Cessna 188 Series Service Manual 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