What was found
CORROSION IN R/H AFT BEAM FR. 87. REMOVED CORROSION BY BLENDING FOUND TO BE .045" MATERIAL LOSS NOMINAL THICKNESS .071" FOUND TO BE OUT OF LIMITS. INSTALLED FABRICATED DOUBLER IAW SRM 53-23-10 REPAIR 03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION IN R/H AFT BEAM FR. 87. REMOVED CORROSION BY BLENDING FOUND TO BE .045" MATERIAL LOSS NOMINAL THICKNESS .071" FOUND TO BE OUT OF LIMITS. INSTALLED FABRICATED DOUBLER IAW SRM 53-23-10 REPAIR 03.