What was found
(CAN) CREW REPORTED TRAILING EDGE FLAP ASSYMETRY OCCURED BETWEEN 1 AND 0 WHEN SELECTED FOR APPROACH. L/H #1 SKEW SENSOR WAS REPLACED, P/N : 9000421-2 S/N: 12506. SYSTEM TESTED SERVICEABLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CREW REPORTED TRAILING EDGE FLAP ASSYMETRY OCCURED BETWEEN 1 AND 0 WHEN SELECTED FOR APPROACH. L/H #1 SKEW SENSOR WAS REPLACED, P/N : 9000421-2 S/N: 12506. SYSTEM TESTED SERVICEABLE.