What was found
TOP PANEL LBL20 STIFFENER FOUND CRACKED AT BS 290, CRACK LENGTH 1/2". NWW BS 290 LBL20 TOP PANEL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TOP PANEL LBL20 STIFFENER FOUND CRACKED AT BS 290, CRACK LENGTH 1/2". NWW BS 290 LBL20 TOP PANEL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.