What was found
PILOT REPORTED AN UNSATISFACTORY INDICATION OF RT ENGINE ANTI-ICE SYSTEM. AFTER REMOVING ENGINE COWLING, ANTI-ICE VALVE BLEED AIR SUPPLY LINE CONNECTOR HOSE WAS FOUND TO BE RUPTURED AND COMPLETELY TORN FREE. ANTI-ICE VALVE BLEED AIR SUPPLY LINE HAD ALSO CRACKED AT WELD AROUND THE MOUNTING FLANGE AND COMPLETELY PULLED AWAY FROM THE ANTI-ICE VALVE. HOT BLEED AIR WAS BLOWING DIRECTLY ON ANTI-ICE VALVE CANON PLUG WHICH MELTED PIN SOLDER, ALLOWED ELECTRICAL WIRE TO PULL OUT OF CANON PLUG INTO ENG COMPARTMENT. NOTE: REPLACEMENT BLEED AIR LINE WAS ORDERED AND DURING AN INSPECTION FOUND TO BE CRACKED AT THE SAME LOCATION (AROUND THE WELD AT THE MOUNTING FLANGE).