SECTION 5
PERFORMANCE
-
CESSNA
MODEL
2088 (675 SHP)
SAMPLE PROBLEM
The following sample flight problem utilizes information from the
various charts to determine the predicted performance data for a typical
fliaht of an
air~lane not eauio~ed with a carao ~od. A similar calculation
,-
c& be made tor an airplane with a cargo pi;d using cnans :dentfed as
appropriate for this configuration. The following information is known:
AIRPLANE CONFIGURATION (CARGO POD INSTALLED)
Takeoff weight:
Usable fuel:
8600 Pounds
2224 Pounds
TAKEOFF CONDITIONS
Field pressure altitude: 3500 Feet
1
Temperature: 16°C (standard
+
8°C)
Wind component along runway: 12 Knot Headwind
Field length: 4000 Feet
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
Field length: 3000 Feet
(Continued Next Page)
-.
Revision 23
To Next Page
Loading...
