As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H WING AFT SPAR STIFFENER JUST I/B OF AFT BOOST PUMP UPPER ATTACH ANGLE IS CRACKED. / [01] REMOVED AND REPLACED ANGLE AT L/W WING AFT SPAR STIFFENER JUST I/B OF AFT BOOST PUMP UPPER ATTACH AS PER B737 SRM 51-40-02-0G-0;[02] VERIFIED 1.