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November 15, 1998 · Bell 206B · N21466

Matagorda 713

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
November 15, 1998
Injury Outcomes
No injuries (1 uninjured)
Location
Matagorda 713
Aircraft
Bell 206B
Tail Number
N21466
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW99LA026

During takeoff from an offshore oil platform, the helicopter impacted the platform. After the accident, it was confirmed that the helicopter's front two skid tie down straps were not removed during preflight.

NTSB Probable Cause

The pilot's loss of control due to his failure to untie ground straps. A factor was his inadequate preflight inspection.

Full Narrative

On November 15, 1998, approximately 0945 central standard time, a Bell 206B helicopter, N21466, was substantially damaged during takeoff from Matagorda 713, an oil platform on the Gulf of Mexico. The commercial pilot, sole occupant of the helicopter, was not injured. The aircraft was owned and operated by Industrial Helicopters Inc., of Lafayette, Louisiana. Visual meteorological conditions prevailed and no flight plan was filed for the Title 14 CFR Part 91 positioning flight. According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot stated that his schedule the morning of the accident was to transport several different people to four separate platforms. Before leaving the platform, he untied all three platform tiedowns on the helicopter and visually "checked the floats, skids, cross tubes, and the helicopter in general." After untying the main rotor blade he began to fuel the helicopter. Prior to takeoff, he reported completing the checklist. After takeoff, he proceeded to fly the helicopter to M1638, which was the first scheduled platform. His last stop was M1713 where he dropped off two passengers and proceeded to "shut down" the helicopter. At 9:30 a.m. the 10,771 hour pilot secured, "the two front tie downs" to the platform due to the prevailing 30 to 34 knot wind conditions. Subsequently, the pilot decided to take off and he "checked the wind on the air speed indicator", and the winds were still about the same. He untied the main rotor blade, got into the helicopter, and started the engine. As the pilot "pulled pitch" to takeoff, the aircraft pitched forward. He then pulled back on the cyclic and the aircraft "started to come apart." After the accident, the pilot confirmed that he had not removed the front tie downs on the helicopter. After contacting Industrial Helicopter, Inc., arrangements were made by the company for a medical check and drug test of the pilot. The results were negative. The mast and a section of the tail boom separated from the helicopter during the accident sequence.

Flight

Event TypeAccident
Event Time15:45 UTC
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206B
Tail NumberN21466
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250 C-20 · Turboshaft · 420
Seats5

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 61 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind360° @ 15 kt, gusting 25 kt
Visibility10 sm
CeilingOvercast 700 ft
Temperature / Dew Point66 F / 16 C
Altimeter30.00 inHg
Observation Time15:56
Weather SourceWFAC

Appendix: Source Data