What was found
NUMBER TWO EXHAUST NOZZLE HAS A CRACK. ENGINEERING ORDER 4478A115 & FAA 8110-3 DATED 19 JAN 2010. ACCOMPLISHED TO STOP DRILL CRACK AS INTERIM REPAIR & DVI EVERY 3 FLIGHT CYCLES. NOZZLE MUST BE REPLACED BEFORE NEXT A-CHECK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMBER TWO EXHAUST NOZZLE HAS A CRACK. ENGINEERING ORDER 4478A115 & FAA 8110-3 DATED 19 JAN 2010. ACCOMPLISHED TO STOP DRILL CRACK AS INTERIM REPAIR & DVI EVERY 3 FLIGHT CYCLES. NOZZLE MUST BE REPLACED BEFORE NEXT A-CHECK.