As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER GEAR RETRACTION LOSS OF HYD SYST. A; HYD A ENG1 AND ELEC2 LOW PRESSURE LIGHTS; FLT CTRL A LOW PRESSURE LIGHTS AND FEEL DIFF PRESS LIGHTS ALL ILLUMINATED AND HYDR A QRT WAS ZERO<[01] FOUND MAIN GEAR RETRACT PRESSURE FUSE LEAKING. R/R MAIN GEAR RETRACT FUSE PER AMM 32-32-21. UP TO SUBTASK E FOR INSTALLATION.