SOLOY TURBINE PAC
SECTION 4
POHS CESSNA U/TU 206G
NORMAL PROCEDURES
4-21
F.A.A. Approved
November 17, 2015
ENROUTE CLIMB
Normally, maximum continuous power and a climb speed of 100 – 120
KIAS is maintained to cruise altitude. At lower altitudes, the torque limit of
78 PSI will be set until the TOT limit of 738
C dictates the power available.
If it is necessary to climb rapidly to altitude, the best rate-of-climb speed
should be used with the power limits shown in the table below. This speed
is 97 KIAS at sea level with 5 minute power, decreasing to 74 KIAS at
20,000 feet and 87 KIAS to 71 KIAS with maximum continuous power.
If an obstruction dictates the use of a steep climb angle, climb with flaps
retracted and the power limits shown below at 65 KIAS.
TEMPERATURE RANGE
TIME
Up to 738
C
No Limit
738
C – 810
C
5 Minutes
Over 810
C
Not Allowed
TORQUE LIMIT
TIME
Up to 78 PSI
No Limit
78 – 101.4 PSI
5 Minutes
Over 101.4 PSI
Not Allowed
CRUISE
Set cruise power and observe the 738
TOT and the 78 PSI torque limits.
Set propeller RPM, as desired, between 1630 RPM and 1810 RPM.
CAUTION
AVOID CONTINUOUS OPERATION (>60 SECONDS)
BETWEEN 1358 RPM AND 1630 RPM PROPELLER
SPEED AT TORQUE SETTING GREATER THAN 20
PSI
Check the reading of the engine instruments and monitor fuel gauges
during flight. The power control may be secured in its position by use of
the friction knob on the control rod.
During flight an imbalance can occur between the wing tanks. If the fuel
low warning system is installed, the pilot may select to use fuel from either
tank to correct for an imbalance, but the pilot must return the fuel selector
to BOTH once the imbalance is corrected. If a FUEL LOW light illuminates
during cruise, switch the fuel selector to the tank for which the FUEL LOW
light is NOT illuminated. When both lights are on, select BOTH and land
as soon as practical. When the fuel selector is in either the LEFT or
RIGHT position the FUEL CONFIG light will be illuminated.
UNCONTROLLED
COPY
