Cessna 182 1978 - Page 489

MODEL
182
&
T182
SERIES
SERVICE
MANUAL
Replace
In
thickness
With
(or
thicker)
MS20426AD5
.090
NAS1399B5,
NAS1399D5
(Countersunk)
.080
CR3212-5
.071
NAS1739B5,
NAS1739E5
.063
NAS1769D5
.050
CR3242-5
(See
Note
1)
.063
NAS1739B6,
NAS1739D6,
NAS1769D6,
CR3212-6
.040
CR3242-6
.032
AN509-10
Screw
with
MS20365
Nut
MS20426AD5
.071
NAS1739B5,
NAS1739D5
(Dimpled)
.090
NAS1739B6,
NAS1739D6,
CR3212-6
MS20426AD6
(Countersunk)
.071
NAS1769D6
.063
CR3242-6
.032
AN509-10
Screw
with
MS20365
Nut
MS20426AD6
.090
NAS1739B6,
NAS1739D6
(Dimpled)
.032
AN509-10
Screw
with
MS20365
Nut
NOTE
1:
Rework
required.
Countersink
oversize
to
accommodate
oversize
rivet.
NOTE
2:
Do
not
use
blind
rivets
in
high-vibration
areas
or
to
pull
heavy
sheets
or
extrusions
together.
High-vibration
areas
include
the
nacelle
or
engine
compartment
including
the
firewall.
Heavy
sheets
or extrusions
include
spar
caps.
18-6B