What was found
NR 1 ENGINE EXHAUST CONE HAS A CRACK A T 9 O'CLOCK. CRACK LOCATED IN ZONE 1 AND IS 7.5 INCHES IN LENGTH. ACP EVA 80212 STOP DRILLED HOLE. CRACK CAN BE WELD REPAIRED IAW SM USING AMS5837 FILLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE EXHAUST CONE HAS A CRACK A T 9 O'CLOCK. CRACK LOCATED IN ZONE 1 AND IS 7.5 INCHES IN LENGTH. ACP EVA 80212 STOP DRILLED HOLE. CRACK CAN BE WELD REPAIRED IAW SM USING AMS5837 FILLER.