Beechcraft Baron 58 - Page 158

CLIMB-TWO
ENGINE
(2-BLADE
PROPELLER)
(TH.l090
and
Mler)
CLIMB SPEED 104 KNOTS (ALL WEIGHTS)
-60
-50 -40
-30
-20
-10
0 10 20 30 40 50
OUTSIDE AIR TEMPERATURE _ "C
l:Xl
(l)m
(I)
m
~.
(")
~:I:
-4(")
:I:jJ
....
»
....
."
c.l-4
Ql
l:Xl
=' Ql
0.
..
»0
...='
"'C1I
~
ClO
"'0(1)
(I) (I)
::;.~
o _.
..
0
3 ='
~
<
£
18
16
14
12
10
~
8
~
15
6 «
a:
o
lD
:2
d
WC
11,500 FT
5352 LBS
500
~
1000
~ ~
4000
EXAMPLE:
RATE OF
CLIMB.
. . . 500 FTlMIN
CLIMB
GRADIENT.
.....
4%
2500 2000
OAT..
PRESSURE ALTITUDE ..
WEIGHT.
"+1
5000 4500
WEIGHT - POUNDS
L .....
a+
..
'
R
---r-
60
+-i---!
FULL THROTTLE AT 2550 RPM
UP
UP
OPEN
LEAN TO APPROPRIATE
FUEL FLOW
ASSOCIATED CONDITIONS:
POWER ..
FLAPS..
LANDING GEAR.
COWL FLAPS .
MIXTURE.
...
CQ
u:l
C1I
N
al
l:Xl
g>
~
3
e-
(I)
."