Page 576 - POH-SUPER KING AIR B200/B200C

text_perf_sect.fm Page 9 Thursday, April 19, 2007 10:49 AM
Section 5
Super King Air B200/B200C HFG Performance
4. Using the ACCELERATE-GO graphs, enter in reverse using the 6786 feet
value and determine the weight for which this accelerate-go distance is
possible.
a. Take-off weight of 10,600 pounds with flaps at 0%
b. Take-off weight of 11,380 pounds with flaps at 40%
5. Enter the TAKE-OFF FLIGHT PATH graph to determine the minimum
gradient of climb which will result in a flight path clear of the 175-foot-high
ridge 3000 feet beyond the end of the runway. (Refer to the TAKE-OFF
FLIGHT PATH diagram.)
a. Ridge = 175 feet AGL
b. From Reference Zero (9486 - 6786) = 2700 feet
c. Minimum Gradient of Climb = 5.2%
6. Enter the NET GRADIENT OF CLIMB - FLAPS 0% graph at 10,600 pounds
and the NET GRADIENT OF CLIMB - FLAPS 40% graph at 11,380 pounds.
• Both resulting gradients are less than 5.2%.
7. Enter in reverse the NET GRADIENT OF CLIMB graphs using the 5.2% net
gradient of climb value to determine the weights for which a climb at this
value is possible.
a. Flaps 0% = 9700 pounds
b. Flaps 40% = 9000 pounds

Revised: April, 2007 HIGH FLOTATION GEAR
P/N 101-590010-279 5-9