As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
APU INLET PANEL SUPPORT ANGLE HAS EVIDENCE OF CORROSION AT ANCHOR NUT ATTACH POINT LOCATED AT BS 1790 S6R CORROSION REMOVED IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-04- 1A ORIGINAL MATERIAL THICKNESS = 0.063" REMOVED MATERIAL = 0.030". SUPPORT ANGLE AT BS 1790 REPLACED IAW SRM 51-40-02 AND BOEING DRAWING # 148N3105.