiveness?

When wing lift has been reduced.

What should a pilot do to maintain "best range" airplane performance when a tailwind is encountered?

Decrease speed.

Which maximum range factor decreases as weight decreases?

Airspeed.

Which procedure produces the minimum fuel consumption for a given leg of the cruise flight?

Increase speed for a headwind.

At what speed, with reference to L/Dmax does maximum range for a jet airplane occur?

A speed greater than that for L/Dmax.

Maximum range performance of a turbojet aircraft is obtained by which procedure as aircraft weight reduces?

Increasing altitude or decreasing speed.

What is the reason for variations in geometric pitch along a propeller or rotor blade?

It permist a relatively constant angle of attack along its length when cruising flight.

Under normal operating conditions, which combination of MAP and RPM produce the most severe wear, fatigue, and damage to high performance reciprocating engines?

High RPM and low MAP.

What effect does high relative humidity have upon the maximum power output of modern aircraft engines?

Reciprocating engines will experience a significanrt loss of BHP.

Where is the critical altitude of a supercharged-reciprocating engine?

The highest altitude at which a desired manifold pressure can be obtained.

What is controlled by the waste gate of a turbocharged-reciprocating engine?

Exhaust gas discharge.

Under what condition should stalls never be practiced in a twin-engine airplane?

With one engine inoperative.

What does the blue radial line on the airspeed indicator of a light, twin-engine airplane represent?

Maximum single-engine rate of climb.

What performance should a pilot of a light, twin-engine airplane be able to maintain at Vmc?

Heading.