As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AT FASTENER HOLE ON UPPER FLANGE OF FRAME AT BS 950C BETWEEN STRINGERS 28R AND 27R. CUT OUT DAMAGED AREA DIM 1 1/4" X 1" IAW SRM 51-40-3 FIG 1, FORMED REPAIR DOUBLER IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 51-40-3 FIG 1 REV 103.