Beechcraft Baron 58 - Page 161

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5650 FT
11500
FT
5400
lBS
(22·7)
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{12.7-4.71 -;:8 GAL
{55·17l
= 38 NM
40
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EXAMPLE.
QAT AT TAKE-OFF
QAT AT CRUISE
AIRPORT PRESSURE
ALTITUDE
CRUISE PRESSURE
ALTITUDE
INITIAL CUMB WEIGHT
TIMETO CLIMB
FUEL TO CLIMB
DISTANCE TO CLIMB
I I 1 I I I I
II
o 10 20 30 40 50 60 70 80
DISTANCE TO
CUMBrvN
M
I1III1111
TTrTTl
II
I
o 2 4 6 8 10 12 14 16
FUEL TO
CLIMB'"
GALS
t t
l~=~:~:::~~~;::;~:~~~L
CLIMB SPEED 139 KNOTS
-50 -40
30 -20 -10 0 '-0 20 30 40 50 0 10 20 30
OUTSIDE AlA
TEMPERATUAE"'oC
TIME TO
CUMBrvM1NUTES
t t
TIME,
FUEL
AND
DISTANCE
TO
CLIMB
ASSOCIATED CONDITIONS
POWER 25 IN, HG OR
FULL
THROTIlE.
2500
RPM
FUEL DENSITY 6.0
LB;GAl
MIXTURE LEAN TO APPROPRIATE FUEL
FLOW
COWL FLAPS CLOSED
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