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Atlas / NTSB / CEN24LA247

NTSB CAROL · Event

Event CEN24LA247

2024-06-29 Midland, Texas, United States Airport · MAF None 1 aircraft Status: Completed

Registry · N451M

FAA Aircraft Registry record.

Make / Model

LANCAIR LANCAIR IV P

Year of manufacture

2005 · 19 years old at event

Engine

CONT MOTOR TSIO-550 SER (280 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20050309

ADS-B equipped

Yes — Mode-S A576E6

Registrant of record

TIMOTHY DUANE HIGH

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s failure to extend and verify landing gear extension which resulted in a wheels-up landing. Contributing was the increased workload due to several airplane issues that occurred during the descent in severe turbulence.

Factual narrative

The pilot reported that he was hired to fly the airplane to another airport following a pre-purchase inspection. The preceding pilot informed the pilot of several issues with the airplane including the propeller control and the cabin door. The pilot said he familiarized himself with the airplane and after about three hours of inspections and ground tests determined the airplane was in a safe condition and proceeded with the flight. He reported that during the descent to the destination airport, the turbulence became severe, noting that his head hit the cabin roof twice even though the lap seat belt was secured. The cockpit was loud and as he advanced the throttle after lowering the flaps 10 degrees, the cabin noise increased, and the propeller indications became erratic. Several engine instruments were giving erratic readings as well and the pilot was additionally concerned about the cabin door latches becoming loose in the turbulence. The airplane was operating properly and after a minute the propeller indications stabilized. All these events added to his workload. The pilot said that while approaching to land and after lowering the flaps, he reached for the landing gear handle, noting that these checks were performed in severe turbulence. He visually confirmed that the flaps were fully extended by looking out the side window and believed that he looked at the gear indicator lights but didn’t clearly remember this. He also did not remember shading the landing gear position indicator with his hand as he had done previously. During the landing, the airplane settled onto its belly and the airplane slid to a stop. He noted that after the accident, the landing gear handle and flap handle were both in the mid-position. The airplane sustained substantial damage to the fuselage. When the airplane was being recovered from the runway, aircraft power was turned on and the landing gear selector placed in the fully down position. The landing gear extended and locked into the fully extended position with no anomalies noted. 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 systems-Landing gear system-Landing gear selector-Not used/operated
  • Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
  • Environmental issues-Conditions/weather/phenomena-Turbulence-Clear air turbulence-Effect on operation
  • Personnel issues-Psychological-Attention/monitoring-Monitoring equip/instruments-Pilot

Verbatim from NTSB's published report. Source file NTSB_2024_CEN24LA247.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 (turbulence). 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 ↗