SECTION 5 CESSNA
PERFORMANCE MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
SAMPLE PROBLEM
The following sample flight problem utilizes information from the
various charts to determine the predicted performance data for a typical
flight of an airplane equipped with a cargo pod. A similar calculation
can be made for an airplane without a cargo pod using charts identified
as appropriate for this configuration. Assume the following information
has already been determined:
AIRPLANE CONFIGURATION (CARGO POD INSTALLED)
Takeoff weight 8600 Pounds
Usable fuel 2246 Pounds
TAKEOFF CONDITIONS:
Field pressure altitude 3500 Feet
Temperature 16°C (8°C Above Standard)
Wind component along runway 12 Knot Headwind
Field length 4000 Feet (Paved, Level, Dry
Runway)
CRUISE CONDITIONS:
Total distance 650 Nautical Miles
Pressure altitude 11,500 Feet
Temperature 8°C
Expected wind enroute 10 Knot Headwind
LANDING CONDITIONS:
Field pressure altitude 1500 Feet
Temperature 25°C
Wind component along runway 12 Knot Headwind
Field length 3000 Feet (Paved, Level, Dry
Runway)
208BPHCUS-00
5-4
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