Page 580 - POH-SUPER KING AIR B200/B200C

text_perf_sect.fm Page 13 Thursday, April 19, 2007 10:49 AM
Section 5
Super King Air B200/B200C HFG Performance
Calculations for flight time, block speed and fuel requirements for a proposed flight
are detailed below.
Enter the ISA CONVERSION graph at the conditions indicated:
DEPARTURE
Pressure Altitude. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5433 ft
OAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28°C
ISA Condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISA + 23°C
LEG A - LEG C
Pressure Altitude. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26,000 ft
OAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . -10°C
ISA Condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISA + 27°C
LEG C - LEG E
Pressure Altitude. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26,000 ft
OAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . -20°C
ISA Condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISA + 17°C
DESTINATION

Pressure Altitude. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4732 ft
OAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32°C
ISA Condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISA + 27°C
Enter the TIME, FUEL, AND DISTANCE TO CLIMB graph at 28°C to 5433 feet
and to 12,500 pounds, and enter at -10°C to 26,000 feet and to 12,500 pounds
and read:
Time to Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 - 3 = 18 minutes
Fuel Used to Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . 251 - 43 = 208 pounds
Distance Traveled . . . . . . . . . . . . . . . . . . . . . . . . . . 65 - 7 = 58 nautical miles
Enter the TIME, FUEL, AND DISTANCE TO DESCEND graph at 26,000 feet and
enter again at 4732 feet and read:
Time to Descend. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 - 3 = 14 minutes
Fuel Used to Descend. . . . . . . . . . . . . . . . . . . . . . . . . 163 - 37 = 126 pounds
Descend Distance. . . . . . . . . . . . . . . . . . . . . . . . . 81 - 14 = 67 nautical miles
The estimated average cruise weight is approximately 11,600 pounds.
Enter the tables for NORMAL CRUISE POWER at 1800 RPM for ISA + 10°C, ISA
+ 20°C and ISA + 30°C and read the cruise speeds for 26,000 feet at 12,000
pounds and 11,000 pounds.

Revised: April, 2007 HIGH FLOTATION GEAR
P/N 101-590010-279 5-13