As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING M-CHECK FOUND THRESHOLD PLATE SUPPORT ANGLE 2 EA AT BS 1640 & 1681 LBL 54 INCHES HAS CORROSION. REMOVED PLATE SUPPORT ANGLE IAW SRM 51-40-02, FABRICATED PLATE SUPPORT ANGLE AND PLATED ANGLE SUPPORT 1 EA LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01, INSTALLED PLATE SUPPORT ANGLE AFT AND FWD IAW SRM 51-40-02.