Performance, Limitations, & factors that affect them

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21 Terms

1
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Define Performance

The action or process of carrying out or accomplishing an action, task, or function

2
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What factors (limitations) are most affected by performance?

  • T/O & LDG distance

  • Climb rate/ Ceiling

  • Payload

  • Range

  • Speed

  • Maneuverability

  • Stability

  • Fuel burn

3
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What are some things about an Airport Environments Runways & Layout that would affect performance?

Whats the runway surface made of?

  • Any surface that is not hard and smooth increases ground roll

  • Braking Effectiveness 

    • Soft surfaces slow an aircraft much faster than smooth and slick surfaces

    • Wet runways reduce braking effectiveness and can result in hydroplaning 

  • Runway Gradient: The change in height over the length of the runway, expressed as a percentage

  • Runways available based on wind conditions

4
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What are some things about an Airport Environments Surrounding Terrain & Obstacles that would affect performance?

Various Obstacles including towers, buildings, construction equipment, Trees?

  • Can the aircraft clear the obstacles based on the specific conditions?

  • Is a max angle versus max rate of climb required

  • Are there specific noise abatement or climb rate procedures requiring specific performance

5
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Differences between calculated & actual performance?

Even with having all the numbers, your pre-flight calculations will never be perfect

  • Stick to the POH only for any aircraft specific calculations needed

  • We plan for set configurations for a flight, deviating from that could mean less performance

6
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What factors does weight & balance directly affect with the aircraft?

  • Weight affects Performance

  • Balance affects Stability

7
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What are some affects increasing weight has on the aircraft T/O & LDG?

  • Higher T/O & LDG speed

  • Longer T/O run & LDG roll

  • Reduced rate and angle of climb

8
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What are some affects increasing weight has on the aircraft cruise performance?

  • Lower maximum altitude

  • Slower cruise speed

  • Reduced range & Increased fuel consumption

9
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What are some effects of overloading the weight of the aircraft?

  • Degraded climb performance

    • May not even be able to takeoff

  • Overheating during climbs

    • Added wear on engine parts

  • Over stressing the aircraft

10
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How does CG affect an aircraft's controllability?

Stability & controllability have an inverse relationship:

  • As stability increases, the control forces required to overcome that stability become greater, meaning controllability decreases.

11
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What are the effects on Stability & Controlability with a to far forward CG?

  • Problems controlling and raising the nose, especially at low airspeeds (takeoff and landing)

  • “Heavier” and consequently slower than the same airplane with a further aft CG

    • Requires a higher AOA to maintain altitude, resulting in more drag which produces a higher stalling speed

  • More controllable in a stall

    • The longer arm from the CG makes the elevator more effective

      • The nose heavy loading results in a tendency for the nose to drop, or assist in breaking the stall

<ul><li><p><span>Problems controlling and raising the nose, especially at low airspeeds (takeoff and landing)</span></p></li><li><p><span><strong>“Heavier”</strong> and consequently slower than the same airplane with a further aft CG</span></p><ul><li><p><span>Requires a higher AOA to maintain altitude, resulting in more drag which produces a higher stalling speed</span></p></li></ul></li><li><p><span><strong>More controllable</strong> in a stall</span></p><ul><li><p><span>The longer arm from the CG makes the elevator more effective</span></p><ul><li><p><span>The nose heavy loading results in a tendency for the nose to drop, or assist in breaking the stall</span></p></li></ul></li></ul></li></ul><p></p>
12
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What are the effects on Stability & Controlability with a to far Aft CG?

  • It produces very light control forces which makes it very easy to over-stress the airplane

  • “Lighter” and consequently faster than the same airplane with a more forward CG

    • Less back pressure & lower AOA needed to maintain altitude

    • Lower AOA = Less drag, & produces a Lower stall speed

  • Less controllable in a stall/spin

    • Due to the shorter arm of the CG to the elevator

      • Greater deflection is required to produce the same result as with a farther forward CG

        • Can lead to a Flat spin

<ul><li><p><span>It produces very light control forces which makes it very easy to over-stress the airplane</span></p></li></ul><ul><li><p><span><strong>“Lighter”</strong> and consequently faster than the same airplane with a more forward CG</span></p><ul><li><p><span>Less back pressure &amp; lower AOA needed to maintain altitude</span></p></li><li><p><span>Lower AOA = Less drag, &amp; produces a <strong>Lower stall speed</strong></span></p></li></ul></li><li><p><span><strong>Less controllable</strong> in a stall/spin</span></p><ul><li><p><span>Due to the shorter arm of the CG to the elevator</span></p><ul><li><p><span>Greater deflection is required to produce the same result as with a farther forward CG</span></p><ul><li><p>Can lead to a Flat spin</p></li></ul></li></ul></li></ul></li></ul><p></p>
13
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What are the effects on Stability, Controlability, & CG with a Laterally Loaded Aircraft?

Unbalanced loading can have adverse effects 

  • Trim, or maintain constant control pressure

    • Increases drag, decreases efficiency

14
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When is Parasite drag most prevalent?

At higher airspeeds

  • More air moving over uneven surface of aircraft

<p>At higher airspeeds</p><ul><li><p>More air moving over uneven surface of aircraft</p></li></ul><p></p>
15
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When is Induced drag most prevalent?

At low airspeeds

  • Lower AOA & smaller Vortices

<p>At low airspeeds</p><ul><li><p>Lower AOA &amp; smaller Vortices</p></li></ul><p></p>
16
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Define Thrust

Force or pressure exterted on an object

17
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Define Power

A measurement of the rate of performing work &/or transferring NRG

  • Horsepower or kilowatts

18
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Define Angle of Climb (AOC)

Comparison of altitude gained relative to distance traveled

  • Vx is used for this performance

19
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Define Rate of Climb (ROC)

Comparison of Altitude gained relative to the time needed to reach that altitude

  • Vy is used for this performance

20
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Range VS Endurance?

Range

  • Amount of distance you can travel

Endurance

  • Amount of time you can stay in the air

21
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What are the dangers of exceeding aircraft limitations?

  • Needing more runway than is available for T/O or LDG

  • Not enough performance to clear any obstacles

  • Not having enough fuel to reach your destination

  • Damage caused by exceeding strucural or aerodynamic limits

  • Loss of control for T/O & LDG by exceeding Max crosswind component