Summary
On February 01, 2005, a Bell 206B (N59MB) was involved in an incident near Lancaster, PA. 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 loss of lateral control while attempting to transition to a hover from the ground. A factor was the bright sunlight conditions.
On February 1, 2005, at 1426 eastern standard time, a Bell 206B, N59MB, was substantially damaged while attempting to transition to a hover from the ground at the Lancaster Airport, Lancaster, Pennsylvania. The certificated private pilot was not injured. 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 raising the collective to hover the helicopter, it immediately rolled over onto its right side.
This incident is documented in NTSB report NYC05CA047. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N59MB.
Accident Details
Probable Cause and Findings
The pilot's loss of lateral control while attempting to transition to a hover from the ground. A factor was the bright sunlight conditions.
Aircraft Information
Registered Owner (Historical)
Analysis
On February 1, 2005, at 1426 eastern standard time, a Bell 206B, N59MB, was substantially damaged while attempting to transition to a hover from the ground at the Lancaster Airport, Lancaster, Pennsylvania. The certificated private pilot was not injured. 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 raising the collective to hover the helicopter, it immediately rolled over onto its right side. The pilot added that the helicopter was positioned into the direct sunlight, and he experienced "dazzling sunlight" being reflected from surrounding snow banks.
The pilot did not report any mechanical difficulties with the helicopter.
Inspection of the helicopter revealed that the main rotor blades and the tail rotor assembly sustained substantial damage.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC05CA047