What was found
LT ATTACH ANGLE FOR VERTICLE TO FUSELAGE IS CRACKED AT STA 1474. INSTALLED REPAIR ON ATTACH ANGLE PER SRM 53-05 FIG 23 AND SRM 53-05 FIG 23A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT ATTACH ANGLE FOR VERTICLE TO FUSELAGE IS CRACKED AT STA 1474. INSTALLED REPAIR ON ATTACH ANGLE PER SRM 53-05 FIG 23 AND SRM 53-05 FIG 23A.