What was found
HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE RT UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 16-17 AND STRINGERS 10AR-11R. REPAIRED PER SRM 530000-300-803-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE RT UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 16-17 AND STRINGERS 10AR-11R. REPAIRED PER SRM 530000-300-803-A01.