What was found
CRACK IN TOOLING HOLE ON FORWARD FRAME OF C2 CARGO DOOR AT STRINGER 20R. THE FRAME WAS REPLACED IAW SRM 51-10-02, REV 113, PAGE 8, PARA 8, 51-40-02, PARA 4, PAGE 2, PAGE 4, PARA 7, AND DWG. 65-47959, REV D, SHEET 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN TOOLING HOLE ON FORWARD FRAME OF C2 CARGO DOOR AT STRINGER 20R. THE FRAME WAS REPLACED IAW SRM 51-10-02, REV 113, PAGE 8, PARA 8, 51-40-02, PARA 4, PAGE 2, PAGE 4, PARA 7, AND DWG. 65-47959, REV D, SHEET 5.