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Cessna 402C User Manual

Cessna 402C
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SECTION
2
LIMITATIONS
SECTION 2
LIMITATIONS
TABLE
OF
CONTENTS
INTROOUCTION
. . . . . .
AIRSPEED
LIMITATIONS
. .
ENGINE
LIMITATIONS
. . .
MISCELLANEOUS
INSTRUMENT
MARKINGS
..••.
. .
WEIGHT
LIMITS
. . . .
MANEUVER
LIMITS
. . . .
FLIGHT
LOAD
FACTOR
LIMITS
FLIGHT
CREW
LIMITS
. .
INTRODUCTION
Page
2-1
2-2
2-3
2-6
2-6
2-7
2-7
2-7
OPERATION
LIMITS
..
.
..
FUEL
LIMITATIONS
. . . . .
MAXII~Ufl
OPERATING
ALTITUDE
LIMIT
. . . . . . . .
MAXIMUM
PASSENGER
SEATING
LIMITS
.,
. . . . . . .
REQUIRED
PLACARDS
. . . . . .
A'dh In10 lei":!)
C."t/i"'ns
Page
2-7
2-7
2-8
2-8
2-9
,,2-/f
Section 2 of
this
handbook
presents
the
operating
limitations,the
significance of
such
limitations, instrument markings, color coding
and
basic placards necessary for the safe operation of
the
airplane,
its
powerplants, standard systems
and
standard
equipment.
The
limitations
included in
this
section
and
Section 9
have
been
approved
by
the
Federal
Aviation Administration.
Observance
of these operating limitations
is
required
by
law.
Operation
in
countries other
than
the
United
States
may
require
observance of other
limitations.
procedures or
performance
data
in
appli-
cable
supplements
.
.....
-------NOTE----------,
Refer
to Section 9
of
this
handbook
for
amended
operating
limitations.
operating procedures, per-
formance
data
and
other necessary information for
airplanes
equipped
with
specific
options.
FAA
Approved
I November 1979
2-1

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Cessna 402C Specifications

General IconGeneral
ManufacturerCessna
Model402C
TypeLight twin-engine aircraft
Maximum Takeoff Weight6, 850 lb (3, 107 kg)
Service Ceiling26, 900 ft (8, 200 m)
Seating CapacityUp to 9 passengers
Wingspan44 ft 2 in (13.46 m)
Length36 feet 10 inches (11.23 meters)
Height11 ft 5 in (3.48 m)
Cabin Width4 feet 2 inches (1.27 meters)
Cabin Height4 ft 2 in (1.27 m)
Fuel Capacity213 US gallons (806 liters)
Engines2 × Continental TSIO-520-VB turbocharged piston engines

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