Summary
On August 09, 2006, a Bell 206B (N121RH) was involved in an incident near Orlando, FL. All 5 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 failure to refuel the helicopter prior to the accident flight, which resulted in a loss of engine power during cruise flight, and a hard landing.
The airline transport certificated pilot, with four passengers, departed on a Title 14, CFR Part 91, local area revenue sightseeing flight in a skid-equipped helicopter. According to the operator's chief pilot, the accident pilot reported that while in cruise flight, the fuel pump warning light illuminated, and he began a precautionary landing approach to a vacant parking lot. While on final approach to the parking lot, the pilot said the "engine flamed out." The pilot initiated an autorotation, but the helicopter landed hard. The helicopter's landing gear cross-tubes were deformed, the pilot's windscreen was broken, and the fuselage received structural damage. An FAA inspector reported that an examination of the helicopter revealed that it had flown 1.5 hours before the accident.
This incident is documented in NTSB report ANC06CA122. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N121RH.
Accident Details
Probable Cause and Findings
The pilot's failure to refuel the helicopter prior to the accident flight, which resulted in a loss of engine power during cruise flight, and a hard landing.
Aircraft Information
Registered Owner (Historical)
Analysis
The airline transport certificated pilot, with four passengers, departed on a Title 14, CFR Part 91, local area revenue sightseeing flight in a skid-equipped helicopter. According to the operator's chief pilot, the accident pilot reported that while in cruise flight, the fuel pump warning light illuminated, and he began a precautionary landing approach to a vacant parking lot. While on final approach to the parking lot, the pilot said the "engine flamed out." The pilot initiated an autorotation, but the helicopter landed hard. The helicopter's landing gear cross-tubes were deformed, the pilot's windscreen was broken, and the fuselage received structural damage. An FAA inspector reported that an examination of the helicopter revealed that it had flown 1.5 hours before the accident. The helicopter's fuel gauge, annunciator system, fuel pump, and fuel system, functioned normally. A pressure check of the fuel lines revealed no leakage. The inspector indicated that the fuel tank contained about 40 ounces of fuel. The inspector reported that during his examination of the helicopter, no mechanical malfunction was found.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC06CA122