What was found
NUMBER TWO EXHAUST NOZZLE HAS TWO CRACKS. ENGINEERING ORDER 4478A114 ACCOMPLISHED STOP DRILL AS INTERIM REPAIR AND 3 CYCLE REINSPECTION. NOZZLE MUST BE REPLACED BEFORE NEXT A CHECK. THIS EO APPROVED BY FAA 8110-3 DATED 11 JAN 2010.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMBER TWO EXHAUST NOZZLE HAS TWO CRACKS. ENGINEERING ORDER 4478A114 ACCOMPLISHED STOP DRILL AS INTERIM REPAIR AND 3 CYCLE REINSPECTION. NOZZLE MUST BE REPLACED BEFORE NEXT A CHECK. THIS EO APPROVED BY FAA 8110-3 DATED 11 JAN 2010.