A104 Flashcards

1
Q

As weight increases, aircraft performance _____________.

A

Decreases

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2
Q

Define useful load

A

The variable weight—pilot, passengers, baggage, usable fuel

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3
Q

Define center of gravity

A

The balance point on an aircraft

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4
Q

In weight and balance calculations, what is the arm?

A

The distance from the datum line to the item

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5
Q

Define datum line

A

An imaginary vertical plane which all measurements are taken from

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6
Q

What affects does an aft CG have in relation to stall speed, stability, and cruise speed?

A

Stall speed: lower (flies at a lower angle of attack because of the additional downward force on tail)

Stability: less stable (elevator has a shorter arm from CG, requiring greater deflection to produce same result)

Cruise speed: higher cruise speed (less downward force on tail which requires less lift which in turn creates less drag)

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7
Q

What effects does a forward CG have on stall speed, stability, and cruise speed?

A

Stall speed: higher indicated stall speed (total lift increased with higher angle of attack which increases drag)

Stability: more stable (elevator has longer arm which will require less deflection to produce same results)

Cruise speed: slower cruise speed (more lift required, higher angle of attack, more drag)

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8
Q

define moment

A

The product of the weight multiplied by the arm

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9
Q

Where is the air most dense?

A

Sea level (close to ground)

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10
Q

How does air density affect performance?

A

Greater density, better performance

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11
Q

What main three environmental conditions affect aircraft performance?

A

Air pressure, temperature, humidity

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12
Q

Increase in air pressure causes a(n) ___________ in air density.

A

Increase

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13
Q

Higher air temperature equals _____________ air density

A

Lower

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14
Q

What affect does high temperature have in aircraft performance?

A

Lower aircraft performance

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15
Q

Define humidity

A

Amount of water vapor in the air

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16
Q

Water vapor is ___________ than air.

A

Lighter

17
Q

As humidity increases, air density ____________.

A

Decreases

18
Q

As humidity increases, aircraft performance ____________.

A

Decreases

19
Q

As humidity increases, air density ___________.

A

Decreases

20
Q

What altitude and pressure, temp, humidity levels are best for aircraft performance?

A

Sea level, high pressure, low temps, low humidity

21
Q

What is pressure altitude?

A

Pressure altitude tells you how high you have to fly to have the same pressure you have now

**Height above the standard datum plane

What altitude the plane feels like it’s flying at based off atmospheric conditions

22
Q

What is the standard temperature lapse rate?

A

Increase in 1000ft = decrease by 2 degrees Celsius

23
Q

What is the standard pressure lapse rate?

A

Increase in 1000ft = decrease in 1in mmHg

24
Q

How do you determine the pressure altitude when preparing preflight?

A

Apply correction factor (added or subtracted) to the known field elevation.

25
Q

define density altitude

A

The pressure altitude corrected for non-standard temperature

Based off the temp, how will this affect the aircraft performance?

Increases temp decreases air density which decreases aircraft performance

26
Q

How do you determine total takeoff distance required?

A

Add takeoff distance plus landing roll!

27
Q

Define Vy

A

Best rate of climb

Greatest gain in altitude in the shortest possible time

28
Q

Define Vx

A

Best angle of climb

Greatest gain in altitude in the shortest horizontal distance

29
Q

Define Vso

A

The power-off stalling speed or minimum steady flight speed

Lower limit of white arc (stall speed with flaps LDG)

30
Q

Define Vs1

A

The power-off stalling speed or the minimum steady flight speed at which the aeroplane is controllable in a specified configuration. (stall speed with flaps - cruise)

31
Q

Define Vfe

A

The highest airspeed permissible with the wing flaps in a prescribed extended position (t/o or LDG)

32
Q

Define Va

A

The design maneuvering airspeed period this is the maximum speed at which the limit load can be imposed without causing structural damage.

(106KIAS)

33
Q

Define Vno

A

The maximum structural cruising speed or the maximum airspeed for normal operation.

34
Q

Define Vne

A

The airspeed which should never be exceeded. If flight is attempted above this speed, structural damage or structural failure may result