What was found
INITIAL INSPECTION: CRACK ON AFT ANGLE BTW INNER SKIN AND SIDE STEPS PANEL. (L1). SUMMARY: AFT DRAG ANGLE BTW INNER SKIN AND SIDE STEPS PANEL WAS REPAIRED PER SRM 52-11-04-201-002-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INITIAL INSPECTION: CRACK ON AFT ANGLE BTW INNER SKIN AND SIDE STEPS PANEL. (L1). SUMMARY: AFT DRAG ANGLE BTW INNER SKIN AND SIDE STEPS PANEL WAS REPAIRED PER SRM 52-11-04-201-002-A01.