What was found
FUSELAGE INTERIOR LONGERON SPLICE FITTING CRACKED AT FS 680.5, RIGHT LONGERON 10 AT UPPER NUT ANGLE. MAINTENANCE REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE INTERIOR LONGERON SPLICE FITTING CRACKED AT FS 680.5, RIGHT LONGERON 10 AT UPPER NUT ANGLE. MAINTENANCE REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.