Cessna 402C Pilot Operating Handbook page 8

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SECTION 1
GENERAL
TABLE OF CONTENTS
Page
SECTION 1
GENERAL
Page
INTRODUCTION
ENGINES . . .
THREE-VIEW DRAWING
PROPELLERS
FUEL .
OIL . . . . . . . .
MAXIMUM CERTIFICATED
WEIGHTS . . . . . .
CABIN, BAGGAGE AND ENTRY
DIMENSIONS . . . . . .
STANDARD AIRPLANE WEIGHTS
SPECIFIC LOADINGS . . .
INTRODUCTION
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1-2
1-3
1-3
1-4
1-4
1-5
1-7
1-8
SYMBOLS, ABBREVIATIONS
AND TERMINDLOGY . . .
General Airspeed Ter-
minology and Symbols
Meteorological
Terminology . . . .
Power Terminology . .
Airplane Performance
and Flight Planning
Terminology . . .
Weight and Balance
Tenn; n01 09Y . . . .
1-8
1-8
1-9
1-10
1-10
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This handbook consists of 9 sections and an alphabetical index as
shown on the Contents page. This handbook includes the material required
to be furnished to the pilot by CAR Part 3. It also contains supplemental
I
data supplied
by
Cessna Aircraft Company. Specific information can be
rapidly found by referring to the Contents page for the appropriate sec-
tion, then referring to the Table Of Contents on the first page of the
appropriate section, or
by
the use of the Alphabetical Index.
Section 1 of the handbook presents basic airplane data and general
infonnation which will be of value to the pilot.
ENGINES
Number of Engines: 2
Manufacturer:
Engine Model
Number:
Teledyne Continental Motors
TSIO-520-VB
Engine Type.:
Turbocharged,
horizontally
di splacement.
fuel-injected, direct drive, air-cooled,
opposed, six-cylinder, 520 cubic-inch
•
Horsepower:
325 rated horsepower at 2700 propeller RPM and 39.0
inches Hg. manifold pressure to the critical altitude of
12,000 feet.
310 horsepower at 2600 propeller RPM and 39.0 inches H9.
manifold pressure to the critical altitude of 16,000
feet.
I November 1979
Revision 2 - 3 AU9 1981
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