What was found
AIR TURNBACK, TOTAL LOSS OF B SYSTEM HYDRAULIC FLUID DURING FLAP RETRACTION, AFTER TAKEOFF. R&R NR 2 ELECTRIC HYDRAULIC PUMP NR 2 ENGINE HYDRAULIC PUMP NR 7 HYDRAULIC PUMP NR 7. SPOILER ACTUATOR IAW AMM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AIR TURNBACK, TOTAL LOSS OF B SYSTEM HYDRAULIC FLUID DURING FLAP RETRACTION, AFTER TAKEOFF. R&R NR 2 ELECTRIC HYDRAULIC PUMP NR 2 ENGINE HYDRAULIC PUMP NR 7 HYDRAULIC PUMP NR 7. SPOILER ACTUATOR IAW AMM.