What was found
CORROSION OUT LIMITS ON FUSELAGE SKIN BS 1118 BETWEEN LONGERONS 27 - 28L. SKIN WAS REPAIRED IAW SRM 53-04, FIG 57 AND SRM 51-10-3, PAR 14, 21 SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION OUT LIMITS ON FUSELAGE SKIN BS 1118 BETWEEN LONGERONS 27 - 28L. SKIN WAS REPAIRED IAW SRM 53-04, FIG 57 AND SRM 51-10-3, PAR 14, 21 SRM 51-30-5.