WmB Flashcards

(36 cards)

1
Q

the ability of an aircraft to accomplish
certain things that make it useful for
certain purposes.

A

AIRCRAFT PERFORMANCE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Performance varies due to several factors such as

A

■ temperature
■ air density
■ weight
■ humidity

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Standard Temperature:

A

15°C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Standard Pressure:

A

29.92 “Hg or 1013.2 mb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Standard Temperature Lapse Rate:

A

1.98 °C/1000 feet up

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Standard Pressure Lapse Rate:

A

1 “Hg/1000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

the height above the standard datum plane (SDP).

A

PRESSURE ALTITUDE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

the vertical distance above sea level in the standard atmosphere at which a given
density is to be found.

A

DENSITY ALTITUDE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

As the density of the air increases, _________________________

A

aircraft performance increases.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

As the density of the air decreases, _________

A

aircraft performance decreases.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

“As density altitude increases, aircraft performance _______”

A

Decreases

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

It is directly proportional to
pressure.

A

Density

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

As pressure increases, density ___”

A

Increases

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

As temperature increases, density ____

A

Decreases

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

the amount of water vapor contained in
the atmosphere and is expressed as a percentage of the maximum amount of water
vapor the air can hold.

A

Humidity

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

As humidity increases, density ____”

17
Q

obtained when the power or thrust required equals
the maximum power or thrust available from the
powerplant.

A

Maximum level flight speed

18
Q

“As altitude increases, performance _______”

19
Q

It occurs when you have the greatest amount of flying time for the
least amount of fuel.

A

Maximum Endurance

20
Q

It occurs when you get the greatest distance for a given amount of fuel.

A

Maximum Range

21
Q

The amount of power that is applied to
the brakes without skidding the tires

A

Braking Effectiveness

22
Q

The amount of change in runway height over the length of the runway.

A

Runway Gradient or Slope

23
Q

This is a condition in which the aircraft
tires ride on a thin sheet of water rather
than on the runway’s surface.

24
Q

Effects of Increased weight on takeoff:

A

● higher lift-off speed
● greater mass to accelerate
● increased drag and ground friction

25
Effects of Increased weight on landing
● higher approach speed ● more runway used to decelerate ● wear and tear on brakes
26
Effects of takeoff (headwind)
- lower groundspeed needed to reach rotation speed - shorter ground roll
27
Effects of takeoff (tailwind)
higher groundspeed needed to reach rotation speed longer ground roll
28
Effects if landing (headwind)
○ less ground roll ○ ground speed is lower at touchdown
29
Effects of landing (tailwind)
○ increased landing roll ○ ground speed is higher at touchdown
30
Effects of T/O below rotation speed:
■ T/O below rotation speed: ● aircraft could stall ● difficult to control ● low initial rate of climb
31
Effects of T/O above rotation speed:
● improved initial rate of climb and “feel” of the aircraft ● increase in takeoff distance
32
Effects of Landing below specified speed
● aircraft may stall ● difficult to control ● develop high rates of descent
33
Landing above specified speed
● improves controllability slightly (especially in crosswinds) ● increase in landing distance
34
An increase in density altitude on takeoff:
● greater takeoff speed ● decreased thrust and reduced accelerating force
35
Increase in density altitude on landing:
● increased landing speed but does not alter retarding force
36
○ Examples of Performance Charts:
■ Airspeed Calibration ■ Temperature Conversion ■ Wind Component Chart ■ Density Altitude Chart ■ Takeoff Distance ■ Landing Distance ■ Rate of Climb ■ Time, Fuel, Distance to Climb ■ Range Profile ■ Endurance Profile