Cessna T182 Series User Manual

MODEL
182 & T182
SERIES
SERVICE
MANUAL
SECTION 1
GENERAL DESCRIPTION
Page
No.
Page No.
TABLE OF CONTENTS
Aerofiche/Manual TABLE
OF CONTENTS Aerofiche Manual
GENERAL DESCRIPTION
.
. ... 1A7/1-1
Torque Values
- Bolts ......
1A10/1-4
Model 182,
F182, and T182
Series
. 1A7/1-1
Torque Values
- Fittings
... .
1A131-7
Description.
......
.. 1A7/1-1
SAFETYING
PROCEDURES
....
1A14 1-8
Aircraft Specifications
... . 1A7/1-1
SAFETY WIRE
PROCEDURES
.... . 1A14
1-8
Stations ...
.....
.. 1A7/1-1
USE
OF COTTER
PINS .......
1A18
1-12
GENERAL
AIRFRAME
PRACTICES
. .
1A10/1-4
USE
OF LOCKING
CLIPS
.
. .
. 1A20,1-14
TORQUEING
PROCEDURES
. ....
1A10/1-4
USE OF LOCKWASHERS
...... 1A20/1-14
Calculating
Torque .......
1A10/1-4
USE OF SELF-LOCKING
NUTS
. .. 1A20/1-14
1-1. GENERAL DESCRIPTION. series aircraft consists of a single air-cooled, six
cylinder horizontally-opposed
0-470
Series Con-
1-2. MODEL 182, F182, and T182
SERIES. tinental engine.
The power plant for the T182
series aircraft
is a turbocharged,
air-cooled,
1-3. DESCRIPTION.
The Cessna
Model 182, F182
horizontally-opposed,
six-cylinder, 0-540
Lycoming
and T182 series aircraft,
described in this manual,
engine.
Both engines are coupled
directly to a two-
are high wing, strut-braced
monoplanes of
all-metal, bladed
all-metal, constant speed
McCauley propeller.
semimonocoque construction. The aircraft are of
conventional
design consisting of five
basic units,
1-4. AIRCRAFT SPECIFICATIONS.
Leading
par-
i. e. fuselage, wing,
stabilizers, flight
control sur- ticulars
of these aircraft,
with dimensions based
on
faces and landing gear. The landing gear
is of con- gross weight, are given in figure
1-1. If these di-
temporary
fixed tricycle layout
for increased ground
mensions are
used for constructing a
hangar or com-
stability
and is equipped with
steerable nose gear,
puting clearances,
remember that such
factors as
tubular spring-steel
main gear struts
and ABS speed
nose gear strut inflation,
tire pressures, tire
sizes
fairings for all wheels. In addition,
the nose gear and load distribution
may result in some dimensions
utilizes an air/hydraulic fluid type shock strut, that are considerably different from those listed.
Standard cabin
seating is four place with
an optional
child's seat installation
available. A carpeted bag- 1-5. STATIONS.
A station diagram is shown in
gage compartment area is provided aft of the pass- figure 1-2 to assist in locating equipment where a
enger seats. The power plant for the 182 and F182 written description is inadequate or impractical.
Revision 1 1-1

Cessna T182 Series Specifications

General

Engine Type	Lycoming IO-540-AB1A5
Horsepower	230 hp
Seating Capacity	4
Service Ceiling	18, 100 feet
Takeoff Distance	1, 600 feet
Landing Distance	1, 350 ft
Type	Single-engine
Max Takeoff Weight	3, 100 lb
Wingspan	36 ft
Length	29 ft
Height	9 feet 3 inches
Fuel Capacity	92 US gal (348 L)