As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND AT FRAME "0" DURING AN INSPECTION BELOW THE NOSE CONE FAN BOX. IAW E-MAIL FROM MFG ENGINEERING AT FRAME 0, EVALUATION OF AREA AFTER BLENDING OF CORROSION ITEM A AND D WILL REQUIRE A REPAIR. USED REPAIR DWG F2MA2110010A5 EO1-1 FOR THIS REPAIR. FOR AREAS B AND C AT FRAME 0 THE THICKNESS REMAINING IS STRUCTURALLY ACCEPTABLE IAW DFJ LETTER F2000 53-20-2-220 DATED 8/23/16. RESTORED PAINT PROTECTION.