Beechcraft Baron 58 - Page 154

TAKE-OFF
DISTANCE
-40 -30
-zo
·10 6 10 20 30 40 50
OUTSIDE
AIR
TEMPERATURE
",oc
5000
4000
t;
~
CJl
CJ)m
3000
~
.~._~
~
~~
0
-10
2000
~:D
.....
»
.....
."
1000
(0)-1
III
CJl
::I III
c. ..
»0
....
::1
"'01
~CXl
EXAMPLE:
"DC/)
OAT
is-c (59°FI
Gl Gl
PRESSURE ALTITUDE
5650 FEET
:l,n
TAKE-OFF
WEIGHT
5400 LBS
o :!'.
HEAD WIND COMPONENT
9.5 KNOTS
... 0
GROUND ROLL
'900
FEET
3 ::I
III
<
TOTAL OISTANCE OVER
::I
50 FT OBSTACLE
3090 FEET
n
TAKE-OFF SPEED AT
CD
LIFT-OFF B6 KTS
50 FT
94 KTS
6000
4ObO
0
'0
20 30 0
WIND COMPONENT OBSTACLE HEIGHT
'"
KNOTS '" FEET
5000 4500
WEIGHT
"'POUNDS
TAKE-OFF SPEEDS (ALL WEIGHTS)
LIFT-OFFB6 KNOTS
50 FEET94 KNOTS
.......
r
"
il
~
ASSOCIATED CONDITION
POWER TAKE-OFF POWER
MIXTURE LEAN TO
APPROPRIATE
FUEL FLOW
FLAPS uP
LANOING GEAR RETRACT AFTER POSITIVE
CLIMB ESTABLISHEO
COWL FLAPS OPEN
~
N
~
o
n
...
o
17
Gl
..
...
<0
.....
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