What was found
LEVEL 2 CORROSION, FUSELAGE SKIN CORRODED BETWEEN BS 1530 AND BS 1540 BETWEEN LONGERON 36 AND LONGERON 34 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 2 CORROSION, FUSELAGE SKIN CORRODED BETWEEN BS 1530 AND BS 1540 BETWEEN LONGERON 36 AND LONGERON 34 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)