What was found
FUSELAGE FRAME IS CRACKED AT BS 400 BETWEEN STRINGER 8L-9L. CUT-OUT DAMAGED AREA, FABRICATED REPAIR PARTS & INSTALLED AT FUSELAGE FRAME BS 400 STRINGER 8L-9L 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 AT BS 400 BETWEEN STRINGER 8L-9L. CUT-OUT DAMAGED AREA, FABRICATED REPAIR PARTS & INSTALLED AT FUSELAGE FRAME BS 400 STRINGER 8L-9L IAW EA 5310-04716 REV E.