What was found
DURING INSPECTION, FOUND A CRACK ON THE ANGLE BETWEEN BS 927 AND 947.5, LBL 1. THE ANGLE WAS REPLACED IAW SRM 51-40-02, PAR 4, AND DWG 147A5430, REV.A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND A CRACK ON THE ANGLE BETWEEN BS 927 AND 947.5, LBL 1. THE ANGLE WAS REPLACED IAW SRM 51-40-02, PAR 4, AND DWG 147A5430, REV.A.