What was found
AFTER SECOND ENGINE START ECAM MESSAGE, AIR ENG 1 BLEED FAULT. RETORQUED ALL LINES AND CONNECTOR TO PRESSURE RELIEF VALVE AND PERFORMED TSM 36-11-81-810-908-A. GROUND RUN OK. OK FOR SERVICE. RII ACCOMPLISHED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER SECOND ENGINE START ECAM MESSAGE, AIR ENG 1 BLEED FAULT. RETORQUED ALL LINES AND CONNECTOR TO PRESSURE RELIEF VALVE AND PERFORMED TSM 36-11-81-810-908-A. GROUND RUN OK. OK FOR SERVICE. RII ACCOMPLISHED.