DFW07LA169

NTSB accident investigation · Bell 206L-3 · High Island 138 · July 22, 2007

Accident · No injuriesLimited investigationFinal report
Date
July 22, 2007, 14:50 local (19:50 UTC)
Place
High Island 138
Injuries
3 uninjured
Damage
Destroyed
Phase of flight
Takeoff
Aircraft
N330PBell 206L-3
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 2007
Report
Approved by Office Director
Parties
Baton Rouge, Louisiana
FAA report
20070722016269A
Case key
66291

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

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

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightTakeoff
Weather condition - temperature,high
Rotor rpm - not maintainedPilot in commandCause
In flight collision with objectDescent - uncontrolled
Object - other
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - water
Emergency floats - not deployedPilot in command

Analysis

The 1,236-hour commercial helicopter pilot, who reported having accumulated 79-hours in the same make and model aircraft, lost control of the helicopter while attempting to takeoff from an offshore platform. The pilot performed a pre-departure check of the engine instruments. He then increased collective to gain altitude, as he lowered the nose of the helicopter to gain forward airspeed, and continued his takeoff run. During the takeoff run, as the helicopter neared the edge of the 28 by 28-foot helipad on the platform, the nose of the helicopter yawed to the left, and the helicopter began to descend. The helicopter's right skid collided with a solar panel mounted to the heliport's railing, and the helicopter continued over the edge of the platform descending vertically into the water, about 70-feet below. The pilot reported that he felt that he had experienced a partial loss of engine power which resulted in his loss of control. The pilot further stated that he did not have time to deploy the skid-mounted emergency floats before the helicopter entered the water, and subsequently sank. The temperature at the time of the mishap was 97 degrees Fahrenheit. At the time of the mishap, the helicopter was calculated to be 50-pounds below its maximum gross weight. A post-accident examination of the helicopter and the powertrain did not reveal any pre-accident mechanical anomalies or discrepancies.

Factual narrative

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.

Aircraft

Registration
N330P
Reported as
Bell 206L-3
Category
Helicopter
Serial number
51295
Airframe hours
6,544
Engine
Allison 250-C30P, 650 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Registered owner
Air Logisitics, LLC
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · July 1, 2007
Departed
Gulf of Mexico
Destination
LAF · Layfayette, LA
Flight plan
Company VFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
32
Injuries
None
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, With waivers/limitations
Last flight review
May 1, 2007
Seat
Right
Flight hours
1,236 total · 79 in this make and model · 1,236 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Temperature
97 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N330P · 1

Matched to the same aircraft by N-number and date.