Cessna T182 Series User Manual

MODEL
182 & T182
SERIES
SERVICE
MANUAL
Use
rivet
pattern
at
wing
station
23.62 for repair from wing sta-
tion
23. 62 to
wing station
85. 86.
Use rivet pattern
at wing station
100.
50 for lap splice patterns
,
.
from wing station 100. 50 to 190.
00.
See figure
1-2 for
wing
stations.
Use
rivet
spacing
similar
to the
pattern at wing station
100. 50
at
leading edge
ribs between
lap splices.
Select
number of flush rivets
to
be
used
at
each
wing
station
leading
edge
rib from
table
below.
RIBS:
Blind
rivets
may be
substituted
for
solid rivets in proportionally increased
numbers in
accordance with
the table.
SPARS:
Blind rivets
may
be installed
in wing
spars
only
in those
locations
where
blind
rivets
were used
during
original
manufacture,
ie fuel
bay area
of front
spars on
aircraft
with integral fuel bays.
NUMBER
OF FLUSH RIVETS
IN DIMPLED SKIN
RE-
QUIRED
IN REPLACEMENT
LEADING EDGE
SKINS
STATION
MS20426-4
CR2248-4
RIB
118
18
22
EXISTING
136
15
18
TACK RIVET
154
11
13
190
10
12
PATCH
EXISTING
RIVET
PATTERN
TYPICAL LEADING EDGE SECTION
Figure
18-11.
Bonded Leading
Edge
Repair
18-32

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)