What was found
AFTER AIRCRAFT WAS PARKED, CREW NOTICED HYDRAULIC FLUID LEAKING FROM THE NOSE WHEEL WELL. INVESTIGATION FOUND THE ROD END FITTING, P/N 1159HM20116, WAS CRACKED ON THE NOSE GEAR ACTUATOR ALLOWING COMBINED HYDRAULIC SYSTEM FLUID TO DRAIN. ACTUATOR, S/N 32-105, HAS BEEN SENT TO GAC, SAV FOR EVALUATION. (M)