What was found
DURING ENGINE START PROCEDURES, RIGHT FWD FUEL PUMP EICAS MESSAGE AND PRESS LIGHT WHEN SWITCH TURNED ON. REMOVED AND REPLACED THE FUEL PRESSURE SWITCH IAW AMM 28-42-01. OPS TESTED OK, LEAK CHECKED OK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ENGINE START PROCEDURES, RIGHT FWD FUEL PUMP EICAS MESSAGE AND PRESS LIGHT WHEN SWITCH TURNED ON. REMOVED AND REPLACED THE FUEL PRESSURE SWITCH IAW AMM 28-42-01. OPS TESTED OK, LEAK CHECKED OK.