2.101A. WIDE BAND FM ANTENNA PAN MOUNT FUSELAGE REPAIR (AVIM) continued
b. Repair crack(s).
(1) Trim away cracked aircraft skin or stop drill crack(s) as required (TM 1-1500-204-23).
Rivets around crack repair must have 0.62 INCH minimum edge distance from trim area to end of
(2) Drill new rivet holes (4) equally spaced around crack repair.
(3) Remove all sharp edges.
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