5 fatalities

2017-12-24: Cessna 340 (N247AT) — Aviation Transportation — Bartow, United States of America

Bartow, United States of AmericaTakeoff (climb)

On December 24, 2017, a Cessna 340 (registration N247AT) operated by Aviation Transportation was involved in an aviation accident near Bartow, United States of America during takeoff. 5 people were killed. Investigators recorded the probable cause as: The pilot's loss of control due to spatial disorientation during takeoff in instrument meteorological conditions. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781191596Data APIEditorial standards

A multiengine airplane with a pilot and four passengers crashed shortly after takeoff in dense fog. The pilot, who requested a tow due to low visibility, experienced spatial disorientation and lost control, according to investigators.

Accident Overview

An instrument-rated private pilot and four passengers were aboard a multiengine airplane when it crashed shortly after takeoff. The aircraft had been towed from a hangar to the ramp at the pilot's request, as he wished to avoid obstacles while taxiing in dense fog.

Witness Accounts

Witnesses reported hearing the pre-takeoff engine run-up near the end of the runway, but could not see the airplane due to the fog. The engines sounded normal during the run-up and takeoff. A witness video captured the takeoff roll, but the airplane was obscured by the dense fog. During the roll, the airplane's tires emitted a chirping sound, consistent with a side load during touchdown on the runway. The video ended before the accident. Witnesses stated that the takeoff continued, followed by the sound of impact and an explosion.

Weather and Weight

At the time of the accident, visibility was less than 1/4 mile in fog, with an overcast ceiling at 300 feet above ground level. The airplane's weight exceeded the maximum takeoff weight by about 105 pounds and was outside the center of gravity moment envelope. The excess weight would have likely extended the takeoff roll, decreased the climb rate, and increased the elevator pressure needed to lift off.

Wreckage and Examination

A majority of the airplane was consumed by postcrash fire. Ground impact marks and wreckage distribution indicated that the airplane rolled left over the departure end of the runway and struck the ground inverted in a nearly vertical, nose-low attitude. Examination of both engines showed operating signatures consistent with takeoff power at impact. The elevator trim tab and actuator were found beyond their full up travel limits, and the trim cable exhibited tension overload separations near the actuator. It is likely that when the cable separated, the chain turned the sprocket and extended the actuator rod beyond full travel. No anomalies were observed in the airframe, engines, or cockpit instrumentation that would have precluded normal operation. The investigation was unable to determine the autopilot's status during the takeoff.

Probable Cause

Based on evidence, it is likely that when the airplane entered instrument meteorological conditions, the pilot experienced spatial disorientation, leading to a loss of control and descent into terrain.