What was found
FUSELAGE FRAME IS CRACKED @ BS 440 BETWEEN STRINGER 8R & 9R. CUT OUT CRACKS & INSTALLED REPAIR ANGLES IAW EA 5310-04716 REV E - OPERATION 02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME IS CRACKED @ BS 440 BETWEEN STRINGER 8R & 9R. CUT OUT CRACKS & INSTALLED REPAIR ANGLES IAW EA 5310-04716 REV E - OPERATION 02.