What was found
L/H VERT TO FUSELAGE ANGLE IS CRACKED AT FR 76.(CRACK APROX 1 INCH LONG) -C/A-INSTALLED NEW ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H VERT TO FUSELAGE ANGLE IS CRACKED AT FR 76.(CRACK APROX 1 INCH LONG) -C/A-INSTALLED NEW ANGLE IAW SRM 51-40-02.