What was found
R/W-O/B MID FLAP COVE PANEL CRACKED AT SUPPORT ARM APPROX 14". AREA IS BETWEEN NR 7/8 CANOE-MARKED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
R/W-O/B MID FLAP COVE PANEL CRACKED AT SUPPORT ARM APPROX 14". AREA IS BETWEEN NR 7/8 CANOE-MARKED.