AYRES
AYRES S2R series and Model 600 S2D airplanes (Docket No. 98-CE-56-AD) - proposes to supersede AD 97-17-03, which currently requires inspecting the 1/4-inch and 5/16-inch bolt hole areas on the lower spar caps for fatigue cracking, and replacing any lower spar cap where fatigue cracking is found...
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