Beechcraft Baron 58 - Page 151

BEECHCRAFTBaron 5B
Serial TH
773 and After
TAKE-OFF
WEIGHT
TO ACHIEVE POSITIVE SINGLE ENGINE
RATE-OF-CUMB AT LlFT·OFF
Section V
Performance
ASSOCIATED CONDITIONS
EXAMPLE
AIRPLANE
POWER
FLAPS
LANDING GEAR
INOPERATIVE PROPELLER
13000
12000
11000
10000
I-
w
~ 9000
~
~ 8000
::J
!::
~ 7000
«
~ 6000
::J
(J)
ffl 5000
a:
Q.
4000
3000
2000
1000
AIRBORNE
TAKE-OFF
UP
DOWN
FEATHERED
PRESSURE ALTITUDE
OAT
TAKE-OFF WEIGHT
5650 FEET
15°C
4850
SL
3000
3500 4000
4500 5000
5500
October 1976
WEIGHT rv POUNDS
5-21