Vne Flashcards
0
Q
Vno
A
Max structural cruising speed top of Green arc 155
1
Q
Vne
A
Never exceed 194
2
Q
Vle
A
Max speed with gear extended 194
3
Q
Vfe
A
Next flap extension speed top of White arc
Landing 111
approach 137
4
Q
Vse
A
Best rate of climb single engine
Blueline
82
5
Q
Vy
A
Best rate of climb
79
6
Q
Vx
A
Best angle of climb single engine
77
7
Q
Vx cruise
A
86
8
Q
Vr
A
Rotation
72
9
Q
Vs
A
Stall speed with zero flaps
Bottom of Green arc
62
10
Q
Vso
A
Stall speed in landing configuration
Bottom of white arc
56
11
Q
Vmc
A
Minimum controllable airspeed with critical engine inoperative
Redline 68 kts
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
13
Q
Vlo
Vloe
A
Max landing gear operation or extension 194 kts
14
Q
Stalling speed LDG flaps
A
Ldg flaps 1400 kg - 49 kts
Ldg flaps 1785 kg - 57 kts
15
Q
Stalling speed APP flaps
A
Vs
1400 - 53 kts
1785 - 61 kts
16
Q
stalling speed clean
A
Vs 1400 - 56
1785 - 64
17
Q
best glide flaps up
A
82 kts
18
Q
best angle of climb
A
Vx 79
19
Q
best rate of climb
A
Vy 79 kts
20
Q
best rate of climb one engine
A
Vyse 82 kts
21
Q
minimal control speed
A
Vmca 68
22
Q
minimal control speed for TRG
A
Vsse 82 kts
23
Q
minimum control speed in ice
A
Vmca in ice 72 kts
24
operating speed in ice
121 - 160 kts
25
cruising climb speed
86 kts
Higher-speed forward
Better visibility
Cooler engine
26
rotation speed
70 to 72 kts
27
max APP flap speed
Vfe 137 kts
28
Max LDG flap speed
Vfe 111 kts
29
Max landing gear extension
Vloe = 194
30
Max LG extended
Vle 194 kts
31
Max LG retraction
Vlor - 156 kts
32
Approach speed flaps up
Vref - 85 /86 kts
33
Approach Flaps APP
Vref - 82 kts
34
Approach flaps LDG
Vref - 76 / 78 kts
35
minimum go around speed flaps up
82 kts
36
Max cruising speed
Vno - 155
37
Never Exceed speed
Vne - 194 kts
38
maneuvering speed
Va - 120 / 126
39
What is Multi engine pilots priority during takeoff roll
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
Multi engine pilots second concern on takeoff
Obtain the best rate of climb speed (Vy) in the least amount of time
41
Service ceiling
Maximum density altitude where best rate of climb will be equal 100 feet per min at maximum weight
42
What Affects service ceiling
Weight
Pressure altitude
Temperature
43
Vsse
VSSE is specified by the airplane manufacturer in the new handbooks and is the minimum speed at which to perform intentional engine cuts.
44
accelerate-stop distance
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
accelerate-go distance
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
Before every takeoff - consider what factors
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
What are the four factors affecting climb out?
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
Vsse
VSSE is specified by the airplane manufacturer in the new handbooks and is the minimum speed at which to perform intentional engine cuts.
49
accelerate-stop distance
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
accelerate-go distance
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
Before every takeoff - consider what factors
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
What are the four factors affecting climb out?
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
Advantages of claim – cruise airspeed versus best-rate-of-climb
A. Better forward speed
B. Only small reduction in rate of climb
C. Increase for visibility
D. Better Engine cooling
54
What are the single – engine climb performance requirements for light twins
Simply determine the single engine claim at 5000 feet MSL. No requirements.
55
Service ceiling?
```
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
What is absolute service ceiling?
Maximum density altitude the airplane is capable of attaining or maintaining; also density altitude where Vx and Vy are equal
57
Define: single-engine-service-ceiling
Maximum density altitude at which the single-engine best rate of climb speed Vyse will produce 50 ft./m rate of climb
58
Define single-engine absolute ceiling
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
