What was found
FUSELAGE FRAME IS CRACKED @ BS 400 BETWEEN STRINGER 8R & 9R. FABRICATED & AMP; INSTALLED REPAIR PARTS, IAW 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 400 BETWEEN STRINGER 8R & 9R. FABRICATED & AMP; INSTALLED REPAIR PARTS, IAW EA 5310-04716 REV E OP 2.