As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND 3 INCH CRACK ON THE FUSELAGE SKIN AT BS 887 ALONG STRINGER 24R. CUT OUT DAMAGED PORTION OF SKIN. VERIFIED CRACK REMOVED USING HFEC. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)