What was found
LEFTHAND FUSE TO VERTICAL FIN CONNECTION ANGLE IS CRACKED AT THE 50 PERCENT SPAR LOCATION. REPAIRED IAW FOKKER SRM 55-31-01, PAGE 2 AND SRM 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFTHAND FUSE TO VERTICAL FIN CONNECTION ANGLE IS CRACKED AT THE 50 PERCENT SPAR LOCATION. REPAIRED IAW FOKKER SRM 55-31-01, PAGE 2 AND SRM 51-31-01.