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September 29, 2004 · Bell 206L · N34CA

Gulf Of Mexico

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 29, 2004
Injury Outcomes
No injuries (3 uninjured)
Location
Gulf Of Mexico
Aircraft
Bell 206L
Tail Number
N34CA
Injuries
None
Aircraft Damage
Destroyed
NTSB Number
MIA04LA132

The pilot stated that while on approach, within about 300 to 400 yards of the oil platform, as he increased collective input to control the rate of descent, the engine failed to respond normally. As collective input was increased he said the rpms decreased and did not recover, so he stopped applying collective to stop the rotor rpms from decreasing below 90 percent. According to the pilot, no other adverse indications were observed, and the rate of descent increased. He said he applied the remaining collective pitch input to arrest the rate of descent just prior to impacting the water. After impact he said he tried 2 times to inflate the floats, but both attempts were unsuccessful. He and both passengers exited the helicopter, and it sank in about 600 feet of water, and was not recovered.

NTSB Probable Cause

A loss of engine power for undetermined reasons while on short final to land on an oil platform in the Gulf of Mexico, which resulted in the pilot ditching the helicopter into the water.

Full Narrative

On September 29, 2004, about 0615 central daylight time, a Bell 206L helicopter, N34CA, registered to and operated by Panther Helicopters Inc., as a Title 14 CFR part 135 on demand air taxi flight, ditched into the Gulf of Mexico. Visual meteorological conditions prevailed, and a company visual flight rules flight plan was filed. The airline transport-rated pilot and two passengers were not injured, and the helicopter sank in the Gulf of Mexico, and was not recovered. The flight originated in Belle Chasse, Louisiana, the same day, about 0508. The pilot stated that the hour-long flight from Belle Chasse, Louisiana, to Viosca Knoll oil platform No. VK817, had initially been uneventful. He further stated that at a distance of approximately 2 miles from the platform, he started a descent from his cruising altitude of 1,000 feet. During the final approach, when within about 300 to 400 yards, he said he increased collective input to control the rate of descent, but the engine failed to respond normally. As collective input was increased, he said the rpms decreased and did not recover. He said he stopped applying collective to prevent the rpms from decreasing below 90 percent, and further stated that he noted no other adverse indications. He said the rate of descent increased, and he applied the remaining collective pitch input to arrest the rate of descent, just prior to impacting the water. The helicopter impacted the water with "normal forces", and the pilot said he tried twice to inflate the floats, but both attempts were unsuccessful. During the ditching, the helicopter had impacted the surface of the water with a slight movement to the left front, and the main rotor on the left side impacted the water. The pilot said that he and both passengers exited the helicopter, and it sank in about 600 feet of water. Personnel from a nearby boat recovered the pilot and passengers from the Gulf of Mexico, and transported them to the oil platform. The passenger who was seated in the front left seat, said that when the helicopter was about 300 yards from the platform, it "started going down" and attempts by the pilot to "lift" the helicopter were unsuccessful. He further stated that he did not notice anything unusual with the helicopter during the flight, until it was located within 300 yards of the platform, when heard no sounds associated with the main rotor blades impacting the water. He said the pilot tried three separate times to deploy the floats, but all attempts were unsuccessful.

Flight

Event TypeAccident
Event Time11:15 UTC
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206L
Tail NumberN34CA
Aircraft CategoryHeli
DamageDestroyed
Operating RulePart 135
Engines1
Engine TypeTurboshaft
Engine DetailsRolls-Royce · 250-C20 SER · Turboshaft · 450
Seats7

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 58 · First Class · None

Conditions

ConditionsVMC
LightDawn
WindCalm
Visibility4 sm
CeilingNone
Temperature / Dew Point70 F
Altimeter29.93 inHg
Observation Time10:51
Weather SourceWFAC

Appendix: Source Data