What was found
INSPECTION FOUND A 1.25 INCH CRACK IN RT FUSELAGE FRAME AT STA 312, LONGERON 13R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4, FIGURE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.25 INCH CRACK IN RT FUSELAGE FRAME AT STA 312, LONGERON 13R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4, FIGURE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-0.