Page 581 - POH-SUPER KING AIR B200/B200C

text_perf_sect.fm Page 14 Thursday, April 19, 2007 10:49 AM
Section 5
HFG Performance Super King Air B200/B200C
CRUISE TRUE AIRSPEEDS - (FL 260)

12,000 POUNDS 11,000 POUNDS

ISA + 10°C ISA + 20°C ISA + 30°C ISA + 10°C ISA + 20°C ISA + 30°C
272 270 266 277 274 272

Interpolate between these speeds for ISA + 27°C and ISA + 17°C at 11,600
pounds.
Cruise True Airspeed (IAS + 27°C) . . . . . . . . . . . . . . . . . . . . . . . . .269 knots
Cruise True Airspeed (IAS + 17°C) . . . . . . . . . . . . . . . . . . . . . . . . .273 knots

Enter the *NORMAL CRUISE POWER at 1800 RPM graph at 26,000 feet and
read the recommended torque setting for ISA + 27°C (-3°C IOAT) and ISA + 17°C
(-13°C IOAT):
ISA + 27°C (-3°C IOAT) . . . . . . . . . . . . . . . . . . 1434 ft-lbs torque per engine
ISA + 17°C (-13°C IOAT) . . . . . . . . . . . . . . . . . 1501 ft-lbs torque per engine
Enter the *FUEL FLOW at NORMAL CRUISE POWER at 1800 RPM graph at
26,000 feet and read the fuel flow for ISA + 27°C (-3°C IOAT) and ISA + 17°C
(-13°C IOAT):
ISA + 27°C (-3°C IOAT)
Fuel Flow Per Engine. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .263 lbs/hr
Total Fuel Flow. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .526 lbs/hr
ISA + 17°C (-13°C IOAT)
Fuel Flow Per Engine. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .273 lbs/hr
Total Fuel Flow. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .546 lbs/hr
*NOTE: For flight planning, enter these graphs at the ISA condition forecast; for
enroute power settings and fuel flow, enter the graphs at the actual IOAT.

Time = Distance ÷ Ground Speed
Fuel Used = (Time) x (Total Fuel Flow)

HIGH FLOTATION GEAR Revised: April, 2007
5-14 P/N 101-590010-279