N555JCTextron Aviation 208B · 2025

On April 6, 2015, about 1300 central daylight time, a Hughes 369D, N555JC, operated by Haverfield Aviation, Inc., was substantially damaged when it impacted the Tennessee River adjacent to the Natchez Trace Bridge, near Cherokee, Alabama. The commercial pilot was fatally injured. Low ceilings and fog prevailed. A company flight plan was filed for the flight, which originated at Roscoe Turner Airport (CRX), Corinth, Mississippi, about 1230, destined for Scottsboro Municipal Airport-Word Field (4A6), Scottsboro, Alabama. The positioning flight was conducted under the provisions of 14 Code of Federal Regulations Part 91.

According to a witness, a former private pilot, he heard the helicopter land in a National Park Service field contiguous to his property, on the north side of the river, about 3,900 feet from the 1-mile-long, north-south Natchez Trace Parkway Bridge. He couldn't see the bridge at the time due to fog and light mist.

The helicopter remained on the ground for about 45 seconds, still powered with rotors turning; then power increased and it took off smoothly, clearing trees by about 30 feet. The helicopter subsequently headed toward the bridge, and after about 10 to 15 seconds, the witness lost sight of it in the fog. As the helicopter flew, the witness heard no anomalies, and the engine sounded "healthy." He subsequently heard the helicopter hit the water with no change in sound until impact.

According to another witness, he was fishing under the south end of the bridge when the accident occurred. The weather was foggy with low visibility and rain.

The witness heard the helicopter for about 10 to 15 minutes before eventually seeing it crossing the river, then saw it coming toward him, paralleling the west side of the bridge. When he first saw the helicopter through the fog, it was level with the top of the bridge. It began a gradual descent, then about 10 seconds before water impact, dropped to about 25 feet above the water. It subsequently descended at a 10- to 15-degree angle (and from a partial reenactment, described as a "gradual flight in"), and impacted the water near the center of the river, about 50 to 100 feet east of a green buoy (about 100 yards west of the bridge.)

There was no change in sound before the helicopter hit the water, with the same "whining" noise until impact. At impact, the witness saw the helicopter's tail "kick over" the top of the main rotor blades and snap off. The helicopter did not hit the bridge.

The pilot, age 54, held a commercial pilot certificate with helicopter rating. He also held an instrument-helicopter rating. According to a report submitted by the operator, the pilot had accumulated 6,884 hours of flight time, all in rotorcraft, 2,079 hours in make and model, and 52 hours in the previous 30 days. The pilot's latest FAA second class medical certificate was obtained on February 1, 2015.

The mechanic reported to company personnel that he had picked up the pilot at Memphis International Airport, Memphis, Tennessee, the night before and they had dinner together. They also had breakfast the morning of the accident, and that the pilot's "demeanor was great." They spoke about the pilot's health and he said he just completed a flight physical and his cholesterol was low; "he felt great."

The helicopter was powered by a Rolls Royce 250-C20B engine, driving a rotor head with five metal rotor blades. The airframe had accumulated 9,813 hours of operation, and the engine had accumulated 13,181 hours of operation. There were no recording devices onboard the helicopter. Flight instrumentation was limited to an airspeed indicator, an attitude indicator, an altimeter, and a vertical speed indicator.

Weather, recorded at Northwest Alabama Regional Airport (MSL), Muscle Shoals Alabama, about 20 miles to the southeast, at 1318, included calm winds, 1 statute mile visibility, heavy rain, fog, and an overcast cloud layer at 800 feet.

Photographs taken from under the southern end of the bridge, just before the accident, revealed medium gray skies, and in the distance (from the shoreline where the helicopter came), a darker gray band of trees and terrain partially shrouded in fog. The water was a darker gray interspersed with bands of lighter gray.

The helicopter's mechanic noted that the pilot and he had waited at their hotel until bad weather had passed, and once that occurred, pilot then launched to pass behind it.

The helicopter was powered by a Rolls Royce 250-C20B engine, driving a rotor head with five metal rotor blades. The airframe had accumulated 9,813 hours of operation, and the engine had accumulated 13,181 hours of operation. There were no recording devices onboard the helicopter. Flight instrumentation was limited to an airspeed indicator, an attitude indicator, an altimeter, and a vertical speed indicator.

The helicopter was recovered from the river on April 9, 2015. It was missing the aft part of the tail boom, including the tail rotor and gear box, from about 33 inches (fuselage station 230) aft of the tail boom mount, and only remnants of one main rotor blade were subsequently recovered; the other blades remained missing. The left skid was also missing.

Damage began at the helicopter's front, lower left side, and extended upwards. There was no hydraulic crushing (water impact damage) to the bottom of the fuselage.

Control continuity was confirmed from the cockpit to the rotor head, both vertically through the collective, and laterally and longitudinally through the cyclic. Yaw control through the rudder pedals was confirmed from the cockpit to the remnants of the "long tail rotor control rod" in the severed tail boom.

Rotor system drive continuity was confirmed from the engine to the transmission, the transmission to the rotor hub, and from the transmission aft to where the tail rotor drive shaft was severed along with the tail boom.

Three of the five rotor blades were fractured just outboard of the doubler at the main rotor root fitting, and two blades were fractured through the strap assemblies and blade pitch housings, consistent with full power on the rotor system at water impact. Extensive damage was also found on the hub upper shoe in the vicinity of all five pitch change housings, consistent with a medium-to-high collective setting at the time of impact.

The longitudinal and lateral trim actuator assemblies were subsequently removed and the ram positions were measured with both indicating mid-travel positions. The actuator motors were also tested, with one initially being able to run full travel, but subsequently failing to run, and, the other, which had an indent mark on it, not being able to run.

Because the helicopter was not initially located, NTSB did not immediately respond. The helicopter was located on April 7, 2015, and the NTSB Investigator in Charge arrived early on April 8, 2015. Initial witness information was obtained by Haverfield Aviation personnel on April 7, 2015, with follow-up information obtained as needed by NTSB. In addition, FAA Flight Standards District Office inspectors from Birmingham, Alabama, would have normally responded to the accident, but due to office-wide training, inspectors from the Nashville, Tennessee, office responded.

The pilot's body was recovered on April 14, 2015, about 7 miles downriver from the accident site. The next day, an autopsy was performed at the Alabama Department of Forensic Sciences, Huntsville, Alabama, where cause of death was determined to be "blunt force injuries and drowning," and manner of death was determined to be "accident."

Toxicological testing was subsequently performed at the FAA's Civil Aerospace Medical Institute, Oklahoma City, Oklahoma, where pseudoephedrine was found in a liver sample and urine, and ephedrine was found in urine.

According to the National Institute of Health website, pseudoephedrine is an over-the-counter decongestant, and ephedrine is its metabolic byproduct.

Ethanol, butanol and propanol were also found in various samples, consistent with postmortem production from the body's extended time in the water.