What was found
4 INCH LONG CRACK NEAR BASE OF NR 2 COMM ANTENNA, IN FUSELAGE SKIN. REPAIRED BY INSTALLING EXTERNAL DOUBLER IAW AERODESIGN ENGINEERING REPORT NR 6586-1 AND BSRM 51-40-02. LT PN 129-430065-1, PANEL ASSY-LT BONDED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
4 INCH LONG CRACK NEAR BASE OF NR 2 COMM ANTENNA, IN FUSELAGE SKIN. REPAIRED BY INSTALLING EXTERNAL DOUBLER IAW AERODESIGN ENGINEERING REPORT NR 6586-1 AND BSRM 51-40-02. LT PN 129-430065-1, PANEL ASSY-LT BONDED.