What was found
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 1060 AT LONGERON 12R-12R ATTACH POINT. THE CRACKED AREA OF FRAME WAS CUT OUT IAW SRM 53-03. A NEW FRAME AND SPLICES WERE INSTALLED IAW SRM 51-01-8 AND 51-01, PAGE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 1060 AT LONGERON 12R-12R ATTACH POINT. THE CRACKED AREA OF FRAME WAS CUT OUT IAW SRM 53-03. A NEW FRAME AND SPLICES WERE INSTALLED IAW SRM 51-01-8 AND 51-01, PAGE 1.