What was found
INSPECTION FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STA 900 BETWEEN LONGERON 37L AND 38L. THE CORRODED AREA OF SKIN WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER AND FINGER DOUBLER USING RIVETS IAW SRM 53-20-00 AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STA 900 BETWEEN LONGERON 37L AND 38L. THE CORRODED AREA OF SKIN WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER AND FINGER DOUBLER USING RIVETS IAW SRM 53-20-00 AND 51-31-01.