Powerplant Limitations - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

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SECTION 2
OPERATING LIMITATIONS

POWERPLANT LIMITATIONS

ENGINE
Engine Manufacturer . . . . . . . . . . . . . . Pratt & Whitney Canada Inc.
Engine Model Number . . . . . . . . . . . . . . . . . . . . . . . . . . . . PT6A-140
Engine Operating Limits . . . . . . . . . . . . . . . . . . Refer to Figure 2-3
Fuel Grade and Approved Fuel Additives . .Refer to Fuel Limitations
OIL SPECIFICATION
Oil conforming to Pratt & Whitney Engine Service Bulletin No. 1001,
and all revisions or supplements thereto, must be used. Refer to
Section 8, Airplane Handling, Service and Maintenance, Servicing,
Oil, for a listing of approved oils.
When adding oil, service the engine with the type and viscosity
which is currently being used in the engine.
PROPELLER
Propeller Manufacturer . . . . . . . . . . . . . . . . . . Hartzell Propeller Inc.
Propeller Model Number . . . . . . . . . . . .HC-B3TN-3AF/T10890CN-2
Propeller Diameter
Maximum. . . . . . . . . . . . . . . . . . . . . . . . . . . . 106 Inches (2.7 m)
Minimum . . . . . . . . . . . . . . . . . . . . . . . . . . . . 104 Inches (2.6 m)
Hartzell Propeller Blade Angle at 42-inch Station:
Feathered . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78.0 + 1.0°
Low Pitch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.5 + 0.2°
Maximum Reverse . . . . . . . . . . . . . . . . . . . . . . . . . . . -21 + 0.5°
2-6
(Continued Next Page)
U.S.
CESSNA
MODEL 208B (867 SHP)
GARMIN G1000
FAA APPROVED
208BPHCUS-01

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