What was found
ON APPROACH, GOT A FLAPS FAIL AMBER CAS, WHEN SELECTING FLAPS 1. RAN QRC AND CAS EXTINGUISHED. SELECTED FLAPS 1 AND GOT THE FLAPS FAIL AMBER CAS AGAIN. DISCONNECTED FLAP POWER BOX CONNECTOR, DISCONNECTED LT & RT INBOARD FLEX SHAFTS FROM PCU'S, DISCONNECTED OB RH AND LH FLAP ACTUATOR BRAKE CONNECTORS, &FOUND RIGGING THROUGH GARMIN FOR POSITION 1 (FLAPS UP) GREEN AND DID NOT NEED A ELECTRICAL RE-RIG. IAW MM 27-50-00. REVIEWED ARES DOWNLOADS AND ADVISED THAT THE FLAP MOTOR AMPERAGE WAS AT 300+ AMPS WHEN FAULT OCCURRED. SUSPECT A LOCKED ACTUATOR BECAUSE OF FLAPS NOT BEING RIGGED CORRECTLY. INSPECT FLAPS UPON ARRIVAL & NOTICED THAT FLAP PANELS ON BOTH WINGS WERE ABOVE BEING FLUSH WITH THE TOP OF WING. PERFORMED FLAP CONTROL SYS RIGGING & FLAP CONTROL SYS ELECTRICAL RIGGING PROCEDURES IAW MM 27-50-00. OPS FLAPS MULTIPLE TIMES & FLAPS DID NOT FAIL AGAIN. COMPLETED RIG CHECK OF LT & RT WING INBD & OTBD FLAP STOPS. FOUND STOPS TO BE WITHIN LIMITATIONS. IAW MM 27-50-00 (REV 14) COMPLETED FLAP TRAVEL CHECKS. TRAVEL CHECKS FOUND WITHIN LIMITATIONS. COMPLETED SEVERAL FULL FLAP ACTUATIONS FROM MULTIPLE VARIOUS POSITIONS & FULL TRAVELS. NO FAULTS FOUND AT THIS TIME. IAW MM 27-50-00 (REV 14).