What was found
(CAN) 2 INCH CRACK AT S 17R BETWEEN BS 727B AND BS 747 ON RT AFT SIDE OF FUSELAGE. CRACK REPAIRED IAW MFG SRM 53-30-3 FIG 48 PROCEDURE IV AND VII.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) 2 INCH CRACK AT S 17R BETWEEN BS 727B AND BS 747 ON RT AFT SIDE OF FUSELAGE. CRACK REPAIRED IAW MFG SRM 53-30-3 FIG 48 PROCEDURE IV AND VII.