As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON STRINGER 21 RIGHT, BETWEEN FRAMES 19 AND 20 AND ALSO BETWEEN FRAMES 21 AND 22. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAGE REPAIR AND REPLACEMENT. (M)