Landing / Ground Loss of Control · NTSB WPR21FA353
BEECH S35 — Billings, MT
| Date | September 27, 2021 |
| Location | Billings, MT |
| Aircraft | BEECH S35 |
| Purpose of flight | Personal |
| Conditions | Dusk · Visual Meteorological Cond |
| Phase / occurrence | Landing-flare/touchdown Abnormal runway contact |
| Pilot age | 25 |
| Pilot total time | 373 hrs · Building experience |
| Time in type | Unknown |
| Fatalities | 2, 1 serious |
Probable cause
NTSB findings
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Not attained/maintained
- Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
What happened
The pilot reported that he was conducting a cross-country flight with an intended destination that did not have runway lighting. As the airplane neared the intended destination, the pilot voiced his concern to one passenger (who was pilot rated) about the dusk conditions with no runway lights and the passenger reassured him about the landing. The pilot stated that, as the airplane was landing, the pilot-rated passenger knew something was wrong and told the pilot to “add power.” The airplane subsequently made a left turn and impacted trees in a nose-high attitude; a postimpact fire ensued.
Witnesses located near the accident site reported observing the airplane on final approach. One witness stated that the airplane appeared to be “slightly high and slightly fast” while on final approach to the runway and that the airplane had “floated down the runway” before a hard touchdown. Another witness stated that the left wing appeared to have stalled, and that the airplane landed hard on the left main landing gear first. One of the witnesses further stated that the airplane began to “wobble” and depart the left side of the runway, which followed by an increase in engine power and a go-around attempt. The witness added that engine power continued as the left wingtip was dragged across the ground about halfway through the go-around attempt.
Postaccident examination of the airframe and engine revealed no evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation.
Based on the runway and ground marks, and witnesses’ observations of the landing, the pilot continued an unstabilized landing approach, and delayed execution of a go-around, which resulted in a hard landing and subsequent loss of airplane control.