As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK IN STRINGER 24 RIGHT UNDER 1010 FRAME. *S/D* STOP DRILLED CRACK PER FED-EX SRM 51-10-1, FABRICATED J-CHANNEL PER FED-EX SRM 53-10-3. ALODINED AND PRIMED PER FED-EX SRM/ MM 51-10-2 AND 51-20-151. INSTALLED J-CHANNEL REPAIR PER FED-EX SRM 53-10-3.