Cessna T188C - Page 332

MODEL
188
& T188
SERIES
SERVICE
MANUAL
7
2
11 1
>
NON-SHOCKMOUNTED
188-0001 THRU
188-0049 EXCEPT
WHEN
I
MODIFIED
PER
SK210-84
11
5
9
SHOCKMOUNTED
2 7r 188-0050 THRU 18801424 EXCEPT WHEM
8
/
MODIFIED
PER
SK210-84
7
B
3
2
1
IWARNING
1
2
On
Models manufactured
prior to mid
1971
should alternator
thru-bolt
loosening
or
breaking
occur,
Cessna Service
Letter
SE71-40
dated
November
24,
1971
should
be complied
with.
On
models
manufactured
after
mid
1971
a
new
high
strength
thru-
bolt and
a
K shaped
retainer
are
installed.
1
Torque
bolts 45 to
55 pound-inches.
2
97
1. Bolt.
2. Washer
\
3.
Arm - Adjusting
/
4. Belt
- Alternator
NON-SHOCKMOUNTED
5.
Alternator
Assembly
.,
5.
Alternator
Assembly
2
18801425
THRU
18802256
EXCEPT
WHEN
6.
N
,ut
/
~
'S
i
MODIFIED
PER
SK210-84
7. Support Assembly
8.
Bushing
- Rubber
9,
Bushing
NON-SHOCKMOUNTED
2
6
10.
Mount
- Bonded
18802257
THRU
18803240
EXCEPT
WHEN
11.
Safety
Wire
MODIFIED
PER
SK210-84
Figure 16-4.
Alternator
Installation (Sheet
1 of 4)
16-28