Summary
On August 03, 2002, a Robinson R-44 (N44EK) was involved in an incident near Atlantic City, NJ. All 3 people 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 improper flare during approach.
On August 3, 2002, about 1700 eastern daylight time, a Robinson R-44, N44EK, was substantially damaged while landing at the Steel Pier Heliport (92N), Atlantic City, New Jersey. The certificated commercial pilot and two passengers were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the commercial sightseeing flight conducted under 14 CFR Part 91.
The pilot stated that he was completing a 3-minute sightseeing flight. During his final approach to the heliport, the wind shifted, which resulted in a higher than normal sink rate. Additionally, a higher than anticipated ground speed caused the pilot to flare "harder." Subsequently, the tail rotor struck the heliport perimeter fence, and the helicopter began to spin.
This incident is documented in NTSB report NYC02LA157. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N44EK.
Accident Details
Probable Cause and Findings
The pilot's improper flare during approach.
Aircraft Information
Registered Owner (Current)
Analysis
On August 3, 2002, about 1700 eastern daylight time, a Robinson R-44, N44EK, was substantially damaged while landing at the Steel Pier Heliport (92N), Atlantic City, New Jersey. The certificated commercial pilot and two passengers were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the commercial sightseeing flight conducted under 14 CFR Part 91.
The pilot stated that he was completing a 3-minute sightseeing flight. During his final approach to the heliport, the wind shifted, which resulted in a higher than normal sink rate. Additionally, a higher than anticipated ground speed caused the pilot to flare "harder." Subsequently, the tail rotor struck the heliport perimeter fence, and the helicopter began to spin. However, the pilot was able to land the helicopter uneventfully at the heliport. The pilot added that prior to the collision, he did not experience any mechanical malfunctions with the helicopter.
Examination of the wreckage by a Federal Aviation Administration inspector revealed that the tail rotor and gearbox had separated from the helicopter.
The reported winds at an airport approximately 10 miles west of the accident site, at 1654, were from 130 degrees at 8 knots, with no gusts.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC02LA157