What was found
RH ENG IGNITOR #2 INOP. PERFORMED OPERATIONAL TEST OF IGNITION CONTROL SYSTEM RIGHT ENGINE, OPERATES NORMAL PER REF B767 AMM 74-00-00, REMOVED AND REPLACED #2 IGNITOR PLUG IAW AMM 74-21-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RH ENG IGNITOR #2 INOP. PERFORMED OPERATIONAL TEST OF IGNITION CONTROL SYSTEM RIGHT ENGINE, OPERATES NORMAL PER REF B767 AMM 74-00-00, REMOVED AND REPLACED #2 IGNITOR PLUG IAW AMM 74-21-02.