What was found
RIGHT OVERWING FRAME INNER CHORD CRACKED THROUGH LOWER FASTENER HOLE AT BS 616 MID CABIN AREA. *S/D* REMOVED CRACK, FABRICATED STIFFENER ANGLE & FILLER AND INSTALLED REPAIR PER AMM 53-11-89.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT OVERWING FRAME INNER CHORD CRACKED THROUGH LOWER FASTENER HOLE AT BS 616 MID CABIN AREA. *S/D* REMOVED CRACK, FABRICATED STIFFENER ANGLE & FILLER AND INSTALLED REPAIR PER AMM 53-11-89.