What was found
FRAME INNER CHORD TRANSITION RADIUS CRACKED. CRACK LENGTH APPROXIMATELY 0.32" ON RT SIDE BS 903.5. L89R BELOW WL 200, REPAIRED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME INNER CHORD TRANSITION RADIUS CRACKED. CRACK LENGTH APPROXIMATELY 0.32" ON RT SIDE BS 903.5. L89R BELOW WL 200, REPAIRED.