V-speeds & AC Info Flashcards

1
Q

What is the normal climb out speed?

A

75-85

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2
Q

What is V-Y?

A

Best rate-of-climb

74

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3
Q

What is V-X?

A

Best angle-of-climb

62

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4
Q

What is V-FE?

A

Max flaps-down speed

85

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5
Q

What is V-SO?

A

Stall speed in normal landing configuration

40

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6
Q

What is V-S1?

A

the clean (flaps and gear up) stall speed

48

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7
Q

What is the approach to landing speed?

A

65-75

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8
Q

What is V-A?

A

Maneuvering speed

105

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9
Q

What is V-NE?

A

Never-exceed speed

163

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10
Q

What is V-NO

A

Maximum structural cruising speed

129

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11
Q

What engine-out glide speed will give you the maximum range?

A

68

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12
Q

What airspeed is used for a SHORT-field take off?

A

Rotate at 51

Climb at 56

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13
Q

Describe SHORT field take off procedure

A
Wing flaps 10°
Use all available runway
Brakes - apply
Throttle - FULL
Mixture - FULL RICH
Brakes - RELEASE
Elevator or Control - SLIGHTLY TAIL LOW
Rotate - 51
Climb - 56 (until all obstacles are cleared)
Wing flaps - RETRACT SLOWLY (when airspeed > 60)
Climb - Best Rate - 74
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14
Q

What airspeed is used for a SHORT-field landing?

A

61

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15
Q

Describe a SHORT-field landing.

A
Wing flaps - FULL
Airspeed - 61
Elevator Trim Control - ADJUST
Power - IDLE (as obstacle is cleared)
Touchdown - ON MAIN WHEELS FIRST
Brakes - APPLY (light to moderate)
Elevator Control - BACK (aerodynamic braking)
Wing Flaps - UP
Brakes - APPLY (as required)
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16
Q

What airspeed is used for a SOFT-field take off?

A

let airplane lift off when it’s ready & remain in ground effect

17
Q

Describe SOFT field take off procedure

A
Wing Flaps - 10°
Taxi onto runway with yoke back/no braking/wide turns
Trhottle - FULL
Elevator Control - TAIL LOW
Remain in GROUND EFFECT until after lift off
Climb - 62 (until all obstacles cleared)
Wing flaps - RETRACT SLOWLY
Climb - 74
18
Q

Describe a SOFT-field landing.

A
Wing flaps - FULL
Airspeed - 61
Elevator Trim Control - ADJUST
Power - JUST ABOVE IDLE 
Soft Touchdown - ON MAIN WHEELS FIRST
Brakes - APPLY (light to moderate)
Elevator Control - BACK (nose wheel up on rollout)
Brakes - NONE
19
Q

Describe the engine.

A

Textron Lycoming 180 BHP
Normally aspirated, direct drive, air-cooled
horizontally opposed, fuel injected