Cessna 182 1978 - Page 154

MODEL
182 &
T182 SERIES
SERVICE
MANUAL
Apply
Universal
Oil
Dynaplex
21C
Regular
the
pipe
threaded
brake
fitting
only.
A
26
25
24
27*
Bolt
length may vary ac-
cording
to the
number
of
21
shims used, and if option-
al wheel fairing has been
installed.
12
14
24 28
31
Where fitting (10) joins strut assembly
29
30
(23),
install
with
wet
primer
(Green
SECTION
A-A
zinc chromate
or equivalent)
on faying
SECTION
A-A
surfaces
only.
INBOARD
Apply
Y8560
Polyurethane
tape
(3M Co.,
St.
Paul, Minnesota)
where fairing (6) will cause chafing.
1. Snap
Ring
10.
Fitting
17. Cotter
Pin
24.
Outboard
Forging
2. Strut-Attach
Pin 11. Shim
18.
Hub Cap
25. Plug Button
3. Upper
Fairing 12.
Axle
19. Back Plate
26. Inboard Forging
4. Brake Line 13. Torque Plate 20. Brake Cylinder 27. Cover Plate
5. Step Tread
14. Lower Fairing 21. Bracket
28. Spacer
6. Strut Fairing 15. Wheel
Assembly 22. Sta-Strap
29. Retainer Ring
7. Step Assembly 16.
Axle Nut 23. Strut Assembly
30. Bushing
8. Hose 31. Main Gear Spring
9. Bracket
Figure
5-1. Main
Landing Gear
5-4
Revision
1