Beechcraft Baron 58 - Page 160

TAKE-OFF
CLIMB
GRADIENT
-
ONE
ENGINE
INOPERATIVE
ASSOCIATED CONDITIONS:
Cf'
N
co
o
g
0-
CD
..
...
CO
....
en
POWER
LANDING GEAR
FLAPS
INOPERATIVE
PROPELLER
TAKE-OFF
UP UP
FEATHERED
CLIMB SPEED (ALL
WEIGHTSI
94 KTS
-40 -30 -20 -10 0 10 20 30 40 50
OUTSIDE AIR
TEMPERATURE~oC
EXAMPLE
OAT
PRESSURE AL
TllUDE
WEIGHT
GRADIENT OF CLIMB CLIMB SPEED
6
4
;F.
(
....
z
w
is
..:
a:
o
III
0
:;;
:;
u
-1
-2
-3
-4
I'·
"'1"
I I I
5000
4500
4000
WEIGHT
~
POUNOS
15°C
5650
FT
4850
LBS
2.1%
94 KTS
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o
~.
..
0
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CD
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CD
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