What was found
AFT FUSELAGE INT TAIL AREA FOUND CRACK AT CANTED FRAME RT AREA STA 1178.225 BETWEEN STA 16R AND 17R. INSTALLED FORMER ANGLE REPAIR PER SRM 51-70-11 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE INT TAIL AREA FOUND CRACK AT CANTED FRAME RT AREA STA 1178.225 BETWEEN STA 16R AND 17R. INSTALLED FORMER ANGLE REPAIR PER SRM 51-70-11 FIG 201.