As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER CABIN FUSELAGE FRAME AT STA 1640 STRINGER 6R IS CHAFFED. R EPORTED BY V921209 REPAIRED UPPER CABIN FUSELAGE FRAME @ STA 1640 BETWEEN STR 5R & 6R IAW AMES DOCUMENT 47527REA02 AND UAL EC/RA 5302-01035. REF NO N-ROUTINE 151186-0200-0129 FOR DETAILS