What was found
NR 1 ENGINE FIREWALL ANGLE IS CRACKED AT BOTH ENDS JUST BELOW AFT TOP HEAT SHIELD. REPAIRED IAW DHC-8 SRM 51-40-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE FIREWALL ANGLE IS CRACKED AT BOTH ENDS JUST BELOW AFT TOP HEAT SHIELD. REPAIRED IAW DHC-8 SRM 51-40-11.