SOLOY TURBINE PAC
SECTION 1
POHS CESSNA U/TU 206G
GENERAL
1-4
F.A.A. Approved
November 14, 2014
INTRODUCTION
This handbook supplement contains nine sections and includes the material
required to be furnished to the pilot by CAR Part 3. 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, LLC/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:
S/Ns: U20603522 thru U20604649
Total Capacity:
80 Gallons
Total Usable:
76 Gallons
S/Ns: U20602589, U20604650 thru U20606847 and on
Total Capacity:
92 Gallons
Total Usable:
88 Gallons
OIL
Oil Specifications: See handling, service and maintenance, Section 8
Oil Capacity:
9 U.S. Quarts, including oil filter.
UNCONTROLLED
COPY
