N330P

Substantial
None

Bell 206LS/N: 51295

Accident Details

Date
Wednesday, August 17, 2005
NTSB Number
DFW05CA213
Location
Gulf of Mexico
Event ID
20051020X01701
Coordinates
27.633333, -96.216667
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain clearance with a stationary object while landing.

Aircraft Information

Registration
N330P
Make
BELL
Serial Number
51295
Engine Type
Turbo-shaft
Year Built
1989
Model / ICAO
206LB06T
Aircraft Type
Rotorcraft
No. of Engines
2

Registered Owner (Historical)

Name
AIR LOGISTICS LLC
Address
4605 INDUSTRIAL DR
Status
Deregistered
City
NEW IBERIA
State / Zip Code
LA 70560-9124
Country
United States

Analysis

On August 17, 2005, at 1008 central daylight time, a Bell 206L single-engine helicopter, N330P, was substantially damaged when the tail rotor contacted the safety fence while landing on the helipad at the Mustang Island 111 offshore oil platform, located in the Gulf of Mexico. The helicopter was registered to and operated by Air Logistics, LLC of New Iberia, Louisiana. The commercial pilot, sole occupant, was 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 91 positioning flight. The flight originated from a nearby oil platform, at approximately 1005.

The 2,258-hour pilot reported that he made his approach to the platform, so he would be landing to the east; there was little or no wind. After crossing the helipad skirting, he flared to "zero out my groundspeed". The pilot added that afterhe leveled out the helicopter, "I heard a clunk and saw debris flying around me". He reported there were no vibrations nor any abnormal indications, prior to the landing. After the pilot performed an emergency engine shutdown, the helicopter came to rest in the middle of the platform facing south.

Photographs of the helicopter revealed the vertical fin was completely separated from the tail boom, and both tail rotor blades were sheared-off near the tail rotor.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05CA213