As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN S-8R AND S-9R STA 500L L=0.15" FABRICATED ANGLES PER EA 5310-04716 REVF STEP9 FIG3. REMOVED THE DAMAGE PER EA5310-04716 REVF STEP9 FIG3. INSTALLED REPAIR PARTS. ACP RII INSPECTION PER ALL CRITICAL STEP IN GMM09-25-05.