N40506

HISTORY OF FLIGHTOn May 14, 2023, at an unknown time, a Robinson R22 Beta helicopter, N40506, was substantially damaged during a crash near Brady, Texas. The non-certificated pilot was fatally injured. Although the helicopter was operated under Title 14 Code of Federal Regulations (CFR) Part 91, evidence from the investigation suggests there was no intent for flight as defined by 49 CFR § 830.2 and, accordingly, the event was not classified as an accident.

There were no witnesses to the crash. According to one of the pilot’s daughters, the pilot regularly attended a Sunday morning church service at 1100 in Brady, Texas, but on the morning of the crash he was not seen at the church service. After several unsuccessful attempts to reach the pilot via phone on the afternoon of May 14 and the morning of May 15, a family member asked a neighbor to check on the pilot at his residence, where the helicopter wreckage and pilot were found near the house. The pilot was reportedly wearing his church clothes and dress boots. PERSONNEL INFORMATIONA search of FAA airman certification records found no record of a pilot certificate ever being issued to the pilot.

The pilot’s family provided a pilot logbook that contained a combined FAA third-class medical and student pilot certificate dated February 3, 1970. The medical/student pilot certificate was expired. The final logbook entry was a 90-day solo endorsement for a Cessna 172 airplane dated January 17, 1971. Further review of the pilot logbook did not reveal any flights completed in a helicopter. According to the pilot’s family, he had served in the US Army but in a non-pilot role. The pilot’s baseline ability to fly helicopters could not be assessed with the available documentation. AIRCRAFT INFORMATIONThe last annual inspection of the helicopter was completed on October 10, 2003, at 3,449.7 total airframe hours. The logbook documentation did not reveal any maintenance actions after the annual inspection. At the time of the crash, the airframe total time was 3,527.0 hours, and the engine total time since new and time since overhaul were 4,035.7 hours and 1,527.3 hours, respectively. AIRPORT INFORMATIONThe last annual inspection of the helicopter was completed on October 10, 2003, at 3,449.7 total airframe hours. The logbook documentation did not reveal any maintenance actions after the annual inspection. At the time of the crash, the airframe total time was 3,527.0 hours, and the engine total time since new and time since overhaul were 4,035.7 hours and 1,527.3 hours, respectively. WRECKAGE AND IMPACT INFORMATIONThe helicopter was found on its right side, facing west, about 15 ft from the north wall of the house, as shown in figure 1. The helicopter was about 70 ft southwest from a concrete pad that the pilot used during ground operations, as shown in figure 2. The helicopter’s ground handling wheels and a hand truck associated with a battery charger were found beside the concrete pad, as shown in figure 3. The battery charger and its integrated jumper cables were found about 60 ft from the concrete pad against the rear right tire of a white sedan parked beside the helicopter wreckage, as shown in figure 4. The hood and roof of the white sedan exhibited fresh dirt deposits.

There was a small truck, full-sized recreational vehicle, and two steel drums located between the concrete pad and the helicopter wreckage, as shown in figure 5. Based on ground impact marks and the overall wreckage distribution, the helicopter ascended at least 7 ft to clear the obstacles before it impacted the ground near the house.

The pilot-side cabin door, normally installed on the right side of the helicopter, separated from the fuselage during impact and was found about 20 ft from the main wreckage. The right door hinges did not have retaining rings installed. The passenger side cabin door remained closed, latched, and undamaged on the helicopter. According to first responders, the pilot was found in the right side of the cabin with his torso still seated in the right seat, and he was not wearing the available seat restraints.

Figure 1. Main wreckage overview

Figure 2. Location of main wreckage in north side yard of house (red arrows) and concrete pad (yellow arrows) with inset aerial photo depicting property layout.

Figure 3. Concrete pad, hand truck used with battery charger (red boxes), and ground handling wheels (red arrows).

Figure 4. Main wreckage, sedan, and battery charger with jumper cables (red arrow).

Figure 5. Main wreckage with obstacles along projected flight path.

Flight control continuity was confirmed from the cyclic and collective to the swashplate assembly where both ears exhibited fracture features consistent with overstress. Both blade pitch control links remained intact. The cyclic friction was on and, as shown in figure 6, the collective friction control was off. Tail rotor flight control continuity was confirmed from the anti-torque pedals to the tail rotor blades.

Figure 6. Collective friction in off position.

Both main rotor blades were bowed upward with chordwise creases throughout their span. Both blades had rough score marks along their leading edge from mid-span out to their respective tip. The tail rotor blades exhibited normal wear along the leading edge with no impact damage.

The main transmission and tail rotor gear box rotated freely by hand. The tail rotor drive shaft remained intact. The lower and upper sheaves appeared undamaged, and the V-belts exhibited no abnormal wear. The V-belts were in place on the lower sheave and positioned one groove forward on the upper sheave. The upper and lower support bearings rotated smoothly. The upper sheave engaged the clutch shaft when rotated by hand in a counterclockwise direction (looking forward) and rotated smoothly on the shaft when rotated in a clockwise direction.

The helicopter’s main fuel tank contained about 4 gallons of fuel, and the auxiliary fuel tank contained unusable fuel. The gascolator bowl was full of fuel that was blue in color with no water or debris and had the odor of 100 low-lead aviation fuel. The gascolator fuel screen was clear of debris. The airframe fuel lines were undamaged and remained attached to the carburetor inlet. The fuel shutoff valve was found open.

There was a short chain loop installed on the landing skid aft cross tube, as shown in figure 7. According to the pilot’s family, to move the helicopter while on the ground, the pilot would connect an electric winch cable to a short chain loop on the helicopter’s landing skid aft cross tube. The electric winch motor was located at the rear of the shed where the helicopter was normally stored. However, if he intended to fly, the pilot would remove the short chain loop before the flight. The winch cable was not connected to the chain loop at the time of the crash and was found on the floor of the shed undamaged.

Figure 7. Chain loop around the landing gear skid aft cross tube.

The engine started and operated normally during several postcrash engine runs. The wreckage examination and engine test runs did not reveal any preimpact mechanical anomalies that would have prevented normal operation of the helicopter. ADDITIONAL INFORMATIONAccording to one of the pilot’s daughters, the pilot purchased the helicopter in March 2016 as an investment and she could not recall the last time he flew the helicopter. She stated that the pilot would occasionally bring the helicopter out of the shed to perform an engine run and, on multiple occasions, he forgot to engage the collective friction control, which resulted in unintended movement of the helicopter on the ground while the engine was running. The pilot kept the helicopter’s battery connected to a charger while the helicopter was stored in the shed and during the engine runs on the concrete pad. MEDICAL AND PATHOLOGICAL INFORMATIONThe 93-year-old pilot had an extensive past medical history, including a stroke in 2019 with residual left upper extremity weakness, Parkinson’s disease resulting in a tremor of his right hand, coronary artery disease, a recent electrocardiogram with arrhythmias, high blood pressure, high cholesterol, degenerative arthritis of the spine, chronic kidney disease, and recurrent urinary tract infections resulting in hospital admissions.

On January 19, 2023, during his most recent hospital admission, the pilot was diagnosed with moderate senile dementia. His medication list at that time included carbidopa/levodopa, a prescription medication commonly used to treat Parkinson’s disease; atorvastatin, a prescription medication commonly used to control cholesterol and reduce cardiovascular risk; gabapentin, a prescription medication commonly used to treat nerve pain; aspirin, an over-the-counter medication commonly used to treat pain and fever and to reduce cardiovascular risk; finasteride, a prescription medication commonly used to treat an enlarged prostate; and levothyroxine, a prescription medication commonly used to treat low thyroid hormone.

The autopsy of the pilot was performed by Central Texas Autopsy, Lockhart, Texas, as authorized by a McCulloch County Judge. According to the autopsy report, the pilot’s cause of death was blunt force head and chest trauma, and the manner of death was accident. The heart was described as enlarged with severe calcific coronary artery disease, including 50-90% stenosis of the right coronary artery, 40% stenosis of the left main coronary artery, 50-80% stenosis of the left anterior descending coronary artery and 50-100% stenosis of the circumflex coronary artery. A prior myocardial infarction (heart attack) was noted. The heart was also found to have moderate to severe left ventricular hypertrophy, and severe biventricular dilatation. The aorta was noted to have severe calcific atherosclerotic disease. The kidneys were noted to have changes from severe atherosclerosis. The remainder of the autopsy including exami...