As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1 1/2 INCH CRACK IN THE UPPER AFT CORNER OF THE CUTOUT, FOR THE FWD ACCESS PANEL, ON THE O/B SIDE OF THE RIGHT ENGINE PYLON.#6204 REF AMES NR 167037-0400-0184. CRACK IN UPPER AFT CORNER OF CUTOUT REPAIRED IAW B767 SRM 54-53- 01-2R-G REPAIR 6 SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKS HEET 21 PAGE 1-3