WPR17LA165

During landing, the nose landing gear and right main landing gear collapsed, and the airplane veered off the runway. The pilot stated that it was likely that he switched the hydraulic pump off during the accident flight. Although both the hydraulic switch position and checking the hydraulic system pressure were included in his before-landing checklist, he could not recall their position and indication, respectively, during the accident approach. The pilot also reported that he had been experiencing issues with the landing gear microswitches, and the airplane's landing gear indicator light was inoperative as a result. Postaccident examination of the airplane and landing gear system revealed no evidence of mechanical malfunctions or anomalies that would have precluded normal operation. It is likely that the pilot's failure to properly configure the hydraulic switch, and his subsequent failure to recognize the error during his before-landing check, resulted in inadequate hydraulic pressure to extend and lock the landing gear. The airplane's inoperative landing gear indicator light likely contributed to the pilot's failure to recognize that the landing gear was not fully extended and locked before landing.

On June 25, 2017, about 1310 Pacific daylight time, a Lake LA-4 airplane, N7628L, was substantially damaged when it was involved in an accident near Byron, California. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that, during the approach for landing, he positioned the flaps to the fully extended position. Once established on the approach, he “performed his pre-landing checks, including visual inspection of the landing gear, which looked normal.” The airplane landed normally, and he could feel all three wheels on the ground. Subsequently, the airplane began to sink to the right, followed by a right yaw, then it veered off the right side of the runway. A postaccident examination of the airplane revealed that the nose landing gear and the right landing gear collapsed, and the keel was substantially damaged. The pilot reported that he had experienced issues with the landing gear microswitches failing to close properly on previous flights, which meant that the landing gear down indicator light would not illuminate., Thus, he had to visually confirm that the landing gear was down. He stated that both main landing gear were visible from the cockpit and the nose landing gear was visible from a mirror positioned on the left sponson. The pilot stated that adjustments were made to the microswitches after those flights but that he continued to conduct landings without the landing gear down indicator light being illuminated. He further stated that, for the accident flight, it was most likely that he switched the hydraulic pump off during the flight and didn’t notice the position of the switch or the indicated low hydraulic system pressure during the approach. He stated that both the hydraulic switch position and checking the hydraulic system pressure were part of his before-landing checklist, but he could not recall their position and indication, respectively, during the accident approach. Following the accident, after the airplane was lifted, the right main landing gear was pushed by hand into its down-and-locked position. The nose landing gear locked into position after activating the emergency gear extension pump. There was no evidence of preexisting malfunctions or failures that would have precluded normal operation of the airplane.