What was found
NDT INSPECTION SHOWS CRACK AT HOLE NR 24 RT SKIN PANEL FRONT PITCH LOAD FITTING. REPAIRED PITCH LOAD FITTING RT HOLE 24 IAW ECRA 5730-02769. CF-9 WILL BE GENERATED FOR SUPPLEMENTAL INSP AS REQUIRED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NDT INSPECTION SHOWS CRACK AT HOLE NR 24 RT SKIN PANEL FRONT PITCH LOAD FITTING. REPAIRED PITCH LOAD FITTING RT HOLE 24 IAW ECRA 5730-02769. CF-9 WILL BE GENERATED FOR SUPPLEMENTAL INSP AS REQUIRED.