CESSNA SECTION 5
MODEL 208B 867 SHP PERFORMANCE
GARMIN G1000
U.S.
FAA APPROVED
SAMPLE PROBLEM (Continued)
FUEL REQUIRED (Continued)
The total estimated fuel required is as follows:
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 Pounds
Fuel required for climb, cruise, and descent -1773 Pounds
Landing weight 6827 Pounds
The Short Field Landing Distance chart 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 935 Feet
Total distance to clear a 50-foot obstacle 1740 Feet
A correction for the effect of wind may be made based on information
presented in the note section of the landing chart, using the same
procedure as outlined for takeoff.
Engine start, taxi, and takeoff 35 Pounds
Climb +77 Pounds
Cruise +1311 Pounds
Descent +77 Pounds
Reserve + 273 Pounds
Total Fuel Required 1773 Pounds
208BPHCUS-00
5-11
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