Factors affecting Aircraft Performance Flashcards

1
Q

Aircraft Performance

A

Ability of your airplane to accomplish certain things that makes it useful for a certain purpose.
* e.g. Takeoff, Landing, Cruising etc…

  • To prevent inflight surprises
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2
Q

Factors Affecting Performance

A

Air Density
Weight
Wind
Aircraft performance (Runway)
Aircraft Configuration

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3
Q

Air Density

A

Biggest Aircraft Performance Factor
Airplane and Engine Performance depend on density.
* Wing, Engine & Propeller

Amount of air molecules in a given volume.
Layman’s term. “How thick the air is

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4
Q

Factors affecting Air Density

A

Altitude
Temperature
Humidity

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5
Q

Altitude, (Factors of Air Density)

A
  • “As altitude increases, density/pressure decreases” Due to gravity.
  • Air Becomes “thinner” as altitude is gained.
  • As altitude increases, air mass decreases resulting to the decrease in Pressure & Density

“Higher the altitude, the lesser the air density, the lesser your aircraft will perform”

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6
Q

Temperature (Factors of Air Density)

A
  • As temperature increases, air expands. If air expands, air density decreases.
  • As temperature decreases, air compresses. if air compresses, air density increases.

“Higher the temperature, the lesser the air density, the lesser your aircraft will perform”

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7
Q

Humidity (Factors of Air Density)

A
  • Amount of water vapor in the air.
  • The more humid, more water vapor and less air molecules.

“Higher the humidity, the lesser the air density, the lesser your aircraft will perform”

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8
Q

6 Kinds of Altitude?

A
  1. Indicated Altitude - altimeter reading.
  2. Calibrated Altitude - corrected for instrument and installation error.
  3. Absolute Altitude - height from the field elevation.
  4. True Altitude - height from the mean sea level.
  5. Pressure Altitude - altitude from the standard atmosphere pressure of 29.92 inHg.
  6. Density Altitude - Pressure Altitude corrected for non-standard temp.
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9
Q

Pressure Altitude

A
  • Altitude above the standard atmospheric
    pressure of 29.92 inHg.
  • Indicated altitude when the altimeter
    setting is set to 29.92 inHg.
  • Used in performance calculations.
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10
Q

Density Altitude

A
  • Pressure altitude corrected from
    non-standard temp.
  • Height/altitude measured in terms of the density of the air.
  • In layman’s term “Density Altitude is the Altitude the Aircraft Feels that it is Flying”

“Higher the Density Altitude, the lesser the air density, the lesser your aircraft will perform”

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11
Q

Effects of High-density altitude

A

Cancel the density and you’ll get high altitude. High altitude means.

  • Low Pressure
  • Hot Temperature
  • More Humid
  • Higher Elevation

LOW AIR DENSITY = Poor Performance

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12
Q

Effects of Low density altitude

A

Cancel the density and you’ll get low altitude. low altitude means.

  • High Pressure
  • Cold Temperature
  • Less Humid
  • Lower Elevation

HIGH AIR DENSITY = Better Performance

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13
Q

Effect of Low Air Density to our Airplane

A
  • There are less air molecules for interaction with the wing, therefore decreasing lift.
  • Same goes with the propeller, which is also an airfoil
  • There is less air for engine induction = Less Power Output
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14
Q

Altitude’s Effect on Air Density

A
  • Air is less dense as you gain altitude.
  • There is also a performance decrease due to thinner air.
  • There is however, ONE improvement. True Airspeed Increases
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15
Q

Why true airspeed increases at higher altitude?

A

True Airspeed (TAS), The speed which your aircraft is ACTUALLY flying in the air

  • How? Thinner air means less resistance, hence, less drag.
  • However, your aircraft still maintains the same Indicated Airspeed (IAS)
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16
Q

Aircraft Weight, (Factors Affecting A/C Performance)

A
  • More lift is required
  • A higher fuel burn
  • Longer takeoff distances
  • Slower Climb (Poor climb performance)
  • Less range
  • Higher approach and landing speeds
  • Longer landing distances
17
Q

Wind, (Factors Affecting A/C Performance)

A

Wind significantly affects aircraft performance, with speed and direction impacting flight path, fuel efficiency, and the difficulty of takeoff and landing, requiring pilots to make adjustments and plan accordingly.

18
Q

Take off Ground Roll

A

it is the distance an airplane will travel on the takeoff run from standing start until it leaves the ground

19
Q

Take off Distance

A

it is the distance for the airplane to clear a 50 ft. Obstacle from standing start

20
Q

Take Off Performance
(For Ground Roll/ Take Off Distance)

A

More Weight of Aircraft
* Increase Ground Roll/ Take off Distance

Higher Altitude
* Increase Ground Roll/ Take off Distance

Higher Temperature
* Increase Ground Roll/ Take off Distance

Wind
Headwind
* Decrease Ground Roll/ Take Off Distance

Tailwind
* Increase Ground Roll/ Take Off Distance

Runway Slope
Downslope Runway
* Decrease Ground Roll/ Take Off Distance

Upslope
* Increase Ground Roll/ Take Off Distance

Runway Surface
Soft ground / Unpaved / Dry grass
Increase Ground Roll/ Take off

21
Q

VX (Best angle of climb)

A
  • Most altitude gained for the least horizontal distance travelled
22
Q

VY (Best rate of climb)

A
  • Most altitude gained for the shortest amount of time
23
Q

Service ceiling

A
  • Aircraft will only climb at 100 feet per
    minute (fpm).
24
Q

Absolute ceiling

A
  • Aircraft cannot climb anymore
25
Landing Ground Roll
is the distance an airplane touched the ground to full stop
26
Landing distance
Distance required for an aircraft to overfly / clear a 50-foot obstacle and come to complete stop.
27
Landing Performance (For Ground Roll/ Landing Distance)
More Weight * Increase Ground Roll/Landing Distance High Altitude *Increase Ground Roll/ Landing Distance High Temperature * Increase Ground Roll/ Landing Distance Wind Headwind * Decrease Ground Roll/ Landing Distance Tailwind * Increase Ground Roll/ Landing Distance Runway Slope Downslope Runway * Increase Ground Roll/ Landing Distance Upslope * Decrease Ground Roll/ Landing Distance Soft ground / Unpaved / Dry Grass * Increase Ground Roll/ Landing Distance
28
Aircraft Configuration, (Factors Affecting A/C Performance)
Landing Gear * More drag Flaps * More drag * Shorter takeoff and landing roll Spoilers * More drag
29
Wake Turbulence - Wing Tip Vortices
The air flowing over the bottom surface tends to flow outward as well as rearward. * Greatest when: * Heavy (e.g. large airplane) * Clean Configuration (All Retracted) * Slow Flight (High angle of attack)
30
Ground Effect
It is the result of the interference of the surface of the earth with the airflow patterns about an airplane. The occurrence of ground effect is when an aircraft is about one wingspan and less on the ground,
31
Problems with ground effect during takeoff
An aircraft may be airborne at an indicated airspeed less than that normally required. In this case, the aircraft may become airborne initially with a deficiency of speed and then settle back to the runway.
32
Problems with ground effect during Landing
“Floating” effect may occur. Because of the reduced drag and power-off deceleration in ground effect, any excess speed at the point of flare may incur a considerable “float” distance.
33
Hydroplaning
The phenomenon of a tire skating along a thin film of water and not rotating.
34
Wind Correction Angle (WCA) =
“Difference between where the nose is pointed and where the airplane is traveling”
35
Performance charts usage
* WIND COMPONENT CHART * DENSITY ALTITUDE CHART * RATE OF CLIMB * TIME, FUEL, DISTANCE TO CLIMB * TAKE OFF DISTANCE * LANDING DISTANCE
36
Takeoff and Landing with a Crosswind
Highest direct crosswind value for an airplane during takeoff and landing ★ for pilots of average skill may safely operate in. * Cessna 152 = 12 knots.
37
What happens if maximum demonstrated crosswind component is exceeded?
An alternate airport is required.