What was found
CORROSION FOUND ON THE AFT FUSELAGE SKIN NEAR FS779, STR23R, 21R AND BL0.00 OUTSIDE OF LIMITS. NOMINAL THICKNESS 0.060 IN. MINIMUM 0.033 IN. MATERIAL TYPE 2024-T42 PER AMS-QQ-A-250/5. FOUND DURING 96 MONTH INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION FOUND ON THE AFT FUSELAGE SKIN NEAR FS779, STR23R, 21R AND BL0.00 OUTSIDE OF LIMITS. NOMINAL THICKNESS 0.060 IN. MINIMUM 0.033 IN. MATERIAL TYPE 2024-T42 PER AMS-QQ-A-250/5. FOUND DURING 96 MONTH INSPECTION.