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Cessna 208B - Descriptive Data; Engine; Propeller (Hartzell); Propeller (Mccauley)

Cessna 208B
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CESSNA
MODEL
2088 (675 SHP)
DESCRIPTIVE DATA
SECTION 1
GENERAL
ENGINE
Number of Engines:
1
Engine Manufacturer: Pratt
&
Whitney Canada, Inc.
Engine Model Number:
PT6A-114A.
Engine Type: Free turbine, two-shaft engine utilizing a compressor
section having three axial stages and one centrifugal stage, and
annular reverse-flow combustion chamber, a one-stage
compressor turbine, a one-stage power turbine, and a single
exhaust. The power turbine drives the propeller through a
two-
stage planetary gearbox at the front of the engine.
Horsepower: Flat rated at 675 shaft horse power.
PROPELLER (Hartzell)
Propeller Manufacturer: Hartzell Propeller Products.
Propeller Model Number:
HC-B3MN-3lM10083.
Number of Blades:
3.
Propeller Diameter: Maximum 100 inches.
Minimum 100 inches (No cutoff approved).
Propeller Type: Constant-speed, full-feathering, reversible.
hydraulically-actuated composite-bladed propeller, with a
feathered blade angle of
78.4", a low pitch blade angle of
9",
and
a maximum reverse blade angle of -18" (42-inch station).
PROPELLER (McCauley)
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number:
3GFR34C7031106GA-0.
Number of Blades: 3.
Propeller Diameter: Maximum 106 inches.
Minimum 104 inches.
Propeller Type: Constant-speed, full-feathering, reversible,
hydraulically-actuated aluminum-bladed propeller, with a
feathered blade angle of
88", a low pitch blade angle of 15.6",
and a maximum reverse blade angle of -14" (30-inch station).
1
Revision 23
-,
U.S. 1-5

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