Page 574 - POH-SUPER KING AIR B200/B200C

text_perf_sect.fm Page 7 Thursday, April 19, 2007 10:49 AM
Section 5
Super King Air B200/B200C HFG Performance
MAXIMUM ENROUTE WEIGHT (14 CFR PART 135 OPERATIONS)

To determine the maximum take-off weight, the weight of the fuel used to reach
the MEA is added to the maximum enroute weight.
From the TIME, FUEL, AND DISTANCE TO CLIMB graph, the time, fuel and
distance required to climb from 5433 feet (28°C) to 18,000 feet (-6°C) are:
Time . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 - 3 = 8 minutes
Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 153 - 43 = 110 pounds
Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31 - 7 = 24 nautical miles
Enter the MAXIMUM ENROUTE WEIGHT (14 CFR Part 135 OPERATIONS)
graph at the conditions for the worst route segment of the trip, i.e., 0°C, 18,000
feet, and 29.75 in. Hg:

Maximum Enroute Weight to Meet 14 CFR Part 135 = 12,350 pounds
Requirements + 110 pounds
Maximum Take-off Weight = 12,460 pounds

TAKE-OFF WEIGHT TO MEET 14 CFR PART 25 TAKE-OFF CLIMB
CRITERIA
The following information has been presented to provide the option of limiting
weight to obtain the performance specifications of 14 CFR Part 25 during the
critical take-off and initial climb flight segments. Their use is not mandatory and
full compliance with other regulations applicable to 14 CFR Part 25 is not implied.

The criteria for limiting weight involves the selection from the Take-off Weight
graphs of the most adverse conditions of:
1. One-engine-inoperative climb
2. Field length to accelerate-stop
3. Field length to accelerate-go
4. The take-off flight path required to clear known obstacles beyond the
runway.

Revised: April, 2007 HIGH FLOTATION GEAR
P/N 101-590010-279 5-7