What was found
DURING C-10 INSPECTION, A 3.50 INCH CRACK WAS NOTED IN FS 870 WEB, FORWARD SIDE OF LT MAIN WHEELWELL. REF: C53-100-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-10 INSPECTION, A 3.50 INCH CRACK WAS NOTED IN FS 870 WEB, FORWARD SIDE OF LT MAIN WHEELWELL. REF: C53-100-01.