Summary
On August 28, 2004, a Robinson R44 (N315SG) was involved in an incident near Wildwood, NJ. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's inadequate visual lookout while conducting a nighttime landing to a dolly, which resulted in a stuck skid, and subsequent hard landing. A factor was the nighttime conditions.
On August 27, 2004, at 2150 eastern daylight time, a Robinson R44, N315SG, was substantially damaged landing at the Cape May County Airport (WWD), Wildwood, New Jersey. The certificated commercial pilot was not injured. Night visual meteorological conditions prevailed, and no flight plan was filed for the local flight conducted under 14 CFR Part 91.
According to the pilot, as he was setting the helicopter down onto a dolly, it felt unstable, and he elected to abort the landing. As the pilot raised the collective, the helicopter lurched forward and began to spin to the left.
This incident is documented in NTSB report NYC04CA199. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N315SG.
Accident Details
Probable Cause and Findings
The pilot's inadequate visual lookout while conducting a nighttime landing to a dolly, which resulted in a stuck skid, and subsequent hard landing. A factor was the nighttime conditions.
Aircraft Information
Registered Owner (Current)
Analysis
On August 27, 2004, at 2150 eastern daylight time, a Robinson R44, N315SG, was substantially damaged landing at the Cape May County Airport (WWD), Wildwood, New Jersey. The certificated commercial pilot was not injured. Night visual meteorological conditions prevailed, and no flight plan was filed for the local flight conducted under 14 CFR Part 91.
According to the pilot, as he was setting the helicopter down onto a dolly, it felt unstable, and he elected to abort the landing. As the pilot raised the collective, the helicopter lurched forward and began to spin to the left. The pilot lowered the collective, reduced the throttle, and the helicopter touched down hard onto the ground, spreading the landing skids.
Inspection of the dolly, and the landing skids on the helicopter, revealed that the rear portion of the left skid became stuck under metal framework, which was exposed in an open area near the center section of the dolly.
Inspection of the helicopter revealed that the main rotor blade severed the tail cone and damaged the tail rotor system.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC04CA199