N35417Piper J5A · 1941

On August 19, 2023, about 1254 central daylight time, a Piper J5A, N35417, was involved in an accident near Iola, Wisconsin. The airplane sustained substantial damage, and the pilot was fatally injured. The airplane was operated under Title 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot flew the airplane to Central County Airport (68C), Iola, Wisconsin, from Escanaba, Michigan, so that an annual inspection of the airplane could be performed at 68C by a mechanic. The mechanic stated that the pilot had driven twice and flown once before to 68C. The mechanic talked to the pilot about 1-2 days before the accident, when the pilot told him he would like to fly the airplane to 68C during a “weather window.” The mechanic told the pilot to tie down the airplane if he arrived on the weekend since he was going to be away.

There was no record that the pilot received a ferry permit for the flight since the last annual inspection of the airframe and engine had expired; the airplane’s annual inspection was due in September 2022, about 11 months before the accident.

A friend of the pilot drove to 68C to pick up the pilot; when the friend arrived at the airport, he did not see the airplane. The friend looked around the airport and found the airplane nosed over at the end of a taxiway. The friend then drove to a store and called 911.

There were no witnesses to the accident.

No pilot logbook records showing the pilot had a current flight review were found. The pilot’s wife indicated that she did not know how much flight time the pilot had accumulated in the 30 and 90 days before the accident and that he no longer kept a pilot logbook because he believed that he was “beyond that.” She also said that he no longer flew with a flight instructor.

The airplane was nosed over near the northern end of a north/south grass taxiway at the airport. The airplane was near the middle of the taxiway and was oriented (nose to tail) approximately parallel to the taxiway (about 1,500 ft by 100 ft), which had a heading of about 030°.

The taxiway was mowed and had a grass height of about 3 inches, which was the approximate grass height of the airport runways. The airport had a wind direction indicator and a windsock. The windsock was located about 500 ft down, relative to the southern end, and off the west side of the taxiway.

A ground scar that preceded the airplane and was in line with the airplane nose extended about 16 ft from the airplane’s nose. The wing leading edges did not have impact damage. The propeller spinner and the underside cowl aft of the spinner had longitude scoring. The spinner had no rotational scoring/scratches. The propeller blades did not exhibit S-shaped bends/twists consistent with torsion due to engine power.

Examination of the flight controls confirmed continuity from the control surfaces to the cockpit. Engine control continuity from the engine to the cockpit was confirmed. The fuel selector handle was in the left fuel tank position. Fuel selector detents were present when the fuel selector handle was moved through the off, left, and right positions.

There was no fuel smell or evidence of fuel spillage at the accident site. There was no evidence of fuel leakage of the airplane fuel system. Both wing fuel caps were attached and secure. There were no placards relating to fuel type, quantity, and fueling instructions on the airplane. The header tank gascolator, which had a clear bowl, was approximately half full. The left and right wing tank fuel sight gauges were empty while the airplane was in an upside down attitude.

The airplane was moved to an upright position so that it was resting on its main and tailwheel landing gear during recovery of the airplane. When the airplane was upright at the accident site, the left and right wing tank fuel sight gauges remained empty. The left and right wing fuel sump drains, located at the wing roots, were opened and no fuel drained from the sump drains. The right wing was removed from the airframe and visually examined though the wing fuel filler port and no fuel was present. During removal of the left wing, the wing was raised and about 0.25 gallons of fuel was drained from the wing fuel sump drain. The gascolator sump bowl was now full, and the gascolator sump drain was opened to drain fuel from the header tank, which yielded about 0.5 gallons of fuel.

A postaccident engine run was performed by starting the airplane using the airplane’s battery and starter and a fuel container connected to the left fuselage wing root fuel line. The engine started and operated without any anomalies that would have precluded normal operation.

The airplane’s right front brake master cylinder arm had a bungie cord tied around it and connected to the pilot seat frame. Removal of the bungee cord resulted in the cylinder arm partially retracting. With the bungee in place, the airplane was rolled down the taxiway and the brakes were depressed and released, which actuated and released the brakes without anomaly.

The airplane sustained substantial damage due to impact damage of the rudder.

A Lowrance AirMap 2000C was recovered from the airplane. The Lowrance AirMap does not record date or time, so it is unknown when the data points within memory were recorded. The accident flight was the last recorded set of data points. A plot of those data points is shown in the figure below.

Figure - Google Earth overlay of the airplane’s flight path over 68C.

The FAA performed a medical case review of the 78-year-old male pilot’s medical history, which included high blood pressure, a coronary artery bypass graft (CABG) performed in 2005, paroxysmal atrial fibrillation, bilateral knee replacement, decreased vision in his left eye, chronic obstructive pulmonary disease, acid reflux, and arthritis.

The FAA had granted the pilot a Statement of Demonstrated Ability for his left eye condition and had granted several Authorizations for Special Issuance of medical certification for coronary artery disease, CABG, high blood pressure, and acid reflux. In 2009, the FAA had temporarily withdrawn the pilot’s medical certificate because he had been using the narcotic pain medication tramadol to treat arthritis pain. The pilot’s last FAA aviation medical examination was in November 2010. At that time, he was issued a third-class medical certificate by Special Issuance, limited by a requirement to wear corrective lenses; this certificate expired in 2011. He subsequently completed certain requirements for operations under BasicMed, but these requirements were not current as of the accident date. At the time of the accident, the pilot did not possess current FAA medical certification or BasicMed qualifications.

The pilot’s wife reported that the pilot had a stent redone about 8-12 weeks before the accident. She said the pilot wore a heart monitor after that and received a clean bill of health. Photographed among the pilot’s belongings at the crash site was a typed medication list on a sheet of paper. “[Pilot’s name] meds 12/7/2022” was typed at the top of the sheet of paper. Listed medications were rivaroxaban, clopidogrel, furosemide, spironolactone, metoprolol, terazosin, simvastatin, tramadol, venlafaxine, metformin, allopurinol, cetirizine, and fluticasone.

The Waupaca County Medical Examiner’s Office performed the pilot’s autopsy and death investigation. According autopsy report, the pilot’s cause of death was blunt force trauma to his chest and the manner of death was accident. The pilot’s autopsy identified an enlarged heart with dilated chambers. There was severe narrowing of the native coronary arteries by calcified plaque. Three coronary artery bypass grafts were identified and were not blocked. The autopsy report did not document coronary artery stent presence. Visual examination of the heart muscle did not identify other significant natural disease. Microscopic examination of heart muscle showed mild cell enlargement without other significant identified abnormalities. There was severe, calcified, ulcerated plaque in the pilot’s aorta, and mild calcified plaque in the blood vessels of his brain. He was noted to have obesity and fatty liver. His kidney tissue showed changes consistent with chronic high blood pressure.

NMS Labs performed toxicological testing of postmortem femoral blood from the pilot. Tramadol was detected at 420 ng/mL. O-desmethyltramadol was detected at 96 ng/mL. Venlafaxine was detected at 220 ng/mL. O-desmethylvenlafaxine was detected at 460 ng/mL. Delta-9-tetrahydrocannabinol (delta-9-THC) was detected at 2.4 ng/mL. 11-hydroxy-delta-9-THC was detected at 1.3 ng/mL. Carboxy-delta-9-THC was detected at 11 ng/mL. Caffeine was presumptively detected.

The FAA Forensic Sciences Laboratory also performed toxicological testing of postmortem specimens from the pilot. Tramadol was detected at 547 ng/mL in heart blood and at 12,860 ng/mL in urine. O-desmethyltramadol was detected at 144 ng/mL in heart blood and at 2,043 ng/mL in urine. N-desmethyltramadol testing in heart blood was inconclusive; n-desmethyltramadol was detected at 317 ng/mL in urine. Venlafaxine was detected at 418 ng/mL in heart blood and at 3,885 ng/mL in urine. O-desmethylvenlafaxine was detected at 835 ng/mL in heart blood and at 8,388 ng/mL in urine. 11-hydroxy-tetrahydrocannabinol (11-hydroxy-THC) was detected at 1.7 ng/mL in heart blood and at 11.3 ng/mL in urine. Carboxy-delta-9-THC was detected at 27.4 ng/mL in heart blood and at 11.5 ng/mL in urine.

Norchlorcyclizine was detected at 11 ng/mL in heart blood and at 11 ng/mL in urine. Metformin was detected in heart blood and urine. Glucose was not detected (normal result) in urine or vitreous fluid. Rivaroxaban, furosemide, metoprolol, losartan, terazosin, trimethoprim, and tetrahydrozoline were detected in heart blood and urine.