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DA42 V speeds > Vne > Flashcards

Vne Flashcards

0
Q

Vno

A

Max structural cruising speed top of Green arc 155

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1
Q

Vne

A

Never exceed 194

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2
Q

Vle

A

Max speed with gear extended 194

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3
Q

Vfe

A

Next flap extension speed top of White arc
Landing 111
approach 137

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4
Q

Vse

A

Best rate of climb single engine
Blueline
82

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5
Q

Vy

A

Best rate of climb

79

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6
Q

Vx

A

Best angle of climb single engine

77

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7
Q

Vx cruise

A

86

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8
Q

Vr

A

Rotation

72

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9
Q

Vs

A

Stall speed with zero flaps
Bottom of Green arc
62

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10
Q

Vso

A

Stall speed in landing configuration
Bottom of white arc
56

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11
Q

Vmc

A

Minimum controllable airspeed with critical engine inoperative
Redline 68 kts

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12
Q

Va

A

Maneuvering speed above 3400 pounds 126
Up to 3400 pounds 120
Do not make full or abrupt control surface movements above the speed

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13
Q

Vlo

Vloe

A

Max landing gear operation or extension 194 kts

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14
Q

Stalling speed LDG flaps

A

Ldg flaps 1400 kg - 49 kts

Ldg flaps 1785 kg - 57 kts

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15
Q

Stalling speed APP flaps

A

Vs
1400 - 53 kts
1785 - 61 kts

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16
Q

stalling speed clean

A

Vs 1400 - 56

1785 - 64

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17
Q

best glide flaps up

A

82 kts

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18
Q

best angle of climb

A

Vx 79

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19
Q

best rate of climb

A

Vy 79 kts

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20
Q

best rate of climb one engine

A

Vyse 82 kts

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21
Q

minimal control speed

A

Vmca 68

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22
Q

minimal control speed for TRG

A

Vsse 82 kts

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23
Q

minimum control speed in ice

A

Vmca in ice 72 kts

24
Q

operating speed in ice

A

121 - 160 kts

25
Q

cruising climb speed

A

86 kts
Higher-speed forward
Better visibility
Cooler engine

26
Q

rotation speed

A

70 to 72 kts

27
Q

max APP flap speed

A

Vfe 137 kts

28
Q

Max LDG flap speed

A

Vfe 111 kts

29
Q

Max landing gear extension

A

Vloe = 194

30
Q

Max LG extended

A

Vle 194 kts

31
Q

Max LG retraction

A

Vlor - 156 kts

32
Q

Approach speed flaps up

A

Vref - 85 /86 kts

33
Q

Approach Flaps APP

A

Vref - 82 kts

34
Q

Approach flaps LDG

A

Vref - 76 / 78 kts

35
Q

minimum go around speed flaps up

36
Q

Max cruising speed

37
Q

Never Exceed speed

A

Vne - 194 kts

38
Q

maneuvering speed

A

Va - 120 / 126

39
Q

What is Multi engine pilots priority during takeoff roll

A

Obtain the single engine minimum control speed +5 kn prior to lift off to be able to control the aircraft if a single engine failure

40
Q

Multi engine pilots second concern on takeoff

A

Obtain the best rate of climb speed (Vy) in the least amount of time

41
Q

Service ceiling

A

Maximum density altitude where best rate of climb will be equal 100 feet per min at maximum weight

42
Q

What Affects service ceiling

A

Weight
Pressure altitude
Temperature

43
Q

Vsse

A

VSSE is specified by the airplane manufacturer in the new handbooks and is the minimum speed at which to perform intentional engine cuts.

44
Q

accelerate-stop distance

A

The accelerate-stop distance is the runway length required to accelerate to a specified speed (either VR or VLOF, as specified by the manufacturer), experience an engine failure, and bring the airplane to a complete stop

45
Q

accelerate-go distance

A

The accelerate-go distance is the distance required to accelerate to liftoff speed and, assuming failure of an engine at the moment initial liftoff speed is attained, to continue the takeoff on the remaining engine to a height of 50 feet.

46
Q

Before every takeoff - consider what factors

A

a. Weight and balance
b. Runway length, slope and contamination
c. Normal takeoff ground run distance
d. Ground run distance required to clear a 50- foot obstacle
e. Surrounding terrain and obstructions
f. Nearby emergency landing areas in the event of engine failure
g. Accelerate-stop and accelerate-go distance
h. Existing density altitude and single engine service ceiling
i. Alternate plan of action

47
Q

What are the four factors affecting climb out?

A

Airspeed—too little or too much will decrease climb performance.
Drag—created by gear, flaps, cowl flaps, propeller and airspeed.
Power— the amount available in excess of that needed for level flight.
Weight— passengers, baggage and fuel load greatly affect climb performance.

48
Q

Vsse

A

VSSE is specified by the airplane manufacturer in the new handbooks and is the minimum speed at which to perform intentional engine cuts.

49
Q

accelerate-stop distance

A

The accelerate-stop distance is the runway length required to accelerate to a specified speed (either VR or VLOF, as specified by the manufacturer), experience an engine failure, and bring the airplane to a complete stop

50
Q

accelerate-go distance

A

The accelerate-go distance is the distance required to accelerate to liftoff speed and, assuming failure of an engine at the moment initial liftoff speed is attained, to continue the takeoff on the remaining engine to a height of 50 feet.

51
Q

Before every takeoff - consider what factors

A

a. Weight and balance
b. Runway length, slope and contamination
c. Normal takeoff ground run distance
d. Ground run distance required to clear a 50- foot obstacle
e. Surrounding terrain and obstructions
f. Nearby emergency landing areas in the event of engine failure
g. Accelerate-stop and accelerate-go distance
h. Existing density altitude and single engine service ceiling
i. Alternate plan of action

52
Q

What are the four factors affecting climb out?

A

Airspeed—too little or too much will decrease climb performance.
Drag—created by gear, flaps, cowl flaps, propeller and airspeed.
Power— the amount available in excess of that needed for level flight.
Weight— passengers, baggage and fuel load greatly affect climb performance.

53
Q

Advantages of claim – cruise airspeed versus best-rate-of-climb

A

A. Better forward speed
B. Only small reduction in rate of climb
C. Increase for visibility
D. Better Engine cooling

54
Q

What are the single – engine climb performance requirements for light twins

A

Simply determine the single engine claim at 5000 feet MSL. No requirements.

55
Q

Service ceiling?

A 
Maximum density altitude where best rate – of – climb airspeed will produce 100 feet of climb with maximum weight in a clean configuration with maximum continuous power
Affected by
A. Weight
B. Pressure altitude
C. Temperature
56
Q

What is absolute service ceiling?

A

Maximum density altitude the airplane is capable of attaining or maintaining; also density altitude where Vx and Vy are equal

57
Q

Define: single-engine-service-ceiling

A

Maximum density altitude at which the single-engine best rate of climb speed Vyse will produce 50 ft./m rate of climb

58
Q

Define single-engine absolute ceiling

A
  1. Maximum density altitude the airplane is capable of attaining with the critical engine in opportunity and propeller feathered.
  2. when Vxse equal Vyse are equal 3. when yaw & stall speed are equal

DA42 V speeds (1 decks)

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