What was found
SEVERAL CORRODED POINTS ON INNER FUSELAGE SKIN DOUBLER BETWEEN BS 446 - 484 AND LONGERON 25-26L. THE DOUBLER WAS REPLACED IAW SRM 53-04-5, FIG 9 51-30-2, AND 51-10-3, PAR 14-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SEVERAL CORRODED POINTS ON INNER FUSELAGE SKIN DOUBLER BETWEEN BS 446 - 484 AND LONGERON 25-26L. THE DOUBLER WAS REPLACED IAW SRM 53-04-5, FIG 9 51-30-2, AND 51-10-3, PAR 14-21.