N330P

Destroyed
None

Bell 206L-3S/N: 51295

Accident Details

Date
Sunday, July 22, 2007
NTSB Number
DFW07LA169
Location
High Island 138
Event ID
20070807X01124
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The loss of control as result of the pilot's failure to maintain rotor RPM during takeoff.

Aircraft Information

Registration
N330P
Make
BELL
Serial Number
51295
Engine Type
Turbo-shaft
Year Built
1989
Model / ICAO
206L-3B06T
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 July 22, 2007, at 1450 central daylight time, an emergency float equipped Bell 206L-3 helicopter, N330P, sustained substantial damage upon with the water following a loss of control while attempting to take off from offshore platform High Island 138, in the Gulf of Mexico. The flight was departing from the offshore platform, located about 150 miles south of Lafayette, Louisiana, when the accident occurred. The commercial pilot and the two passengers were not injured. The helicopter was registered to and operated by Air Logistics, LLC., of New Iberia, Louisiana. A company flight plan was filed for the cross-country flight that was destined for the Lafayette Regional Airport (LFT), near Lafayette, Louisiana. Visual meteorological conditions prevailed for the on demand air taxi flight conducted under 14 Code of Federal Regulations Part 135.

According to the accident pilot's written statement that was included with the NTSB Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1) submitted by the operator, the pilot reported that just after takeoff, as he hovered the helicopter over the heliport, he performed a pre-departure check of the engine instruments and everything "looked good." The pilot also noted that a crane was located next to the heliport, so he planned to depart with a correction for a slight left crosswind. While still at a hover above the heliport, the pilot increased the collective to gain altitude, while he lowered the nose of the helicopter to gain forward airspeed and continue his takeoff run. The pilot added that as the helicopter gained forward airspeed nearing the edge of the heliport, the nose of the helicopter yawed to the left, and the helicopter began to descend. The pilot reported that he applied right tail rotor pedal in an attempt to stop the yaw, but the helicopter subsequently drifted to the right, and the right skid collided with "something."

The pilot wrote, in part: "It felt like we lost engine power but I don't think it cut completely... At that point the helicopter came back to the right I do not remember how we cleared the deck but I was able to get 'Mayday' a few times over the radio but don't know if I got the tail number in or not. Once we cleared the platform the helicopter fell down into the water. On the way down I recall hearing an audio warning but do not know which one. Upon hitting the water I don't know if I got the collective up all the way to cushion the landing, but [I] did not have time to deploy the floats." During the impact with the water the windscreen broke and the helicopter filled with water, rolled onto its left side, and sank. All three occupants were able to exit the helicopter and were immediately rescued by the crew of a nearby fishing boat.

According to the operator, the pilot was attempting to take off from a 28 by 28-foot-wide platform when the right skid of the helicopter collided with a solar screen that was attached to the heliport's safety fence. The helicopter, which weighed approximately 4,100 pounds (max gross weight was 4,150 pounds), then descended approximately 70-100 feet and collided with the water in a nose low attitude. The helicopter's floats were armed, but were not deployed. The helicopter sank in 47-feet of water, but was later recovered and transported to the operator's facility in New Iberia, Louisiana.

On July 25, 2007, a Federal Aviation Administration (FAA) airworthiness inspector from the Baton Rouge Flight Standards District Office examined the accident helicopter. The inspector reported the outboard sections of both main rotor blades had separated, the tail rotor drive shaft was sheared, and the windshield was broken. Additionally, flight control continuity was established for all flight controls and examination of the helicopter's fuel system and engine revealed there were no pre-accident mechanical deficiencies.

The operator reported that the accident pilot held a commercial pilot certificate for rotorcraft-helicopter, and had accrued a total of 1,236-hours in helicopters, of which, 78.6-hours were in the Bell 206L-3 helicopter.

Personnel who were present at the offshore platform at the time of the accident reported the weather as calm winds, with sea state calm. The temperature at the time of the accident was reported as approximately 97 degrees Fahrenheit.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW07LA169