What was found
FUSELAGE FRAME IS CRACKED @ BS 500D BETWEEN STRINGER 8L & 9L. FABRICATED & AMP; INSTALLED REPAIR PARTS, IAW F-EA 5310-04716 REV E OP 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME IS CRACKED @ BS 500D BETWEEN STRINGER 8L & 9L. FABRICATED & AMP; INSTALLED REPAIR PARTS, IAW F-EA 5310-04716 REV E OP 2.