EasyManua.ls Logo

Cessna TR182 1979 - Introduction; Engine; Propeller; Fuel

Cessna TR182 1979
328 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
CESSNA
MODELTR182
SECTION,1
GENERAL
INTRODUCTION
This handbook contains 9sections, and includes the material required
to be furnished to the pilot by CAR Part 3.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: Avco Lycoming.
Engine Model Number: 0-540-L3C5D.
Engine Type: Turbocharged, direct-drive, air-cooled, horizontally-
opposed, carburetor equipped, six-cylinder engine with 541.5cu. in.
displacemen t.
Horsepower Rating and Engine Speed: 235rated BHP at 31inches Hg and
2400 RPM.
PROPELLER
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number: B2D34C217/90DHB-8.
Number of Blades: 2.
Propeller Diameter, Maximum: 82 inches.
Minimum: 80.5inches.
Propeller Type: Constant speed and hydraulically actuated, with a low
pitch setting of 15.8°and a high pitch setting of 31.9°(30inch station).
FUEL
Approved Fuel Grades (and Colors):
100LLGrade Aviation Fuel (Blue).
100(Formerly 100/130)Grade Aviation Fuel (Green).
1 October 1978
1-3

Table of Contents