As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FWD SIDE OF FUSELAGE HAS 4EA DENTS AFT OF RADOME AT APPROX FS 211 L21L . REMOVED 2EA FASTENERS FOUND WITHIN 0.5" OF DENT PERIPHERY AT LT FUSELGE SKIN BETWEEN FRAMES 199.09/215.25 AND STGR 23L IAW SRM 51-40-02-0G-0. INSTALLED 2EA FASTENERS AT LT FUSELGE SKIN BETWEEN FRAMES 199.09/215.25 & STGR 23L IAW SRM 51-40-02-0G-0 & EA 757-5310-01-B0559, REV P1, STEP 9.