CEN24LA060

Factual narrative

On December 11, 2023, about 1930 central standard time, a Piper PA24-260, N8729P, was involved in an accident near Anthony, Kansas. The pilot received serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that the purpose of the flight was to retrieve the airplane following its annual inspection. The flight was conducted at night; as the airplane approached the destination airport, the airplane’s interior lighting dimmed and the pilot used a flashlight to view the instrument panel. He selected the landing gear down and mistook the reflection from the flashlight as a gear down indication. When he was about to touch down, the propeller tips contacted the runway and the pilot applied power to go around. During the go-around, the pilot used the emergency gear extension procedure to lower the landing gear, but the airplane was not able to maintain altitude and he executed a forced landing to a field. During the forced landing, the airplane struck power lines, impacted the field, and slid into large round hay bales that were in the field. The airplane sustained substantial damage to the fuselage and wings. In his report, the pilot noted that during the initial approach he should have used the manual gear extension procedure to ensure that the landing gear was in the down position. Postaccident examination of the airplane determined that the airplane’s alternator was not supplying any charge to the battery. The pilot reported that, during the night flight, the airplane’s interior lighting dimmed and he used a flashlight to view the instrument panel. He selected the landing gear down and mistook the reflection from the flashlight as a gear down indication. When he was about to touch down, the propeller tips contacted the runway and the pilot applied power to go around. During the go-around, the pilot used the emergency gear extension procedure to lower the landing gear; however, the airplane was not able to maintain altitude and he executed a forced landing to a field. During the forced landing, the airplane struck power lines, impacted the field, and slid into large round hay bales that were in the field. The airplane sustained substantial damage to the fuselage and wings. Postaccident examination of the airplane determined that the alternator was not supplying any charge to the battery. The pilot noted that during the initial approach, he should have used the manual gear extension procedure to ensure that the landing gear was in the down position. The reduced performance of the engine/propeller combination after the propeller blades made runway contact likely led to the airplane’s inability to maintain altitude during the go-around. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

• — Aircraft-Aircraft systems-Landing gear system-Gear extension and retract sys-Incorrect use/operation
• — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
• — Personnel issues-Action/decision-Action-Lack of action-Pilot
• — Aircraft-Aircraft systems-Electrical power system-Alternator-generator drive sys-Failure