As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIRED 2.5 INCH LONG SKIN CRACK AT FUSELAGE BS 937 STRINGER 26R. CONFIRMED 2.5 INCH REMOVED USING HFEC METHOD. THE REPAIR CONSISTED OF CUTTING OUT THE SKIN CRACK AND FABRICATING A DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)