As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF APU INLET, CORROSION FOUND ON UPPER AND LOWER ANGLES REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW 53-00-04-1A ORIGINAL MATERIAL THICKNESS = 0.063" REMOVED MATERIAL = 0.032" UPPER AND LOWER ANGLES REPLACED IAW SRM 51-40-02 AND BOEING DRAWING NUMBERS 148N3152 AND 148N3105..