What was found
CRACK ANGLE AT ACCESS PANEL 651GB, RT WING. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A2714, SHEET 14, REV-. MEASUREMENT OF CRACK: L= 0.440.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ANGLE AT ACCESS PANEL 651GB, RT WING. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A2714, SHEET 14, REV-. MEASUREMENT OF CRACK: L= 0.440.