What was found
AFTER ENG 1 START ELAC 1 PITCH FAULT WAS PRESENTED ON ECAM. IAW AMM 27-92-17 PB 401 PRESS SWITCH HYD FLIGHT CONTROL, 10CE1, WAS REPLACED, TESTED SATISFACTORY. IAW AMM 27-94-34 PB 401 THE SECOND ONE WAS REPLACED, TESTED OK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER ENG 1 START ELAC 1 PITCH FAULT WAS PRESENTED ON ECAM. IAW AMM 27-92-17 PB 401 PRESS SWITCH HYD FLIGHT CONTROL, 10CE1, WAS REPLACED, TESTED SATISFACTORY. IAW AMM 27-94-34 PB 401 THE SECOND ONE WAS REPLACED, TESTED OK.