As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GEAR TILT EICAS MESSAGE AFTER TAKE OFF. PERFORMED A LEAK CHECK AND NO LEAKS NOTED ON HOSE ASSY FOR BODY GEAR TRUCK POSITIONING ACTUATOR. BLED THE ACTUATOR AND PUT THE HYDRAULIC FUSE IN THE NORMAL POSITION IAW AMM 32-13-15-404-010. PERFORMED PSEU GROUND TEST IAW AMM 32-09-03/501. TEST PASSED.