No fatalities

Robinson R44 Accident During Aerial Application Near Capron, Illinois (N9681R)

Capron, IL, United States

On July 28, 2013, a ROBINSON R44 (registration N9681R) operated by Back Nine Aerial LLC was involved in an aviation accident near Capron, IL. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to maintain main rotor speed while maneuvering at low altitude during an agricultural application flight, which resulted in an uncontrolled descent into terrain. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

On July 28, 2013, a Robinson R44 helicopter, registered N9681R, descended during a turn and impacted terrain while conducting aerial application near Capron, Illinois. The pilot was seriously injured, and the helicopter sustained substantial damage.

Accident Details

On July 28, 2013, about 1544 central daylight time, a Robinson R44 helicopter, registration N9681R, descended during a turn and impacted terrain during an aerial application flight near Capron, Illinois. The helicopter sustained substantial damage, and the commercial pilot sustained serious injuries. The helicopter was registered to and operated by Back Nine Aerial LLC under 14 Code of Federal Regulations Part 137 as an aerial application flight that was not operating on a flight plan. Visual meteorological conditions prevailed for the flight, which originated from East Troy Municipal Airport (57C), East Troy, Wisconsin.

Pilot Narrative

According to the pilot, he departed from 57C at 0640 to perform a series of aerial applications of fungicide on fields near Harvard, Illinois. About 1445, while flying downwind about 150 feet above a field, the helicopter began to descend. The pilot then turned the helicopter into the wind and increased pitch to arrest the descent, which resulted in a low main rotor RPM. There was not sufficient altitude to recover the main rotor RPM, and the helicopter settled into a wooded area, contacting trees. The helicopter came to rest in an upright position.

Post-Accident Examination

A Federal Aviation Administration inspector reported that a 3-4 inch tree limb was broken and exhibited features consistent with being cut by the main rotor blade. Usable fuel was present aboard the helicopter, and there were no mechanical anomalies with the helicopter that would have precluded normal operation.

Investigation Status

The accident investigation did not assign a probable cause in the source material.

Contributing factors

PilotProp/rotor parameters — Not attained/maintained