What was found
INSPECTION FOUND A 1.75 INCH CRACK AT LOWER FASTENER ON FUSELAGE STUB FRAME FORWARD SIDE, STA 616, S16L. THE CRACKED AREA OF FRAME INNER CHORD WAS REMOVED AND A REPAIR ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.75 INCH CRACK AT LOWER FASTENER ON FUSELAGE STUB FRAME FORWARD SIDE, STA 616, S16L. THE CRACKED AREA OF FRAME INNER CHORD WAS REMOVED AND A REPAIR ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.