What was found
CLT - INSPECTION VISUALLY FOUND A 1 INCH CRACK LOCATED AT BS 500B FRAME INNER CHORD (FORMED SECTION AT S24R). INSTALLED DOUBLER PER BOEING SRM 51-40-03, FIG 1. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - INSPECTION VISUALLY FOUND A 1 INCH CRACK LOCATED AT BS 500B FRAME INNER CHORD (FORMED SECTION AT S24R). INSTALLED DOUBLER PER BOEING SRM 51-40-03, FIG 1. (X)