SECTION 5 CESSNA
PERFORMANCE MODEL T182T NAV III
GFC 700 AFCS
U.S.
SAMPLE PROBLEM
The following sample flight problem utilizes information from the
various charts to determine the predicted performance data for a typical
flight. Assume the following information has already been determined:
(Continued Next Page)
AIRPLANE CONFIGURATION:
Takeoff weight 3100 Pounds
Usable fuel 87.0 Gallons
TAKEOFF CONDITIONS:
Field pressure altitude 3500 Feet
Temperature 24°C (16°C Above Standard)
Wind component along runway 12 Knot Headwind
Field length 3500 Feet
CRUISE CONDITIONS:
Total distance 450 Nautical Miles
Pressure altitude 11,500 Feet
Temperature 8°C
Expected wind enroute 10 Knot Headwind
LANDING CONDITIONS:
Field pressure altitude 3000 Feet
Temperature 25°C
Field length 3000 Feet
T182TPHBUS-00
5-4
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