As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 94 TO 110 AT LONGERON 24L AND ON THE T-CAP, FS 110 BETWEEN LONGERONS 24L TO 27R. REPAIRED SKIN (P/N 991911509-85) AND T-CAP (P/N 5911400) PER EA 99-102691.