Density Altitude Flashcards

1
Q

Air density is affected by what 3 factors

A
  1. Pressure
  2. Temperature
  3. Humidity
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2
Q

The main 2 concerns affecting aircraft performance due to air density are;

A
  1. Engine power output
  2. Aerodynamic lift
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3
Q

What are the pressures (hPa) for the following levels

Sea Level
5000
10,000
20,000
30,000
35,000

A

Sea Level - 1013
5000 - 840
10,000 - 700
20,000 - 466
30,000 - 300
35,000 - 240

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4
Q

Marry up the following pressures (hPa) to the correct level

1013
840
700
466
300
240

A

Sea Level - 1013
5000 - 840
10,000 - 700
20,000 - 466
30,000 - 300
35,000 - 240

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5
Q

Air density is DIRECTLY or INVERSELY proportional to atmospheric pressure

A

DIRECTLY

Less pressure = less dense air

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6
Q

Air density is DIRECTLY or INVERSELY proportional to Altitude

A

INVERSELY

MORE altitude = LESS dense

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7
Q

In the troposphere, what is the standard temperature lapse rate

A

(minus) -1.98 ℃
Per 1000 ft

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8
Q

Air is MORE or LESS dense with increase in temperature

A

LESS

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9
Q

Density altitude is impacted more by which affect;
1. Increase in altitude
2. Decrease in temperature

A

INCREASE IN ALTITUDE

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10
Q

Air with the highest moisture content is typically found at what altitude and what temperature

A
  1. LOW altitude
  2. GREATER temperature
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11
Q

A defined standard atmosphere is required for what 4 reasons

A
  1. Performance calculations
  2. Traffic Separation
  3. Expected temperatures at altitude
  4. Baseline (for forecasts)
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12
Q

What is the pressure lapse rate, and up to what altitude

A
  1. -1 hPa per 30 ft
  2. 20,000 ft
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13
Q

POH performance figures are based on what atmospheric conditions

A

ISA CONDITIONS

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14
Q

Air Density affects

Why does air density have an affect on engine power

A

LESS oxygen in air to mix with fuel

Less dense air means less oxygen to mix with fuel, meaning less power to engine

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15
Q

Air Density affects

Why does less dense air have an affect on aerodynamic lift

A

LESS dense air means LESS lift

Less dense air requires more physical speed from the aircraft to produce the same lift than in more dense air. Thus, at higher altitude, TAS is faster than at lower altitude, but IAS would be the same

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16
Q

When calculating for density altitude;

What 2 correction steps need to be carried out

A
  1. Differences in ISA atmopsheric pressure at altitude
  2. Differences in ISA air temperature at altitude
17
Q

Define the difference between PRESSURE altitude and DENSITY altitude

A
  1. PRESSURE altitude is the altitude we would be at under ISA conditions i.e. 1013 hPa
  2. DENSITY altitude is the altitude level the aircraft will perform as based on temperature and pressure corrections, irrespective of actual altitude

Example, An aircraft in ISA conditions at 10,000 ft will have better performance than an aircraft at 10,000 ft but where the temperature is +10℃ warmer. This is because the air is warmer. Warmer air is less dense, less dense air means less oxygen to mix with the fuel so less performance

18
Q

Calculate the difference in pressure altitude

Flying at 4,300 ft with 1032 set on the subscale, what is the pressure altitude

A

Pressure Alt - ISA Alt
1032 - 1013 = 19 hPa
Lapse rate 1 hPa = 30 ft
19 x 30 = 570 ft
4300 - 570 = 3,730 ft

REMEMBER:
Wind off pressure, Wind off altitude
Wind on Pressure, Wind on Altitude