What was found
LOWER FUSELAGE FRAME SECTORS AT FS 847.00 + 16 & FS 847.00+32, BETWEEN STRINGERS 26L AND 26R FOUND TO BE CORRODED BEYOND REPAIRABLE LIMITS. BOTH LOWER FRAME SECTORS REPLACED IAW APPLICABLE SRM'S.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE FRAME SECTORS AT FS 847.00 + 16 & FS 847.00+32, BETWEEN STRINGERS 26L AND 26R FOUND TO BE CORRODED BEYOND REPAIRABLE LIMITS. BOTH LOWER FRAME SECTORS REPLACED IAW APPLICABLE SRM'S.