What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On December 28, 2005, at approximately 11:56 am, after the pilot in command selected gear down for landing, only two gear down and locked lights were illuminated. Pilot called tower and asked for a fly by which showed that the left main gear was not down at all. Pilot tried emergency extension but that was of no effect. Pilot executed a gear up landing with engines shut down and propellers feathered. Damage to aircraft from gear up landing was minor. Left main gear was held up by uplock during landing. Cause of left main gear failure to extend was a broken rod end on the retract/extend actuator. This actuator also releases the uplock. Evidence of a pre-existing crack was evident on broken surface of actuator rod. Pmi for western aviators, inc. reviewed the aircraft's maintenance records and found the previous 50 hour, 100 hour, and annual inspections had been complied with within the required times.
As the FAA filed it
(-23) ON DECEMBER 28, 2005, AT APPROXIMATELY 11:56 AM, AFTER THE PILOT IN COMMAND SELECTED GEAR DOWN FOR LANDING, ONLY TWO GEAR DOWN AND LOCKED LIGHTS WERE ILLUMINATED. PILOT CALLED TOWER AND ASKED FOR A FLY BY WHICH SHOWED THAT THE LEFT MAIN GEAR WAS NOT DOWN AT ALL. PILOT TRIED EMERGENCY EXTENSION BUT THAT WAS OF NO EFFECT. PILOT EXECUTED A GEAR UP LANDING WITH ENGINES SHUT DOWN AND PROPELLERS FEATHERED. DAMAGE TO AIRCRAFT FROM GEAR UP LANDING WAS MINOR. LEFT MAIN GEAR WAS HELD UP BY UPLOCK DURING LANDING. CAUSE OF LEFT MAIN GEAR FAILURE TO EXTEND WAS A BROKEN ROD END ON THE RETRACT/EXTEND ACTUATOR. THIS ACTUATOR ALSO RELEASES THE UPLOCK. EVIDENCE OF A PRE-EXISTING CRACK WAS EVIDENT ON BROKEN SURFACE OF ACTUATOR ROD. PMI FOR WESTERN AVIATORS, INC. REVIEWED THE AIRCRAFT'S MAINTENANCE RECORDS AND FOUND THE PREVIOUS 50 HOUR, 100 HOUR, AND ANNUAL INSPECTIONS HAD BEEN COMPLIED WITH WITHIN THE REQUIRED TIMES.
Other reports on N494SC · 3
Matched to the same aircraft by N-number and date.