Teledyne Continental Motors, Inc.
TM
Non-Overhaul Removal and Replacement
IOF-550 Permold Series Engine Maintenance Manual
10-21
1 April 2007
5.
Apply tension to v-belt (20) by raising the alternator (19) to allow no more than 0.11
inch deflection at the center of the span; tighten the tension bolts (4, 7) to maintain
belt tension. Torque the bolts (4, 7, and 9) to Appendix B specifications.
6.
Perform and “Engine Start” according to instructions in Chapter 7 of OI-24 and verify
proper alternator output according to the Aircraft Maintenance Manual.
1
2,3
9
4
5
6
7
5
8
13
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11
18
10
10
18
17
16
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27
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29
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27
26
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1
2,3
9
4
5
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7
5
8
13
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11
18
10
10
18
17
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27
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29
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24
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20
19
Figure 10-8 repeated for reference
