What was found
CRACK ON RIGHT LOWER FUSELAGE AFT ANGLE BETWEEN FRAMES 41 AND 42. REPLACED THE ANGLE IAW EO 5313Y037 AND SRM 51-42-11 .
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RIGHT LOWER FUSELAGE AFT ANGLE BETWEEN FRAMES 41 AND 42. REPLACED THE ANGLE IAW EO 5313Y037 AND SRM 51-42-11 .