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ERA24LA360

2024-08-26 · Jesup, Georgia, United States · None · 1 aircraft · Status: Completed

Airport JES

Current FAA registration · N686AC

Make / Model
BEECH B100
Year of manufacture
1981 · 43 years old at event
Engine
AIRESEARCH TPE331-5&6SER (776 hp)
Seats / Engines
11 seats · 2 engines
Last airworthiness date
19811207
ADS-B equipped
Yes — Mode-S A91984

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A hard landing short of the runway threshold, which resulted in a collapse of the left main landing gear and subsequent runway excursion during landing.

Factual narrative

The pilot reported that he had completed an instrument approach to the runway and immediately after landing, the airplane began to turn left. When asked to characterize the landing, the pilot described that he believed it was not “ideal” but also was not hard, and that the airplane did not bounce after the touchdown. He also stated that he allowed the left main landing gear to touch down first, due to the prevailing crosswind. Following the landing, the pilot attempted to correct the left turn with right rudder and applied the reverse thrust, but the airplane continued to turn, departing the runway to the left and coming to rest in a marshy area. The airplane sustained substantial damage to the left wing. A postaccident examination of the airplane and runway by a Federal Aviation Administration inspector revealed tire marks that began on the runway about 44 feet short of the runway threshold, along with contact marks on the pavement consistent with a left propeller strike. Continuous skid marks consistent with the right main landing gear tire were observed beginning about 50 feet further down the runway, and continuing for more than 400 feet off the left side of the runway. Additional scrape marks on the ground were consistent with the left wing and left main landing gear dragging along the ground. All of the landing gear tires remained fully inflated. The left main landing gear was collapsed and the actuator clevis on the left main landing gear was separated. The left propeller blades also displayed aft bending and abrasion of their tips. Based on these observations, it is likely that the airplane touched down hard short of the runway threshold, which fractured the left main landing gear actuator clevis, resulting the left main landing gear collapsing and the subsequent loss of directional control and runway excursion. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained
  • — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot

Verbatim from NTSB's published report. Source file NTSB_2024_ERA24LA360.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (runway excursion). All research papers