Casualties unknown

Homebuilt Helicopter Crashes After Low Pass and Maneuvering Near Trail Maintenance (N228CH)

Milan, NH, US

On October 30, 1999, a Godbout EXEC 162F (registration N228CH) was involved in an aviation accident near Milan, NH. Investigators recorded the probable cause as: The pilot's failure to maintain proper rotor rpm while maneuvering, which resulted in main rotor blade flapping, and its subsequent impact with the tail boom. A factor was the pilot's lack of experience in maneuvering flight. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A homebuilt helicopter, after transiting to an area 8 miles from departure, was observed making a low pass along a trail. It maneuvered at about 50 feet over 50-foot trees, entered a steep turn, emitted a loud bang, and descended vertically into woods. The tail boom separated and was found 150 feet away with paint transfer marks matching a main rotor blade.

Accident Overview

The accident involved a homebuilt helicopter that had departed from an unspecified location and transited to an area approximately 8 miles from its departure point. A witness observed the helicopter making a low pass along a 5-mile trail. It then flew to a point about midway along the trail, where trail maintenance was taking place, and began maneuvering at an altitude of about 50 feet above 50-foot trees.

Maneuvering and Impact

The helicopter entered a steep turn, at which point a loud 'bang' was heard. The helicopter then descended almost vertically into the woods. The main wreckage was found upside down, and the tail boom was located about 150 feet away from the main wreckage. Paint transfer marks were found where the tail boom had separated, which matched the paint on the end of a main rotor blade. The blade exhibited downward bending near its inboard end and upward bending near its outboard end. The blade's leading edge had impact marks and paint transfer marks consistent with contact with the tail boom.

Engine and Systems

Fuel was found onboard the helicopter. The engine exhibited scoring marks consistent with a sudden stoppage. There was no evidence of in-flight blade failure or separation. An onboard recording of throttle positions revealed that the throttle had been opened to 29 to 32 percent for the first 4 of the last 5 minutes of flight, consistent with the helicopter transiting the area. From 56 seconds until 6 seconds prior to the last recording, the throttle position was approximately 38 to 40 percent, consistent with the use of added power for maneuvering over the trees. Three seconds before the last recording, the throttle had been closed to 7 percent, before it was returned to 38 percent for the last two seconds of the recording.

Pilot Information

The student pilot had accumulated 64 hours of flight time. He had attended the kit manufacturer's facility three times for training. He had been endorsed for hovering flight, flight through translational lift, and quickstops, provided he remained within 35 feet of the ground at all times. He had previously been involved in an accident while hovering the helicopter. Another builder/pilot, who had flown with the student pilot, stated that his 'ability to maintain proper rotor rpm was a problem.'

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20042. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.