CESSNA SECTION 1
MODEL T182T 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: TIO-540-AK1A
Engine Type: Turbocharged, direct drive, air-cooled, horizontally
opposed, fuel injected, six cylinder engine with 541.5 cu.
in. displacement.
Horsepower Rating and Engine Speed: 235 rated BHP at 32 in.hg. and
2400 RPM
PROPELLER
Propeller Manufacturer: McCauley Propeller Systems
Propeller Model Number: B3D36C442/80VSB-1
Number of Blades: 3
Propeller Diameter: 79 inches
Propeller Type: Constant speed and hydraulically actuated.
(Continued Next Page)
1-5T182TPHBUS-01
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