As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LG WOW SYS FAIL. PERFORMED NLG SHOCK STRUT SERVICING IAW AMM 12-12-09. DURING RELEASE OF NITROGEN AND HYDRAULIC FLUID, FOUND NO FLUID IN NLG SHOCK STRUT. WO REMAINS OPEN. GEAR SWING REQUIRED. PERFORMED FUNCTIONAL TEST OF THE LG EXTENSION AND RETRACTION SYSTEM IAW AMM 32-33-00. OP'S CHK GOOD. OK FOR SVC.