As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CORRODED BETWEEN BS 907 AND BS 967, BETWEEN STRINGER 4 RT AND STRINER 5 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 902.5 TO BS 914, BETWEEN STRINGER 4 RT AND STRINGER 5 RT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. REMOVED CORROSION FROM BS 907 TO BS 967 PER SRM 51-10-6. FOUND WITHIN LIMITS PER SRM 51-30-1 FIG 1. (M)