As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLAP FAIL AMBER CAS DURING APPROACH AND LANDING. FLAPS FAILED AT APROX 2 DEGREES WITH SLATS OUT. FOUND FLAP CONTROL BITE CODE 2. TESTED FLAP PDU IAW MM 27-50-00 CLUTCH TORQUE AMFRAME FAILED- 112 AMPS MAX. FLAP PDU R & R IAW MM 27-52-00 (R35). REMAINDER OF FLAP DRIVE SYS VISUALLY INSPECTED & SYS OPERATIONALLY TESTED & FOUND SERVICABLE.