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.

17
Q

As humidity increases, air density ____________.

18
Q

As humidity increases, aircraft performance ____________.

19
Q

As humidity increases, air density ___________.

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
define density altitude
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
How do you determine total takeoff distance required?
Add takeoff distance plus landing roll!
27
Define Vy
Best rate of climb Greatest gain in altitude in the shortest possible time
28
Define Vx
Best angle of climb Greatest gain in altitude in the shortest horizontal distance
29
Define Vso
The power-off stalling speed or minimum steady flight speed Lower limit of white arc (stall speed with flaps LDG)
30
Define Vs1
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
Define Vfe
The highest airspeed permissible with the wing flaps in a prescribed extended position (t/o or LDG)
32
Define Va
The design maneuvering airspeed period this is the maximum speed at which the limit load can be imposed without causing structural damage. (106KIAS)
33
Define Vno
The maximum structural cruising speed or the maximum airspeed for normal operation.
34
Define Vne
The airspeed which should never be exceeded. If flight is attempted above this speed, structural damage or structural failure may result