What was found
(CAN) DURING GEAR RETRACTION ALL APPROPRIATE CAUTION LIGHTS INDICATING FAILURE OF #2 HYDRAULIC SYSTEM CAME ON. THE NOSE LANDING GEAR DRAG STRUT ACTUATOR FLEX UP LINE WAS FOUND RUPTURED, CAUSING A LOSS OF FLUID IN #2 SYSTEM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING GEAR RETRACTION ALL APPROPRIATE CAUTION LIGHTS INDICATING FAILURE OF #2 HYDRAULIC SYSTEM CAME ON. THE NOSE LANDING GEAR DRAG STRUT ACTUATOR FLEX UP LINE WAS FOUND RUPTURED, CAUSING A LOSS OF FLUID IN #2 SYSTEM.