Probable cause
The pilot's failure to maintain control of the helicopter during a hover.
NTSB analysis
According to the pilot, the purpose of the company test flight was to measure collective stick forces with the collective bias disabled. The pilot, who was the helicopter's only occupant, lifted the helicopter into a hover and then hovered clear of any obstacles. He reported that the collective controls were heavy, as expected, but the helicopter was very controllable. During his attempt to position a force gauge between his hand and the collective grip, the pilot lost control of the helicopter and it landed hard onto the ramp. The helicopter's tail rotor blades impacted the ramp and the helicopter came to rest upright. A postaccident examination of the helicopter showed that the tail rotor blades were bent and the tail rotor driveshaft was sheared. The pilot reported that he should have taken an observer or other personnel on the flight to assist while he concentrated on flying the helicopter.
Text from the NTSB. Open the NTSB docket for CEN11CA638 for the full record.
Event
- Date
- Aug 29, 2011
- Type
- Accident
- Place
- Menominee, Michigan
- Nearest airport
- Menominee-Marinette Twin City (MNM)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Enstrom F-28F
- N-number
- N228F
- Category
- Helicopter
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Flight test
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.