Probable cause
The pilot's loss of directional control while attempting to move the helicopter laterally without first lifting it fully off its landing platform.
NTSB analysis
The pilot had just landed the helicopter on a flatbed trailer when it was determined that it needed to be moved laterally in order for its skids to be correctly attached to the trailer. Therefore the pilot applied enough collective to make the helicopter "light on the skids," and then he applied cyclic input meant to slide the helicopter laterally. When the helicopter did not slide sideways as the pilot desired, he continued to apply left cyclic input, whereupon the helicopter suddenly began to move in a manner that resulted in it starting to fall off the trailer. During the pilot's attempt to regain directional control by lifting the helicopter clear of the trailer, its main rotor blades came in contact with the truck that the trailer was attached to. Once the blades contacted the truck, the helicopter rotated about 180 degrees and impacted the tarmac beside the trailer. Soon after it impacted the tarmac, a fast-growing fire began. During the accident sequence, an individual who was helping with the loading process was struck by a main rotor blade.
Text from the NTSB. Open the NTSB docket for WPR10LA354 for the full record.
Event
- Date
- Jul 16, 2010
- Type
- Accident
- Place
- Salt Lake City, Utah
- Nearest airport
- Salt Lake City Int. (KSLC)
- Highest injury
- Fatal
- Serious injuries
- 2
- Weather
- Visual (VMC)
- Light
- Day
Robinson Helicopter Company R44 II
- N-number
- N944DW
- Category
- Helicopter
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Positioning
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.