Sample Problem - Cessna SKYCATCHER 162 Pilot's Operating Handbook And Flight Training Supplement

SECTION 5
PERFORMANCE

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:
AIRPLANE CONFIGURATION:
Takeoff weight
Usable fuel
TAKEOFF CONDITIONS:
Field pressure altitude
Temperature
Wind component along runway
Field length
CRUISE CONDITIONS:
Total distance
Pressure altitude
Temperature
Expected wind enroute
LANDING CONDITIONS:
Field pressure altitude
Temperature
Field length
5-4
1320 Pounds
24.0 Gallons
1500 Feet
28°C (16°C Above Standard)
14 Knot Head Wind
3500 Feet
260 Nautical Miles
5500 Feet
20°C (16°C Above Standard)
10 Knot Head Wind
2000 Feet
25°C
3000 Feet
(Continued Next Page)
U.S.
CESSNA
MODEL 162
GARMIN G300
162PHUS-01