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Atlas / NTSB / MIA00LA089

NTSB CAROL · Event

Event MIA00LA089

2000-02-10 SALISBURY, North Carolina, United States Airport · RUQ None 1 aircraft Status: Completed

Registry · N2007K

FAA Aircraft Registry record.

Make / Model

BEECH 76

Year of manufacture

1978 · 22 years old at event

Engine

LYCOMING O&VO-360 SER (180 hp)

Seats / Engines

4 seats · 2 engines

Last airworthiness date

19780817

ADS-B equipped

Yes — Mode-S A1955A

Registrant of record

EXECUTIVE FLIGHT INSTITUTE LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The flight instructors inadequate supervision of a dual student who attempted a go around using one engine which resulted in loss of control and impact with the ground.

Factual narrative

On February 10, 2000, about 1845 eastern standard time, a Beech 76, N2007K, registered to Flights Unlimited, Inc., crashed during an aborted landing at Rowan County Airport, Salisbury, North Carolina, while on a Title 14 CFR Part 91 instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the airline transport-rated flight instructor and private-rated dual student were not injured. The flight last departed Salisbury, North Carolina, the same day, about 1840. The flight instructor and dual student stated that the flight departed from Rowan County Airport about 1745. After performing airwork, including flight at minimum control speed (Vmc), they returned to Rowan County Airport for a touch-and-go landing. They entered the pattern after the touch-and-go landing, and planned to make a full stop landing. During this approach the flight instructor simulated the failure of the right engine. During final approach the flight instructor told the dual student he could use both engines for landing. As they approached the flare for landing the student drifted to the left and the instructor told him to go around. During the go around, the dual student used only the left engine. The aircraft rolled to the right after power application, and the flight instructor took control. The flight instructor applied full left rudder and aileron, but could not regain control prior to hitting the ground in the grass to the side of the runway. Examination of the aircraft after the accident was performed by an FAA inspector. The inspector stated the main and nose landing gear had received damage. The surface skin of both wings was wrinkled enough to indicate further internal damage to wing ribs and possibly the spars. At the left wing root the wing was pulled outward away from the fuselage in a way that suggest that there may be additional damage at the wing attachment points. (See FAA Inspector Statement.) While performing a visual approach with a simulated failure of the right engine, the flight instructor told the dual student to use both engines for landing. Just prior to the landing flare, the dual student allowed the aircraft to drift and the flight instructor commanded that he perform a go around. The dual student used only the left engine for the go around and as power was applied, the aircraft rolled to the right. The flight instructor took control and applied full left rudder and aileron, but did not regain control prior to the aircraft impacting the ground in the grass adjacent to the runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2000_MIA00LA089.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 (loss of control). 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 ↗