What was found
AFTER ENGINE START ELEC C1 PUMP FAULT, WAS CARRY OUT PROCEDURE IAW FAULT CODE DMC-B787-A-24-10-F5-H1A-421A-A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER ENGINE START ELEC C1 PUMP FAULT, WAS CARRY OUT PROCEDURE IAW FAULT CODE DMC-B787-A-24-10-F5-H1A-421A-A