What was found
CORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN NEAR FS 779 NEAR STR 22L & 23L, NOMINAL THICKNESS 0.060 IN, MINIMUM 0.035 IN. MATERIAL TYPE 2024-T42 PER AMS-QQ-A-250''5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN NEAR FS 779 NEAR STR 22L & 23L, NOMINAL THICKNESS 0.060 IN, MINIMUM 0.035 IN. MATERIAL TYPE 2024-T42 PER AMS-QQ-A-250''5.