What was found
LOSS OF NR 2 HYDRAULIC QUANTITY IN FLIGHT WITH ASSOCIATED NR 2 ISO VALVE LIGHT AND OB ROLL SPOILER CAUTION LIGHT. NR 2 HYDRAULIC QUANTITY REMAINED AT 2 QUARTS. FOUND TUBE LEAKING AT NR 2 STAY STRUT ACTUATOR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOSS OF NR 2 HYDRAULIC QUANTITY IN FLIGHT WITH ASSOCIATED NR 2 ISO VALVE LIGHT AND OB ROLL SPOILER CAUTION LIGHT. NR 2 HYDRAULIC QUANTITY REMAINED AT 2 QUARTS. FOUND TUBE LEAKING AT NR 2 STAY STRUT ACTUATOR.