N555BA

Substantial
None

Bell 412S/N: 36015

Accident Details

Date
Sunday, May 23, 2004
NTSB Number
FTW04LA133
Location
San Antonio, TX
Event ID
20040524X00634
Coordinates
29.432777, -98.492225
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The pilot's failure to maintain clearance with the parked helicopter while performing a hovering turn.

Aircraft Information

Registration
N555BA
Make
BELL
Serial Number
36015
Engine Type
Turbo-shaft
Year Built
1990
Model / ICAO
412B412
Aircraft Type
Rotorcraft
No. of Engines
2

Registered Owner (Historical)

Name
BELL HELICOPTER TEXTRON INC
Address
PO BOX 482
Status
Deregistered
City
FORT WORTH
State / Zip Code
TX 76101-0482
Country
United States

Analysis

On May 23, 2004, approximately 1605 central daylight time, a Bell 412 twin-engine helicopter, N555BA, sustained substantial damage when its tail rotor struck a parked helicopter while hovering prior to takeoff from the University Hospital helipad, near San Antonio, Texas. The commercial pilot, the flight nurse, and flight paramedic were not injured. The helicopter was registered to Bexar County Hospital District, San Antonio, Texas, and operated by Air Methods Corp., Englewood, Colorado. Visual meteorological conditions prevailed, and a company flight plan was filed for the 14 Code of Federal Regulations Part 91 positioning flight. The flight was departing at the time of the accident and was destined for New Braunfels, Texas.

According to a statement from the pilot, prior to takeoff, the helicopter was facing the northwest. While in a hover and executing a right pedal turn to align into the wind, the helicopter's tail rotor struck another helicopter that was parked on the helipad. The airborne helicopter entered into right yaw, and the pilot reduced collective and throttles. Subsequently, the helicopter landed hard onto the helipad.

In addition, the pilot reported having accumulated a total of approximately 4,640 total rotorcraft flight hours, with 877 in the accident aircraft make and model.

Examination of the helicopter revealed the tail rotor drive shaft was separated, the tail rotor blades were damaged, and the landing gear skids were deformed. The parked helicopter sustained damaged to a main rotor blade, and another parked helicopter was damaged by debris. The concrete helipad measured 90 feet in length and 90 feet in width.

At 1553, the San Antonio International Airport automated surface observing system (ASOS), located approximately 6 nautical miles north of the accident site, reported the wind from 170 degrees at 14 knots, 10 statute miles visibility, sky broken at 4,000 feet above ground level, temperature 88 degrees Fahrenheit, dew point 70 degrees Fahrenheit, and an altimeter setting of 29.86 inches of mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW04LA133