PIPER PA 28-180

Full Narrative

HISTORY OF FLIGHT

On October 13, 2015, about 1733 eastern daylight time, a Piper PA-28-180, N57312, impacted a residential area in Lake Worth, Florida, during approach to Palm Beach County Park-Lantana Airport (LNA), Lantana, Florida. The private pilot and one person on the ground were fatally injured. The airplane was consumed by postimpact fire and destroyed. The airplane was owned by Flyers Inc., and was being operated by a private individual as a 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed, and no flight plan was filed. The flight had departed Kissimmee Gateway Airport (ISM), Kissimmee, Florida, with an intended destination of LNA.

Fueling records indicated that the airplane was then topped off with 20 gallons of 100-low-lead aviation gasoline before departing ISM for a flight to LNA, during which the pilot received flight-following services from air traffic control. Review of recordings of the airport's common traffic advisory frequency revealed that the pilot was 3 miles east of the airport and was going to enter the midfield left downwind leg for runway 15. The pilot then radioed that he was turning a left base leg for runway 15. No other communications were received from the pilot. Radar data provided by the Federal Aviation Administration showed a target correlated to be the accident airplane flying past the runway extended centerline and then making an S-turn before radar coverage was lost.

PERSONAL INFORMATION

According to FAA records, the pilot held a private pilot certificate with an airplane single-engine land rating, which was issued on May 4, 2012. He also held an FAA third-class medical certificate, issued September 23, 2015. At that time, he was 66 inches tall and weighed 180 pounds. He reported treatment for a kidney stone, a laceration repair, and hernia surgery as well as various minor ailments to the FAA. He reported the use of testosterone to treat a low testosterone level. His medical certificate was limited by a requirement to wear corrective lenses for distant vision and have glasses available for near vision.

At the time of the medical examination, the pilot reported 250 hours of total flight time.

AIRCRAFT INFORMATION

The four-seat, low-wing, fixed-tricycle-gear airplane, serial number 28-7405042, was manufactured in 1973. It was powered by a Lycoming O-360, 180-horsepower engine and equipped with a two-bladed, fixed-pitch Sensenich propeller.

A review of maintenance records revealed that the airplane's most recent annual inspection was completed on May 25, 2015. At that time, the airframe had accumulated 6,199 total flight hours and the engine had accumulated 1,320 flight hours since major overhaul.

METEOROLOGICAL INFORMATION

The 1753 recorded weather observation at West Palm Beach International Airport (PBI), West Palm Beach, Florida, located about 4.5 miles north of the accident site, included wind from 140° at 13 knots, visibility 10 miles, few clouds at 5,000 ft, scattered clouds at 25,000 ft, temperature 28° C, dew point 21° C, and altimeter 29.91 inches of Mercury.

WRECKAGE AND IMPACT INFORMATION

The wreckage was examined at the accident site and again at a recovery facility. No readable cockpit instruments were recovered. Aileron control continuity was established from the control chain in the cockpit via aileron cables to their respective aileron bellcranks. The aileron cables had separated and exhibited broomstraw ends, and the bellcranks had separated from the wings. Rudder control continuity was confirmed from the rudder horn to the rudder bar. Stabilator control continuity was confirmed from the "T" bar to the balance weight. The stabilator trim system was not recovered and presumed destroyed by postimpact fire.

The two-bladed propeller remained attached to the engine. One blade was bent aft, was partially melted, and contained leading edge nicks, and the outboard half of the other propeller blade was consumed by fire.

The top spark plugs were removed from the engine, and the propeller was rotated by hand. Camshaft and crankshaft continuity to the rear accessory section was confirmed, and valve train continuity was confirmed to the Nos. 1 and 3 cylinders through rotation of the crankshaft. Due to impact and thermal damage, valve train continuity to the Nos. 2 and 4 cylinders was confirmed by visual inspection.

MEDICAL AND PATHOLOGICAL INFORMATION

The Office of the Medical Examiner, West Palm Beach, Florida, performed an autopsy on the pilot. The autopsy findings included multiple blunt force trauma and thermal injuries. The autopsy also identified heart enlargement and wall thickening and diffuse coronary artery disease with 75 percent stenosis in the left anterior descending and right coronary arteries and 25 percent stenosis of the left main and left circumflex coronary arteries. In addition, there was mild calcification of the mitral valve leaflets.

The FAA Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma, performed toxicology testing on specimens from the pilot. The toxicology tests detected greater than 10% carbon monoxide in blood (heart) and greater than 2.51 (ug/ml) cyanide in blood (heart).