CESSNA
MODEL
2088 (675
SHP)
SECTION 5
PERFORMANCE
SAMPLE PROBLEM
(Continued)
FUEL REQUIRED
(Continued)
The total estimated fuel required is as follows:
Engine start, taxi, and takeoff
35
Climb 94
Cruise 1194
Descent 72
Reserve
230
Total fuel required 1625 Pounds
Once the flight is underway, ground speed checks will provide a
more accurate basis for estimating the time
enroute and the
corresponding fuel required to complete the trip with ample reserve.
LANDING
A procedure similar to takeoff should be used for estimating the landing
distance at the destination airport. The estimated landing weight is as
follows:
Takeoff weight 8600
Fuel required for climb,
cruise, and descent
1625
Landing weight 6975 Pounds
.,
Figure 5-23 presents landing distance information for the short field
technique. The landing distances for a weight of 7000 pounds and
~-,
corresponding to 2000 feet pressure altitude and a temperature of 30°C
~,
should be used and are as follows:
Ground roll: 850 Feet
~,
Total distance to clear a 50-foot obstacle:1650 Feet
A
correction for the effect of w~nd may be made based on Note 2 of the
land ng chart using the same procedure as outlined for takeoff.
-
1
Revision 23
-1
U.S.
5-1
1
To Next Page