What was found
CORROSION FOUND ON LOWER FUSELAGE SKIN AT BS 400+6'- 400+15' BTW STR 27L- 26L. IAW EA 26-153-01372; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITH AN INSPECTION THRESHOLD DEFINED IN EA 26-153-01372-DTI.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION FOUND ON LOWER FUSELAGE SKIN AT BS 400+6'- 400+15' BTW STR 27L- 26L. IAW EA 26-153-01372; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITH AN INSPECTION THRESHOLD DEFINED IN EA 26-153-01372-DTI.