Page 573 - POH-SUPER KING AIR B200/B200C

text_perf_sect.fm Page 6 Thursday, April 19, 2007 10:49 AM
Section 5
HFG Performance Super King Air B200/B200C
Pressure Altitude at departure:

29.92 in. Hg - 29.82 in. Hg = 0.10
0.10 x 1000 feet = 100 feet
The pressure altitude at departure is 100 feet above field elevation.
Pressure Altitude at departure = 5333 + 100 = 5433 feet.
Pressure Altitude at destination:
29.92 in. Hg - 29.60 in. Hg = 0.32
0.32 X 1000 feet = 320 feet
The pressure altitude at destination is 320 feet above field elevation.
Pressure Altitude at destination = 4412 + 320 = 4732 feet.
PERFORMANCE EXAMPLE

TAKE-OFF WEIGHT
Maximum take-off weight limit (from Section II, LIMITATIONS) = 12,500 pounds.
A summary of graphs provided in this handbook to restrict take-off weight is
presented below:
1. MAXIMUM TAKE-OFF WEIGHT PERMITTED BY ENROUTE CLIMB
REQUIREMENT (No Restriction)
2. TAKE-OFF WEIGHT TO ACHIEVE POSITIVE ONE-ENGINE-
INOPERATIVE CLIMB AT LIFT-OFF (separate graphs for Flaps 0% and
Flaps 40%.) (Optional)
3. MAXIMUM ENROUTE WEIGHT (14 CFR PART 135 OPERATIONS)
(Required for 14 CFR Part 135 operations.)
4. TAKE-OFF WEIGHT TO MEET 14 CFR PART 25 TAKE-OFF CLIMB
REQUIREMENTS (separate graphs for Flaps 0% and Flaps 40%.)
(Optional)

MAXIMUM TAKE-OFF WEIGHT PERMITTED BY ENROUTE CLIMB
REQUIREMENT
There is no weight restriction to meet Enroute Climb Requirements.
Maximum allowable take-off weight = 12,500 pounds.

TAKE-OFF WEIGHT TO ACHIEVE POSITIVE ONE-ENGINE-
INOPERATIVE CLIMB AT LIFT-OFF
Enter the graphs at 5433 feet and 28°C to determine the maximum weight at
which the accelerate-go procedures should be attempted.
Maximum Accelerate-Go Weight (Flaps 0%) . . . . . . . . . . . . . . . . .12,500 pounds
Maximum Accelerate-Go Weight (Flaps 40%) . . . . . . . . . . . . . . . .12,450 pounds
HIGH FLOTATION GEAR Revised: April, 2007
5-6 P/N 101-590010-279