NTSB Factual Report

On March 24, 2016, about 0748 eastern daylight time, an experimental, amateur-built Harmon Rocket II, N729PS, was substantially damaged when it impacted terrain near Cheraw, South Carolina. The airline transport pilot was fatally injured. The airplane was owned and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight, which departed Cheraw Municipal Airport (CQW), Cheraw, South Carolina, about 0710.

Witnesses observed the airplane flying at or near treetop height at several locations in and around the town of Cheraw on the morning of the accident. One witness, who was working alongside the Pee Dee River, stated that, just before the accident, the airplane was flying along the river about treetop level when it struck a power line.

An electronic primary flight display and engine monitor system were recovered from the accident site and forwarded to the NTSB Vehicle Recorder Laboratory for examination. Review of the downloaded GPS data revealed a low-level flightpath consistent with witness statements. During the 7 minutes before the accident, the airplane overflew an airport and the Pee Dee River at altitudes as low as 50 ft above ground level. Review of the engine monitor data did not reveal any preimpact mechanical malfunctions.

According to Federal Aviation Administration (FAA) records, the pilot held an airline transport pilot certificate with ratings for airplane single- and multi-engine land as well as a flight engineer certificate. His most recent FAA first-class medical certificate was issued February 25, 2016, at which time he reported 13,289 total hours of flight experience and 31 hours in the previous 6 months. A witness reported that the pilot had accrued about 35 hours flight experience in the accident airplane make and model.

The tandem, two-seat, low-wing, fixed tailwheel airplane, serial number 414, was assembled from a kit and issued an FAA experimental airworthiness certificate on January 21, 2016, which was when its most recent condition inspection occurred. It was powered by a 250-horsepower Lycoming O-540 engine and equipped with a Hartzell two-blade, fixed-pitch propeller. Review of the airplane's logbook revealed that, at the time of the condition inspection, the airframe had 0 hours of operation and the engine had accrued 590.5 hours since major overhaul. Additional maintenance was performed on March 8, 2016, due to a propeller strike. At the time of that maintenance, the airframe and engine had accumulated 12 hours since the condition inspection.

The 0755 recorded weather at CQW about 3 nautical miles west of the accident site, included wind calm, visibility 5 miles in mist, and a clear sky.

Examination of the accident scene by an FAA inspector revealed that two power line cables were found severed about midspan between two towers, one on each side of the Pee Dee River. The airplane came to rest on a wooded island about 150 yards north of the power line crossing and about 50 yards west of the river bank. Damage to the trees surrounding the wreckage was consistent with a near-vertical descent. The airplane came to rest in a nose-down, inverted attitude.

The upper surface of the engine cowling and canopy were crushed, both wings exhibited leading edge damage consistent with several tree impacts, and the left main landing gear was separated at the fuselage. The empennage was partially separated from the fuselage and bent upward and forward with severe crushing in the aft direction. One section of power line cable was found next to the fuselage, and another was found wrapped around the engine cowling. Flight control continuity was confirmed from the control stick and rudder pedals to the ailerons and rudder, and from the control stick through an overload fracture in the push-pull tube to the elevator. Examination of the wreckage did not reveal any preimpact mechanical malfunctions.

The engine crankshaft was fractured in overload just aft of the flywheel. The flywheel, propeller, spinner, and hub remained attached to one another and were found near the rear of the main wreckage. The propeller exhibited gouge marks in the leading edge consistent with the diameter of the power line, as well as scrape marks on the leading edge and rear of the blade that were consistent with impact with the cable. Both blades exhibited s-bending.

The Chesterfield County Coroner's Office, Chestertown, South Carolina, performed an autopsy on the pilot. The autopsy report noted the cause of death as "multiple blunt force injuries."

The FAA's Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma, performed toxicology testing on specimens of the pilot. Review of the toxicology report revealed cyclobenzaprine, norcyclobenzaprine, and diclofenac in blood and urine, 0.004 µg/ml zolpidem in blood and 0.005 µg/ml in urine.

Cyclobenzaprine (of which norcyclobenzaprine is a metabolite) is a prescription muscle relaxant with potentially impairing mental and physical effects. The laboratory was unable to determine the amount present in the specimen. Diclofenac is a prescription analgesic and is not considered to be impairing. Zolpidem is a potentially impairing prescription sleep aid with a therapeutic range of 0.025 to 0.30 µg/ml.

NTSB Probable Cause

The pilot's decision to fly at low altitude, which resulted in a collision with power lines.