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Atlas / NTSB / ERA24LA360

NTSB CAROL · Event

Event ERA24LA360

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

Registry · N686AC

FAA Aircraft Registry record.

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

Registrant of record

STM AIR LLC

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

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or 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

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (runway excursion). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗