Beechcraft Musketeer Sport III A23-19 Pilot Operating Handbook page 95

BEECHCRAFT Sport III
Musketeer A23-19, 19A
SectionV
Performance
Enter the CRUISE PERFORMANCE table for 2600 RPM at
9500 feet:
THROTTLE
ALTITUDE SETTING
FUEL FLOW
TAS
FEET RPM GPH
KNOTS
9500
2600
8 .3
111
Time and fuel used were calculated as follows :
Time
=
Distance
Ground Speed
Fuel Used
=
(Time) (Fuel Flow)
Results are:
FUEL
EST
TIME AT
USED
GROUNO CRUISE FOR
ROUTE
D 1STANCE
SPEED ALTITUDE CRUISE
SEGMENT NM KNOT S HRS: MIN GAL
DEN-TXC
72
108 0 :40 5.5
TXC-GLD
73
108 0:41 5.6
G LO -HUT 194 116 1:40 13 .9
HUT- ICT 28 113 0 :15 2.1
October 1979
5-5