As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REMOVED PREVIOUS REPAIR FUSELAGE FRAME BS 580 STR 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO 9001737 DEM 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED AREA AND PART IAW B727 SRM 51-40-2. INSTALLED NEW FRAME REPAIR IAW B727 SRM 51-40-2 FIG 1.