What was found
FUSELAGE FRAME AT BS 616, 7 INCHES BELOW STRINGER 17R INNER CHORD HAS CRACK RUNNING FROM TIP THROUGH 2 FASTENER HOLES. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE AND FILLER REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT BS 616, 7 INCHES BELOW STRINGER 17R INNER CHORD HAS CRACK RUNNING FROM TIP THROUGH 2 FASTENER HOLES. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE AND FILLER REPAIR.