What was found
CLT - Q6 - 3/16" CRACK IN FWD SIDE OF FRAME IN PENETRATION HOLE AND 3/16" HOLE IN FRAME ANGLE AT BS 500C BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R IAW B737 SRM SRM 53-00-07.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q6 - 3/16" CRACK IN FWD SIDE OF FRAME IN PENETRATION HOLE AND 3/16" HOLE IN FRAME ANGLE AT BS 500C BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R IAW B737 SRM SRM 53-00-07.