What was found
FORWARD RIB BY UPPER MIDDLE HINGE POINT ON RUDDER 1 HAS A 1/8 INCH CRACK. R & R IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD RIB BY UPPER MIDDLE HINGE POINT ON RUDDER 1 HAS A 1/8 INCH CRACK. R & R IAW SRM 51-40-02.