As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN AND STRINGER REPAIR AT BS 341, STRINGER 27L. TO REPAIR THE CORRODED SKIN AND STRINGER 27L AT BS 341. CUT-OUT OF THE CORRODED SKIN AND REPAIR PER A&B OVERHAUL MANUAL FIGURE 12-22. CUT STRINGER 27L BETWEEN BS 332 AND 350. REPAIR PER A&B OVERHAUL MANUAL FIGURE 12-2.