Performance Flashcards

(13 cards)

1
Q

How does temperature affect air density and performance?

A
  • Higher temperature reduces air density
  • Decreases lift, engine power, and propeller efficiency
  • Increases takeoff and landing distances
  • Falls climb rate

Higher temperatures lead to worse performance due to reduced air density.

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2
Q

What is the effect of lower barometric pressure on air density?

A
  • Reduces air density
  • Same effects as high temperature

Low-pressure systems and higher field elevation contribute to reduced air density.

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3
Q

How does humidity impact air density and performance?

A
  • Moist air is less dense than dry air
  • Slightly reduces performance
  • Cumulative effect with heat and altitude

Increased humidity has a small but notable impact on performance.

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4
Q

What is density altitude?

A

This is one of the most important concepts for a pilot to understand, as it directly relates to aircraft performance and safety.

In simple terms, Density Altitude is the altitude the airplane feels like it’s at.

Think of it as the “performance altitude.” If you are at an airport with a field elevation of 5,000 feet, but it’s a very hot day, your Density Altitude might be 8,000 feet. This means your airplane will perform as if it’s at 8,000 feet, not 5,000.

The technical definition is: Pressure altitude corrected for non-standard temperature.

Higher density altitude indicates worse performance.

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5
Q

What three values are needed to find today’s density altitude?

A
  • Airport elevation
  • Altimeter setting
  • Outside air temperature (OAT)

These values are essential for calculating density altitude.

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6
Q

What is the formula for manual approximation of pressure altitude?

A

Pressure altitude ≈ field elevation + (29.92 − altimeter) × 1000 ft

This formula helps estimate pressure altitude based on field elevation and altimeter setting.

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7
Q

To compute density altitude, what should you add for each °C above standard temperature?

A

Add ≈ 120 ft to the pressure altitude

Standard temperature is approximately 15°C at sea level, decreasing ~2°C per 1000 ft.

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8
Q

What are the three segments to evaluate for total distance to clear a 50-ft obstacle on takeoff?

A
  • Ground roll (takeoff roll)
  • Rotation and airborne acceleration to safe climb speed
  • Obstacle clearance distance after lift-off

Each segment is crucial for performance planning during takeoff.

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9
Q

What does the POH chart indicate about the distance to clear a 50 ft obstacle?

A

It tells you where the airplane will be when it reaches 50 ft above the runway

The chart’s distance reflects exact conditions like weight, flaps, wind, and density altitude.

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10
Q

What should you do if your conditions are worse than those in the POH chart?

A

Expect the actual distance to be longer than the POH value

Higher density altitude, tailwind, higher weight, or contaminated runway will increase the distance needed.

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11
Q

What is a practical checklist for flight planning?

N
W
K
R
A
F
T

A
  • Gather runway length, slope/condition
  • Surface wind component
  • Airport elevation, altimeter setting, OAT
  • Airplane weight, flap setting
  • POH performance charts

NOTAMS
WEATHER**
KNOWN TRAFFIC DELYAS
RUNWAY LENGTHS
ALTERNATES
FUEL REQUIREMENTS
T/O LANDING DISTANCES

This checklist helps ensure all factors are considered for safe takeoff planning.

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12
Q

What safety margin is commonly added during flight planning?

A

Commonly 50% margin for unknowns or higher single-pilot risk

This margin helps account for uncertainties in performance calculations.

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13
Q

What should you decide if the POH total distance exceeds available runway or obstacles?

A

Do not attempt the takeoff

Safety is paramount; ensure adequate runway length and obstacle clearance.

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