Page 572 - POH-SUPER KING AIR B200/B200C

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Section 5
Super King Air B200/B200C HFG Performance
INTRODUCTION TO PERFORMANCE AND FLIGHT
PLANNING

The graphs and tables in this Section present performance information for takeoff,
climb, landing and flight planning at various parameters of weight, power, altitude
and temperature. All FAA-approved performance information is included within
this Section. Examples have been presented on all performance graphs.
The following example presents calculations for flight time, block speed and fuel
required for a proposed flight from departure to destination using the conditions
listed below.

CONDITIONS

At Departure:
Outside Air Temperature. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28°C (82°F)
Field Elevation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5333 feet
Altimeter Setting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29.82 in. Hg
Wind . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 330° at 10 knots
Runway 35L Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11,500 feet
ROUTE MAGNETIC MAGNETIC DISTANCE WIND AT OAT AT OAT AT ALTIMETER
SEGMENT COURSE VARIATION NM FL 260 FL 260 18,000 FT SETTING
DIR/ °C °C IN. HG
KNOTS
LEG A 265° 13°E 143 350°/40 -10 -6 29.82
LEG B 270° 15°E 192 350°/40 -10 -7 29.82
LEG C 249° 16°E 81 340°/35 -20 0 29.75
LEG D 250° 16°E 145 340°/35 -20 0 29.75
LEG E 227° 17°E 146 290°/45 -20 -4 29.60
At Destination:
Outside Air Temperature. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32°C (90°F)
Field Elevation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4412 feet
Altimeter Setting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29.60 in. Hg
Wind . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 270° at 5 knots
Runway 25 Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6101 feet
To determine the pressure altitude at departure and destination airports, add 1000
feet to field elevation for each 1.00 in. Hg that the reported altimeter setting value
is below 29.92 in. Hg, and subtract 1000 feet for each 1.00 in. Hg above 29.92 in.
Hg. First, find the difference between 29.92 in. Hg and the reported altimeter
setting. Then multiply the answer by 1000 to find the difference in feet between
field elevation and pressure altitude.

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