A104 Airplane Performance Flashcards

1
Q

explain the effects of weight on aircraft performance

A

Any item onboard adding weight is undersirable, more weight decreases overall performance, more weight=higher takeoff speed, longer runway, longer landing, shorter range, etc

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2
Q

effects of balance on aircraft performance

A

Center of gravity, center of gravity limits, center of gravity range, total aircraft moment

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3
Q

Center of Gravity

A

the balance point of an aircraft, also the center of mass.

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4
Q

center of gravity limits

A

the specified forward and aft points along the longitudinal axis within which the CG must be located during flight to keep it predictable

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5
Q

center of gravity range

A

the distance between the forward and aft CG limits

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6
Q

Total aircraft moment

A

the total weight of the aircraft multiplied by the distance between the datum line and the location of the CG of the aircraft

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7
Q

datum line

A

an imaginary ine in inches whicih all arm measurements are taken

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8
Q

arm

A

the horizontal distance in inches from the reference datum line to the item

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9
Q

moment

A

the product of the weight of an item multiplied by its arm, expressed in in pound, can be positive or negative

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10
Q

Aft CG*

A

Stall Speed-Lower, Stability-lower,

Cruise speed- Higher

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11
Q

Forward CG*

A

Stall speed- Higher
Stability- Higher
Cruise Speed- Lower

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12
Q

explain how atmospheric conditions effect aircraft performance*

A

The lifting capability of an aircraft depends upon the design of the wing, the speed at which the wing moves through the air, and the density of air. Airplane performance depends upon the number of air molecules available around the aircraft

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13
Q

three characteristics of air

A

air pressure, temperature, humidity

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14
Q

air pressure*

A

when air pressure is high, you have better performance.

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15
Q

Pressure altitude*(don’t confuse with air pressure)

A

How high are you in the air

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16
Q

temperature

A

Higher temperature= lower performance because the molecules become more energetic and molecules are more separated

17
Q

humidity

A

Humid air weighs less than dry air. As humidity goes up aircraft performance goes down

18
Q

Describe the characteristics of standard altitude

A

Sea level Barometric pressure of 29.92, sea temperature of 15 degrees Celsius, relative humidity of 0 percent, standard temperature lapse rate of 2 degrees Celsius per 1000 feet and 1 in of mercury per 1000 feet

19
Q

Pressure altitude

A

is the height in the is a that corresponds to the currently sensed pressure around the aircraft

20
Q

Density Altitude

A

is pressure altitude corrected for variations in temperature, and equals pressure altitude in a standard atmosphere

21
Q

Performance speeds

A

Vspeeds (velocity)- speeds that define certain performance and/or limiting characteristics of an aircraft

22
Q

Vso

A

The power-off stalling speed or the minimum flight speed at which the airplane is controllable in the landing configuration

23
Q

Vs

A

the power-off stalling speed or the minimum steady flight speed at which the airplane is controllable in a specific configuration

24
Q

Vfe

A

the highest airspeed permissible with the wing flaps in a prescribed extended position. This is due to the air loads imposed on the structure of flaps

25
Q

Va

A

The design maneuvering airspeed. This is the maximum speed at which the limit load can be imposed without causing structural damage

26
Q

Vno

A

The maximum structural cruising speed or the max airspeed for normal operation

27
Q

Vne

A

The never exceed speed, may cause structural failure

28
Q

Indicated airspeed

A

The speed of the airplane as observed on the AI, the airspeed without correction

29
Q

true airspeed

A

the speed of the airplane relative to air mass in which it is flying. IAS is corrected for air density

30
Q

Ground speed

A

The speed of the airplane in relation to the ground over which it is flying. TAS corrected for winds

31
Q

Best Angle on climb (Vx)

A

The speed that delivers the greatest gain of altitude in the shortest possible horizontal distance

32
Q

Best rate of climb (Vy)

A

the speed that delivers the greatest gain in altitude in the shortest possible time(best glide speed)