What was found
INSPECTION FOUND FUSELAGE SKIN HAD ELONGATED HOLES AT LT VERTICAL FIN ATTACH ANGLE AREA. ALL HOLES WERE REAMED, FILLER WAS FABRICATED AND INSTALLED, AND EDDY CURRENT WAS PERFORMED IAW ECRA 5330-02692.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN HAD ELONGATED HOLES AT LT VERTICAL FIN ATTACH ANGLE AREA. ALL HOLES WERE REAMED, FILLER WAS FABRICATED AND INSTALLED, AND EDDY CURRENT WAS PERFORMED IAW ECRA 5330-02692.