Colorado Aviation Accidents & Incidents

On May 28, 2021, about 1040 mountain daylight time, a Pipistrel Alpha Trainer, N119JP, was substantially damaged when it was involved in an accident near Fort Collins, Colorado. The pilot/airplane owner sustained minor injuries and the flight instructor sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.
The flight instructor reported that the purpose of the flight was to give the pilot a flight review. He reported that they took off and proceeded to a practice area where they conducted flight review maneuvers, emergency procedures, and the flight instructor demonstrated a power on stall. The pilot took over the controls and when he added power, the engine did not respond. He manipulated the throttle several times, but the engine power had reduced to idle and would not change. The pilot informed the flight instructor that the throttle cable was loose at which time the flight instructor took control of the airplane. The flight instructor initiated an emergency landing. The airplane descended to a nearby field and touched down. The nosewheel sank into a small ridge and the airplane flipped upside down and slid to a stop. The airplane exhibited substantial damage to the fuselage structure and empennage.
This engine has two carburetors; each carburetor has a throttle and choke. The throttle cables from each carburetor run to the throttle/choke assembly where they attach to a splitter. On the other side of the splitter is one cable that runs to the cockpit control. The same design is used for the choke.
During a postaccident examination by the Federal Aviation Administration, the throttle cable from the cockpit appeared to fracture near the throttle/choke assembly. As installed, this cable did not have any abnormal or abrupt bends, nor did it show indications of rubbing on other engine components. The only damage to the cable was near the area of the fracture. The throttle/choke assembly, along with the throttle and choke cables, were removed from the engine and shipped to the National Transportation Safety Board materials laboratory for further examination.
Examination of the throttle/choke splitting assembly revealed the single throttle input cable, which runs to the cockpit control, separated within the terminal fitting end of the splitter assembly, thereby disabling the throttle control. The throttle control input cable is coated with flux paste, inserted into a terminal fitting, clamped with a set screw, and joined to the terminal by solder introduced through a hole at the forward end of the terminal. The terminal is then inserted into a through-hole on the side of the splitter fitting. The metallurgical examination of the throttle control cable’s input terminal fitting revealed a void where the solder had not filled the joint. The throttle cable strands showed indications of progressive cracking over time. In addition, the edges of some of the threads were flattened,