SOLOY TURBINE PAC
SECTION 4
POHS CESSNA T206H/206H
NORMAL PROCEDURES
4-21
F.A.A. Approved
May 23, 2003
NOTE
The engine inlet anti-ice must be activated for flight
or ground operation in visible moisture at an OAT of
5
C (41
F) and below (without alternate air on) or
1
C (34
C) and below (with alternate air on) and
while operating in falling or blowing snow.
The annunciator panels should be clear unless the engine alternate air is
in use. Wing flaps should be checked and set from 0
to 20
.
LANDING LIGHTS
If landing lights are to be used to enhance the visibility of the airplane in
the traffic pattern or enroute, it is recommended that only the taxi light be
used. This will extend the service life of the landing light appreciably.
TAKEOFF
With the propeller control set fully FORWARD, advance the power control
to FLIGHT IDLE and allow the engine to stabilize at 1810 N
p
RPM prior to
advancing the power control to TAKEOFF.
Monitor the engine instruments throughout the takeoff. The TOT, ENGINE
TORQUE and SPEED limits for takeoff are as follows:
TEMPERATURE RANGE
TIME
Up to 738
C
No Limit
738
C – 810
C
5 Minutes
810
C – 843
C (Intentional Use of
6 Seconds
temperatures in excess of 810
C
is not recommended.)
Over 843
C
Not Allowed
TORQUE LIMIT
TIME LIMIT
Up to 101.4 PSI
No Limit
101.4 to 106 PSI
5 Minutes
107 to 109 PSI
10 Seconds
Over 109 PSI
Not Allowed
N
1
LIMIT
TIME LIMIT
Up to 105%
No Limit
105% to 106%
15 Seconds
Over 106%
Not Allowed
UNCONTROLLED
COPY
