What was found
NOTED CRACK AND/OR HOLE DAMAGE IN LEFT BS 870 TERMINAL FITTING ROW 1 HOLE NR 1. INVESTIGATED DAMAGE. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NOTED CRACK AND/OR HOLE DAMAGE IN LEFT BS 870 TERMINAL FITTING ROW 1 HOLE NR 1. INVESTIGATED DAMAGE. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP.