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NYC04CA199

2004-08-27 · Wildwood, New Jersey, United States · None · 1 aircraft · Status: Completed

Airport WWD

Current FAA registration · N315SG

Make / Model
ROBINSON HELICOPTER R44
Year of manufacture
2003 · 1 years old at event
Engine
LYCOMING 0-540 SERIES (250 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20030515
ADS-B equipped
Yes — Mode-S A35AFB

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & 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.

Factual narrative

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. As the helicopter was being set down onto a dolly during the hours of darkness, it felt unstable, and the pilot 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. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2004_NYC04CA199.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.