What was found
FUSELAGE FRAME IS CRACKED @ BS 500A BETWEEN STRINGER 8R & 9R. INSTALLED REPAIR ANGLES "A&B" IAW EA 5310-04716 REV-E.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME IS CRACKED @ BS 500A BETWEEN STRINGER 8R & 9R. INSTALLED REPAIR ANGLES "A&B" IAW EA 5310-04716 REV-E.