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Textron Cessna Skyhawk SP - Introduction; Descriptive Data; Engine; Propeller

Textron Cessna Skyhawk SP
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CESSNA SECTION 1
MODEL 172S NAV III GENERAL
GFC 700 AFCS
U.S.
INTRODUCTION
This POH contains 9 sections, and includes the material required to be
furnished to the pilot by 14 CFR 23. It also contains supplemental data
supplied by Cessna Aircraft Company.
Section 1 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: Textron Lycoming
Engine Model Number: IO-360-L2A
Engine Type: Normally aspirated, direct drive, air-cooled, horizontally
opposed, fuel injected, four cylinder engine with 360.0 cu.
in. displacement.
Horsepower Rating and Engine Speed: 180 rated BHP at 2700 RPM
PROPELLER
Propeller Manufacturer: McCauley Propeller Systems
Propeller Model Number: 1A170E/JHA7660
Number of Blades: 2
Propeller Diameter: 76 inches
Propeller Type: Fixed pitch
(Continued Next Page)
1-5172SPHBUS-00

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