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DISTANCE TO ACCELERATE STOP
VERSUS DECISION SPEED
4000
REGO MMENDED SAFE
3600
SING LE ENGINE
TAKE OFF SPEED
'"' 3200
"'
~
~
..
' " '
2800
~
Cl
~
Ul
2400
§
~
tl
~
2000
1600
1200
50
MINIMUM CONTROL SP EED
60
70
80
DECISION SPEED - KIAS
Cl\l.iTlON:
1.
Sa.le.' Contrnut!d Takeoff on
Sin~lc
Engine is Improbable
Belmt So.re: Single Engine Speed. (See Section Ill)
2.
Single J:.:nginC' Control 1s Improbable Uelow Minimum
Cun l r0 l Spc-('d,
Figure 6-5
90
CONDITIONS.
1.
Level Hard Surface Runway
2.
Wing Flaps - UP
3.
Full Throttle and 2700 RPM
Before Brake Release
4.
Mixture at Recommended fuel
Flow
5.
Engine Failure a't Dec1s1011
Speed
8.
lleavy Braklng After Engine
Failure
7.
Weight 5500 founds
B.
Sea Luvel Standard Day
6-5
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