As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV3, AFT ACCESSORY COMPT STA 1446 L17R CANTED FRAME HAS APPROX .1250" CRACK. REMOVED RT PYLON T/E WEDGE FOR FASTENER ACCESS. TRIMMED OUT DAMAGED AREA 1.0" X .75" FABRICATED AND INSTALLED REPAIR DOUBLER AND INSTALLED T/E WEDGE IAW SRM 51-30-1, 51-30-2 AND 51-70-5 FIG 1, 53-14-4 FIG 3.