Cessna Skylane 182T User Manual

CESSNA
SECTION
7
MODEL
182T
NAV
III
AIRPLANE
AND
SYSTEM
DESCRIPTION
GFC
700
AFCS
WING FLAP SYSTEM
The
single
slot
type
wing
flaps,
refer
to
Figure
7-3,
are
extended
or
retracted
by
positioning
the
wing
flap
control
lever
on
the
instrument
panel
to
the
desired
flap
deflection
position.
The
wing
flap
control
lever
is
moved
up
or
down
in
a
slotted
panel
that
provides
mechanical
stops
at
the
10°
and
20°
positions.
To
change
flap
setting,
the
wing
flap
control
lever
is
moved
to
the
right
to
clear
mechanical
stops
at
the
10°
and
20°
positions.
A
scale
and
pointer
to
the
left
of
the
wing
flap
control
lever
indicates
flap
travel
in
degrees.
The
wing
flap
system
circuit
is
protected
by
a
10-ampere
circuit
breaker,
labeled
FLAP,
on
the
left
side
of
the
circuit
breaker
panel.
Wing Flap System }
0785R1037
Figure
7-3
LANDING GEAR SYSTEM
The
landing
gear
is
of
the
tricycle
type,
with
a
steerable
nosewheel
and
two
main
wheels.
Wheel
fairings
are
standard
equipment
for
both
the
main
wheels
and
nosewhee!l.
Shock
absorption
is
provided
by
the
tubular
spring
steel
main
landing
gear
struts
and
the
air/oil
nose
gear
shock
strut.
Each
main
gear
wheel
is
equipped
with
a
hydraulically-
actuated
disc
type
brake
on
the
inboard
side
of
each
wheel.
J182TPHBUS-05
U.S.
7-23

Cessna Skylane 182T Specifications

General

Manufacturer	Cessna
Model	Skylane 182T
Type	Single-engine piston
Engine	Lycoming IO-540-AB1A5
Horsepower	230 hp
Maximum Takeoff Weight	3, 100 lb (1, 406 kg)
Wingspan	36 ft (11.0 m)
Length	29 ft (8.8 m)
Seating Capacity	4
Category	Aircraft
Maximum Speed	148 knots
Stall Speed (with flaps)	49 knots
Rate of Climb	924 feet per minute
Empty Weight	1, 970 pounds
Fuel Capacity	87 gallons
Height	9 feet 4 inches
Maximum Cruise Speed	145 knots
Service Ceiling	18, 100 feet