Page 582 - POH-SUPER KING AIR B200/B200C

text_perf_sect.fm Page 15 Thursday, April 19, 2007 10:49 AM
Section 5
Super King Air B200/B200C HFG Performance
Results are as follows:

ESTIMATED TIME AT FUEL USED
ROUTE DISTANCE GROUND CRUISE FOR
SPEED ALTITUDE CRUISE
NM KNOTS HRS:MIN LBS
LEG A 85* 254 :20 176
LEG B 192 250 :46 404
LEG C 81 262 :19 169
LEG D 145 261 :33 303
LEG E 79* 240 :20 180
TOTAL 582 2:18 1232
* Distance required to climb or descend has been subtracted from segment distance.

TIME, FUEL, AND DISTANCE

TIME FUEL DISTANCE
ITEM
HRS:MIN POUNDS NM
Start, Run-up, Taxi, and Take-off 00:00 90 0
Acceleration
Climb 00:18 208 58
Cruise 2:18 1232 582
Descent 00:14 126 67
TOTAL 2:50 1656 707
Block Speed: 707 NM ÷ 2 hours, 50 minutes = 250 knots

RESERVE FUEL
Reserve Fuel (45 minutes at Maximum Range Power): Assume weight at end of
cruise to be 11,000 pounds. Enter the tables for MAXIMUM RANGE POWER at
1700 RPM for ISA + 10°C and ISA + 20°C, and read the fuel flow for 26,000 feet
at 11,000 pounds:

ISA + 10°C . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 416 lbs/hr Total Fuel Flow
ISA + 20°C . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 416 lbs/hr Total Fuel Flow
Interpolate to find fuel flow at ISA + 17°C:

Total fuel flow for reserve = 416 + 0 = 416 lbs/hr
Reserve Fuel = 45 minutes x 416 lbs/hr = 312 lbs

Revised: April, 2007 HIGH FLOTATION GEAR
P/N 101-590010-279 5-15