Page 755 - POH-SUPER KING AIR B200/B200C

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

runway contaminants may cause propeller blade erosion or foreign object dam-
age to the engines. The following procedure is recommended in such situations.
ROLLING TAKEOFF
(INCREASE SCHEDULED CONTAMINATED RUNWAY TAKEOFF
DISTANCES BY 500 FT)
1. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE
2. Power . . . . . . . . . . . . . . . . . . . . ADJUST SMOOTHLY TO SET MINIMUM
TAKE-OFF POWER WITHIN 10 SECONDS
OF BRAKE RELEASE, OBSERVE ITT
3. [L AFX] & [R AFX] . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ILLUMINATED
(or, [L AUTOFEATHER] & [R AUTOFEATHER] - Illuminated
NOTE
Increasing airspeed will cause torque and ITT to increase.
4. Landing Gear (when positive climb established). . . . . . . . . . . . . . . . . . . UP
5. Flaps (at 121 knots minimum). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

The presentation of performance data in this supplement
for wet and contaminated runways should not be taken as
implying that the ground handling characteristics on these
surfaces will be as good as can be obtained on dry or wet
runways, in particular, following engine failure, operations
in crosswinds, and use of reverse thrust. While adequate
directional control is theoretically adequate for takeoffs and
landings on wet and contaminated runways, pilots should
be aware that extra care will be required during such ope-
ations. Refer to Cold Weather Procedures in Section 4,
NORMAL PROCEDURES, of the POH/AFM.
Landing distances in this supplement assume the airplane
is established on a steady glidepath at the required
approach speed by 50 feet above the surface. At this point,
the power is brought to idle and the airplane is landed
using the minimum flare and a firm touchdown. Using this
procedure on wet and contaminated runways is increas-
ingly important as it ensures a proper touchdown speed
and establishes full weight of the airplane on the tires in the
shortest amount of time. All of this combines to improved
braking performance and decrease landing distance.

Approved Performance Data
Revised: January, 2013
8 of 28 P/N 101-590010-469