As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IN REF CARD 5720-01100-02A STEP. 28, LT ENG DRAG FTG CLAMP, CORROSION POINTS ON FASTENER HOLE NR 2. LEVEL 2 CORROSION ON FASTENER HOLE NR 2 WAS REAMED AT FINAL DIMENSION 0.5780 PER CARD 5720-01100-02A STEP 29. INSPECTION HFEC WAS ACCOMPLISHED, NO CRACKS WERE FOUND AFTER REWORKED IAW AMDS 5720-01100-02A STEP 30 AND IAW NDT MANUAL PART 6, 51-00-16. (LP 1697830 - AIRCRAFT WAS GROUNDED).