SOLOY TURBINE PAC
SECTION 1
POHS CESSNA T206H/206H
GENERAL
1-4
F.A.A. Approved
May 23, 2003
INTRODUCTION
This handbook supplement contains nine sections and includes the material
required to be furnished to the pilot by FAR Part 23. It also contains
supplemental data.
Section I provides basic data and information of general interest. It also
contains definitions or explanations of symbols, abbreviations, and terminology
commonly used.
DESCRIPTIVE DATA
ENGINE
Number of Engines:
1
Engine Manufacturer:
Soloy Corporation/Rolls Royce
Engine Model Number:
Soloy Turbine Pac, 780-1000-1
Horsepower Rating and Engine Speed:
Takeoff power (5 minute):
418 SHP @ 1810 RPM
Maximum continuous Power:
321 SHP @ 1810 RPM
PROPELLER
Propeller Manufacturer:
Hartzell
Propeller Model Number:
HC-C3YN-5A/FC9587D-2
Number of Blades:
3
Propeller Diameter:
95 Inches
Propeller Type:
Constant speed, hydraulically
actuated, full feathering
FUEL
Approved Fuel Grades:
See handling, service and
maintenance, Section 8
Fuel Capacity:
Total Capacity:
92 Gallons
Total Usable:
88 Gallons
Total Capacity Each Tank:
46.0 Gallons
Total Usable Each Tank:
44.0 Gallons
NOTE
To ensure maximum fuel capacity and minimize cross feeding
when refueling, always park the airplane in a wings-level,
normal ground attitude and place the fuel selector in the Left
or Right position. Refer to Figure 1-1 for normal ground
attitude dimensions. See Section 2 for approved fuels.
UNCONTROLLED
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