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.STA827 L= 0.5" FABRICATED ANGLES PER EA 5310-04716 REV F STEP 9 FIG 3 STEP 9 FIG 3 AND NR-51-008. INSTALLED REPAIR PARTS. ACP RII INSPECTION PER ALL CRITICAL STEPS IN GMM09-25-05.