Beechcraft Baron 58 - Page 155

ACCELERATE - STOP DISTANCE
WEIGHT'"
POUNDS
DECISION SPEED 'ALL WEIGHTS'
86 KNOTS
"tI
aI
=:'m
o aI
~ n
3
=.
I» 0
::s
::s
~
<
mID
<Dm
~.
m
e!.o
-I:::t
:::to
,,:0
":J>
~:!1
::s
ID
0.1»
:J>~ ~o
..
::S
<DOl
~
co
15°C
5650
FT
5400 LBS
9.5 KTS
3960
FT
B6 KTS
6000
5000
3000
ACCELERATE - STOP DiSTANCE
DECISION SPEED
liAS}
EXAMPLE
OAT
PRESSURE ALTITUDE
TAKE·OFF WEIGHT
HEADWIND
2000
- I I I
4000 0 10 20 30
WIND COMPONENT
~KNOTS
t:
Eff±l±±!!!fillIlll~UlUB
7000
~
t;;
o
z
«
o
w
W
Q.
Ul
Z
o
in
U
w
o
~
w
!;t
a:
w
..J
W
U
~
~
w
U
Z
~
15
4500
5000-40 -30 -20 -10 0 10 20 30 40 50
OUTSIDE AIR TEMPERATURE'"°C
..
ASSOCIATED CONDITIONS:
POWER 1.TAKE-OFF POWER
2. ENGINE IDLE AT DECISION SPEED
FLAPS UP
COWL FLAPS OPEN
0'1
I
N
0'1
o
n
..
o
cr
<D
~
...
CO
"
(I)