SECTION 5
CESSNA
PERFORMANCE
MODEL 172S NAV III
KAP 140 AUTOPILOT
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:
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AIRPLANE CONFIGURATION:
Takeoff weight
2550 Pounds
Usable fuel
53.0 Gallons
TAKEOFF CONDITIONS:
Field pressure altitude
1500 Feet
Temperature
28°C (16°C Above Standard)
Wind component along runway
12 Knot Headwind
Field length
3500 Feet
CRUISE CONDITIONS:
Total distance
360 Nautical Miles
Pressure altitude
7500 Feet
Temperature
16°C (16°C Above Standard)
Expected wind enroute
10 Knot Headwind
LANDING CONDITIONS:
Field pressure altitude
2000 Feet
Temperature
25°C
Field length
3000 Feet
172SPHAUS-05
5-4
For
Training
Purposes
Only
Summary of Contents for Cessna 172S NAV III Skyhawk SP
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