Aircraft Performance Flashcards

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1
Q

Main elements of aircraft performance

A
Takeoff and Landing distance
Rate of Climb
Ceiling
Payload
Range
Speed
Fuel Economy
Maneuverability
Stability
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2
Q

What factors affect performance during takeoffs and landings?

A
Air density (density altitude)
Surface wind
Runway Surface
Slope of runway
Weight
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3
Q

How does increased weight affect takeoff and landing?

A

Higher liftoff speed
Greater mass to accelerate
Increased retarding force (friction, drag)
Longer takeoff distance

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4
Q

What effect does an increase in density altitude have on takeoff and landing?

A

Increased takeoff distance (great TAS req’d)
Reduced rate of climb (decreased thrust)
Increased true airspeed on approach and landing
Increased landing roll distance

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5
Q

Density Altitude

A

pressure altitude corrected for non-standard temperature. the vertical distance above sea level in the atmosphere at which a given density is found

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6
Q

How does air density affect performance?

A

Direct effect on: lift produced, power output of engine, propeller efficiency, drag forces

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7
Q

What factors affect air density?

A

Altitude: the higher the alt, the less dense the air
Temp: the warmer the air, the less dense it is
Humidity: more humid air is less dense

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8
Q

How does temperature, altitude and humidity affect density altitude?

A
  • Density altitude increases (low air density) with higher temp, altitude and humidity
  • Density altitude decreases (high air density) with lower temp, altitude and humidity
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9
Q

Vso

A

Stall speed in landing configuration (37 KIAS)

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10
Q

Vs1

A

Stall speed clean configuration (41 KIAS)

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11
Q

Vy

A

Best rate of climb (62 KIAS)

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12
Q

Vx

A

Best angle of climb (57 KIAS)

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13
Q

Vle

A

Max landing gear extension speed

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14
Q

VLO

A

Max landing gear operating speed

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15
Q

Vfe

A

Max flaps extended (100, 85, 70 KIAS)

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16
Q

Va

A

Maneuvering Speed - max speed at which limit load factor can be imposed without causing structural damage (102 KIAS)

17
Q

Vno

A

normal operating speed. max cruise speed. above this speed, exceeding load factor may permanently damage structure (124 KIAS)

18
Q

Vne

A

Never exceed speed. Only in smooth air. Above this speed structural damage may occur (148 KIAS)

19
Q

Define pressure altitude and explain why it is important

A

Indicated indicated when the altimeter setting window is adjusted to 29.92. (theoretical plane where air pressure equals 29.92) Pressure altitude is used to compute density altitude, true altitude, true airspeed and other performance data

20
Q

True altitude

A

Height above mean sea level

21
Q

Absolute Altitude

A

Height above ground level