SOLOY TURBINE PAC
SOLOY SUPPLEMENT NO. 2
POHS CESSNA U/TU 206G
ENGINE INLET ANTI-ICE KIT
4 of 4
F.A.A. Approved
October 4, 2005
7. Power Control – FLIGHT IDLE
8. Start Motor Switch – MOTOR
9. TOT 150 degrees or lower and N
1
15% below 15,000 FT. MSL.
N
1
maximum obtainable above 15,000 FT. MSL
10. Start Motor Switch – START and hold.
11. Fuel Cutoff Control – RUN (IN)
12. TOT and N1 – MONITOR (810ºC to 927ºC FOR 10 SECOND
MAXIMUM)
13. De-energize the starter at 58% N1
14. Propeller Control – IN
NOTE
As the propeller comes out of feather, there
will be an oscillation of power until the
propeller RPM stabilizes.
SECTION 4
NORMAL PROCEDURES
The only change to the airplane normal procedures when the Engine Inlet
Anti-Ice system is installed is to check operation on the run-up during the
pre-flight check.
SYSTEM CHECK
1. Engine Inlet Anti-Ice – ON
NOTE
A drop in torque and a rise in TOT is normal
with the actuation of the engine anti-ice
system.
2. Engine Inlet Anti-Ice – AS REQUIRED
SECTION 5
PERFORMANCE
There are no changes to the airplane performance when the Engine Inlet
Anti-Ice system is installed
UNCONTROLLED
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