What was found
DURING CORROSION REMOVAL CRACK WAS FOUND AT CUSP WEB STA Y=660 X=60. IN REF CARD 00278. (S/N 00525). CUSP WEB WAS REPAIRED PER SRM 53-00-55 FIG 126 HFEC WAS ACCOMPLISHED AND NO CRACKS WAS FOUND AFTER CUT OUT PER NDT SPM 06-10-01.001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CORROSION REMOVAL CRACK WAS FOUND AT CUSP WEB STA Y=660 X=60. IN REF CARD 00278. (S/N 00525). CUSP WEB WAS REPAIRED PER SRM 53-00-55 FIG 126 HFEC WAS ACCOMPLISHED AND NO CRACKS WAS FOUND AFTER CUT OUT PER NDT SPM 06-10-01.001.