What was found
CRACK BY LENGTH OF 1.378" AT FRAME INNER CHORD TRANSITION RADIUS STA 903.5 RBL 89.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK BY LENGTH OF 1.378" AT FRAME INNER CHORD TRANSITION RADIUS STA 903.5 RBL 89.