Page 762 - POH-SUPER KING AIR B200/B200C

101-590010-469R3_text.fm Page 15 Tuesday, January 29, 2013 8:56 AM

In the following example, the “TAKEOFF - FLAPS APPROACH, Contaminated
Runway, Non-Level Runway (2% Upslope or 2% Downslope)” table was used to
determine distances. This methodology applies to all other contaminated runway
take-off performance tables.
EXAMPLE:

Runway Condition Standing Water
of 10 mm depth
Flap Setting Approach
OAT 28°C
Pressure Altitude 5433 ft
Take-off Weight 12,500 lbs
Headwind Component 9.5 knots
Runway Slope 2% Upslope
Ground Roll 2700 ft (From POH/AFM)
Total Over 50 ft Obstacle 3750 ft (From POH/AFM)
Index Value 3750 ft (= Total Over 50 ft Obstacle)
Minimum Take-off Run 8903 ft (Using next highest index value of
3800 ft)
9403 ft (Using next highest index value of
3800 ft and rolling takeoff
adjustment).
8810 ft (Using interpolation)
9310 ft (Using interpolation between index
values and rolling takeoff
adjustment).

Approved Performance Data
Revised: January, 2013
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