What was found
WING CENTER SECTION, BS 1241 REAR SPAR WEB CORROSION. CORROSION REMOVED FROM WEB AND REWORKED, THIS IS AN APPROVED ALTERNATE METHOD OF COMPLIANCE REF 8110-3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WING CENTER SECTION, BS 1241 REAR SPAR WEB CORROSION. CORROSION REMOVED FROM WEB AND REWORKED, THIS IS AN APPROVED ALTERNATE METHOD OF COMPLIANCE REF 8110-3. (M)