THRUSH S2R – G10 Maintenance Manual page 106

Single cockpit and dual cockpit
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THRUSH AIRCRAFT, INC – MODEL S2R-G10
AIRCRAFT MAINTENANCE MANUAL
Figure 6-3: Brake Disc and Lining Inspection Criteria
Rivet Acceptance Criteria
1 The split shall not occur inside the crest of the clenched surface.
2 No more than two splits shall occur in a 90° area.
3 A total of no more than three splits shall be allowed.
Figure 6-4
6-9
Effective: 03/26/2010
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