As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE ON RT AFT PIT CROSSBEAM AT FR 65 TO FR 65 FS 3514 TO FS 3514, AND -Y20 UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-15 FIG 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.