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
Summary of Contents for Cessna Grand Caravan Ex 208B
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