What was found
ON CLIMBOUT WHEN FLAPS RETRACTED TO ZERO, INBOARD FLAPS REMAINED AT 2 UNITS. A SYSTEM QUANTITY AND PRESSURE WAS ZERO. RETRACTED FLAPS AND CONTINUED TO ORD. *S/D* REPLACED INBOARD FLAP HYDRAULIC MOTOR, SYSTEM OPS CHECKS OK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON CLIMBOUT WHEN FLAPS RETRACTED TO ZERO, INBOARD FLAPS REMAINED AT 2 UNITS. A SYSTEM QUANTITY AND PRESSURE WAS ZERO. RETRACTED FLAPS AND CONTINUED TO ORD. *S/D* REPLACED INBOARD FLAP HYDRAULIC MOTOR, SYSTEM OPS CHECKS OK.