What was found
CLT - Q-4, VERTICAL STIFFENER CRACKED .5 INCH AFT SIDE BULKHEAD 178, WL 184, LBL 5.7 ON INBOARD SIDE. INSTALLED REPAIR ANGLE AND STRAP PER SRM 53-10-08 FIG 205. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q-4, VERTICAL STIFFENER CRACKED .5 INCH AFT SIDE BULKHEAD 178, WL 184, LBL 5.7 ON INBOARD SIDE. INSTALLED REPAIR ANGLE AND STRAP PER SRM 53-10-08 FIG 205. (X)