Beechcraft Baron G58 Pilot Operating Handbook page 237

Model G58
Interpolate for 11,500 ft and the temperature for the appropri-
ate route segment. Results of the interpolations are:
ROUTE
SEGMENT
LEG A-B
LEG C
LEG D
LEG E
Time and fuel used are calculated as follows:
Time = Distance ÷ Ground Speed
Fuel Used = (Distance ÷ Ground Speed) x Fuel Flow
Results are:
ROUTE
SEGMENT
LEG A
LEG B
LEG C
LEG D
LEG E
TOTAL
* Distance required to climb or descend has been subtracted
from segment distance.
July, 2014
ISA CONDITION
ISA + 3°C
ISA + 8°C
ISA + 17°C
ISA + 18°C
DISTANCE
NM
*30.5
40.0
74.0
87.0
*22.0
253.5
FUEL FLOW
PER ENG
GAL/HR
14.0
13.9
13.6
13.6
EST TIME AT
GROUND CRUISE
SPEED ALTITUDE
KNOTS HRS:MIN
224 :08.2
223 :10.8
182 :24.4
186 :28.1
188 :07.0
Section 5
Performance
TAS
KNOTS
196
196
197
197
FUEL
USED
CRUISE
GAL
3.8
5.0
11.3
12.7
3.2
1:19 36.0
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