What was found
FUSELAGE SKIN AT FRAME 13 CIRCUMFERENTIAL JOINT MID FASTENER HOLE WITH CRACK SIGNAL AT ABOUT STRINGER 23R. REPAIRED IAW EA 6-5330-T0307377 A PART 1. MAJOR REPAIR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT FRAME 13 CIRCUMFERENTIAL JOINT MID FASTENER HOLE WITH CRACK SIGNAL AT ABOUT STRINGER 23R. REPAIRED IAW EA 6-5330-T0307377 A PART 1. MAJOR REPAIR IAW GMM 6-2-100.