What was found
VERTICAL STIFFENER AT FS 218 BETWEEN LONGERONS 24 LT & 23 LT IS CRACKED. REPAIRED STRUT IAW AARD 53-10-00-15.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STIFFENER AT FS 218 BETWEEN LONGERONS 24 LT & 23 LT IS CRACKED. REPAIRED STRUT IAW AARD 53-10-00-15.