What was found
NR 2 ENGINE CONTROL SYS FAULT. IAW TSM 73-21-78-810-816A, REMOVED WATER FROM P30 PRESSURE TUBE AND RECONNECTED. NO FURTHER FAULTS NOTED. IAW FIM OK FOR SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE CONTROL SYS FAULT. IAW TSM 73-21-78-810-816A, REMOVED WATER FROM P30 PRESSURE TUBE AND RECONNECTED. NO FURTHER FAULTS NOTED. IAW FIM OK FOR SERVICE.