What was found
(CAN) AN OUTER FUSELAGE CRACK WAS DISCOVERED AT STRINGER S-18R, STATION 750, APPROXIMATELY 1.125 INCHES LONG. THE CRACK WAS REPAIRED IAW SRM 53-30-3 FIGURE 48, DETAIL IX AND DETAIL XIX.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) AN OUTER FUSELAGE CRACK WAS DISCOVERED AT STRINGER S-18R, STATION 750, APPROXIMATELY 1.125 INCHES LONG. THE CRACK WAS REPAIRED IAW SRM 53-30-3 FIGURE 48, DETAIL IX AND DETAIL XIX.