Loss of Control in Flight · NTSB ANC16FA065
HEFTY Polar Cub — Anchorage, AK
| Date | September 11, 2016 |
| Location | Anchorage, AK |
| Aircraft | HEFTY Polar Cub (amateur-built) |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Uncontrolled descent Collision with terr/obj (non-CFIT) |
| Pilot age | 75 |
| Pilot total time | 2,200 hrs · Experienced |
| Time in type | 1 hrs |
| Fatalities | 1 |
Probable cause
NTSB findings
- Personnel issues-Physical-Impairment/incapacitation-Carbon monoxide-Pilot - C
- Aircraft-Aircraft power plant-Engine exhaust-(general)-Damaged/degraded - C
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Not attained/maintained - C
What happened
The private pilot departed in his float-equipped, experimental, amateur-built airplane during day visual meteorological conditions. According to a friend of the pilot, the purpose of the flight was to fly over a proposed hunting site and then return.
About 90 minutes later, multiple witnesses saw the airplane complete two, low-level, high-speed, 360° right turns over a residential neighborhood. The witnesses said that the airplane's first 360° turn was accomplished at an altitude between 150 and 200 ft above ground level, but the second turn was much lower. Witnesses near the accident site reported that, as the airplane completed the second, steep, 360° turn, the nose of the airplane pitched down, and the airplane began a rapid nose-down descent. The engine rpm then increased significantly, and the wings rolled level just before the airplane impacted a stand of tall trees adjacent to a home. The airplane subsequently descended onto a neighborhood road and came to rest inverted. A postcrash fire ensued about 30 seconds after impact, which quickly engulfed the entire airplane.
According family members and close friends, this was highly unusual behavior for this pilot.
Postaccident examination of the airplane's exhaust system revealed that the muffler can assembly was cracked around most of its circumference near the inlet portion of the muffler, which would have allowed exhaust gases to enter the cockpit/cabin. Toxicology tests revealed 48% carboxyhemoglobin (carbon monoxide) in the pilot's blood. The pilot was a nonsmoker, and nonsmokers normally have no more than 3% carboxyhemoglobin. The pilot's cause of death was extensive blunt force trauma including lacerations of the aorta, heart, and liver, and there was no soot found in his trachea. Although there was a postimpact fire, given the extensive blunt force injuries the pilot sustained and the lack of soot in his trachea, it is likely that the pilot's elevated carboxyhemoglobin level was from acute exposure to carbon monoxide during the 90-minute flight and not from postimpact fire.
Carboxyhemoglobin levels between 10% and 20% can result in confusion, impaired judgment, and difficulty concentrating, and the pilot's 48% carboxyhemoglobin level likely resulted in severe impairment.
No aircraft maintenance records were located for the airplane, which the pilot had built in 1996, so it is unknown when the muffler was last inspected or maintained. Additionally, due to the extensive postimpact fire, it was not possible to determine if the airplane was equipped with any type of carbon monoxide detection equipment. According to friends of the pilot, he conducted all maintenance on the airplane.