What was found
NOSE W/W TOP PANEL BS 265-280 LBL 20 STIFFENER RADIUS FOUND CRACK APPROX 3/4" LONG. NOSE W/W TOP PANEL BS 265-280 LBL 20" STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NOSE W/W TOP PANEL BS 265-280 LBL 20 STIFFENER RADIUS FOUND CRACK APPROX 3/4" LONG. NOSE W/W TOP PANEL BS 265-280 LBL 20" STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.