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Atlas / NTSB / ERA20CA112

NTSB CAROL · Event

Event ERA20CA112

2020-02-23 Augusta, Georgia, United States Airport · DNL Minor 1 aircraft Status: Completed

Registry · N60SH

FAA Aircraft Registry record.

Make / Model

BEECH 58P

Year of manufacture

1980 · 40 years old at event

Engine

CONT MOTOR TSIO-520 SER (300 hp)

Seats / Engines

6 seats · 2 engines

Last airworthiness date

19800311

ADS-B equipped

Yes — Mode-S A7C67E

Registrant of record

BAS PART SALES LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to land and stop the airplane within the available runway, which resulted in a runway overrun. Contributing to the outcome was the pilot's inadvertent feathering of both propellers during approach to landing.

Factual narrative

At the conclusion of a positioning flight for maintenance, the pilot of the twin-engine airplane joined the airport traffic pattern at the destination airport. During the landing flare, the pilot began pulling back on what he thought were the throttle levers, but was instead the propeller control levers, which he pulled into the feather position. When the propellers started feathering, he thought that he had lost power on both engines. He landed the airplane "long" on the remaining runway. It subsequently traveled off the end of the runway, through the airport perimeter security fence, crossed a roadway, and came to rest. During the runway overrun, the airplane was substantially damaged. After the accident, the pilot realized that he had been flying the twin-engine accident airplane like he typically flew his high performance single-engine airplane, and believed that was why he retarded the propeller control levers. Review of photographs provided by a Federal Aviation Administration (FAA) inspector showed that unlike the pilot's high performance single-engine airplane, which had its throttle control located on the left side of the control console with the propeller control in the middle, the twin-engine accident airplane had its propeller control levers located on the left side of the control console and the throttle control levers in the middle. According to FAA Airworthiness records, the twin engine accident airplane was manufactured in 1980. Review of the twin-engine airplane manufacturer's technical information indicated that it was not until 1984 that the manufacturer changed the instrument panel layout and relocated the throttle, propeller, and mixture controls to industry-standard positions, similar to those in the pilot's high performance single-engine airplane. 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).

  • C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Aircraft capability-Landing distance-Capability exceeded - C
  • F Aircraft-Aircraft propeller/rotor-Propeller system-Propeller feather/reversing-Unintentional use/operation - F

Verbatim from NTSB's published report. Source file NTSB_2020_ERA20CA112.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 (maintenance). 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 ↗