As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NOSE WHEEL WELL ACCESS PANEL 114AC HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-10-14. ORG THICK 0.060. REMOVED 0.004 REMAINING THICK 0.056. WITH IN LIMITS IAW B737-800 SRM 53-10-14. ALODINED IAW B737-800 AMM 51-21-41. PRIMED IAW B73-800 SRM 53-10-14. APPLIED TOP COAT IAW B737-800 AMM 51-21-73 THIS IS A CAT B REPAIR DVI REQUIRED EVERY 6,600 FLIGHT CYCLES IAW B737--800 SRM 53-10-14.