N147BH

Substantial
None

Aerospatiale AS350BAS/N: 1273

Accident Details

Date
Monday, July 7, 2003
NTSB Number
FTW03LA178
Location
Ship Shoal 80
Event ID
20030709X01049
Coordinates
28.916666, -91.300003
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain clearance with the safety fence while landing on an off-shore helipad.

Aircraft Information

Registration
N147BH
Make
AEROSPATIALE
Serial Number
1273
Engine Type
Turbo-shaft
Year Built
1980
Model / ICAO
AS350BAAS50
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
GUARDIAN FLIGHT INC
Address
10888 S 300 W
Status
Deregistered
City
SOUTH JORDAN
State / Zip Code
UT 84095-4043
Country
United States

Analysis

On July 7, 2003, at 1822 central daylight time, an Aerospatiale AS350BA single-engine helicopter, N147BH, was substantially damaged when the tail rotor contacted the safety fence while landing on the helipad for the Ship Shoal 80 offshore oil platform, located in the Gulf of Mexico. The helicopter was registered to CFS Air LLC of Danbury, Connecticut, and was being operated by Texair Helicopters, Inc., of Houston, Texas. The commercial pilot and his passenger were not injured. Visual meteorological conditions prevailed, and a company visual flight rule (VFR) flight plan was filed for the 14 Code of Federal Regulations Part 135 domestic on-demand air taxi flight. The flight originated from the nearby Ship Shoal 79 helipad, at 1809.

The 8,800 hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), that he made a "normal" approach into the wind to the center of the helipad and was terminating his approach at a 4 to 5-foot hover. The pilot added that as he leveled the helicopter to set it down on the deck, he heard a loud "metal crunching" noise coming from the rear of the aircraft. The helicopter began rotating to the left and drifting rearward. The helicopter made about 1.5 revolutions before contacting the deck. After deck contact, the helicopter continued to drift to the left. The pilot stopped the drift, and the helicopter came to rest upright. The pilot further reported that, at the time of the accident, the wind was from 120 degrees at 10 knots.

According to the FAA inspector, who traveled to the accident site, the tail boom was partially separated aft of the horizontal stabilizer, and both tail rotor blades were separated near the hub. An examination of the landing area, revealed damage to the safety fence that was consistent with tail rotor contact.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW03LA178