What was found
INBOARD THRUST REVERSER ATTACH ANGLE FORWARD OF CASCADE VANES CRACKED AT 4:00 POSITION AS SEEN WITH SLEEVE DEPLOYED. REMOVED AND REPLACED INBOARD ATTACH ANGLES IAW SRM 51-41-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INBOARD THRUST REVERSER ATTACH ANGLE FORWARD OF CASCADE VANES CRACKED AT 4:00 POSITION AS SEEN WITH SLEEVE DEPLOYED. REMOVED AND REPLACED INBOARD ATTACH ANGLES IAW SRM 51-41-01.