FTW89LA036

NTSB accident investigation · Bell 206B-III · S.Timbalier 151 · January 3, 1989

Accident · Minor injuriesLimited investigationFinal report
Date
January 3, 1989, 12:50 local (18:50 UTC)
Place
S.Timbalier 151
Injuries
1 minor
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N22704Bell 206B-III
Weather
Visual (VMC) · Day
Status
Completed · report July 11, 1990
Report
Approved by Office Director
FAA report
19890103000149A
Case key
22825

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

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Probable cause

A collision between the aircraft and the platform during the emergency autorotation which caused the left skid and float to separate and destabilized the autorotation. The collision was probably unadoidable due to the maneuver that was being conducted at the onset of the emergency. The emergency landing was attempted following an engine failure that was the result of a total compressor failure. The compressor failure was caused by a fatigue failure of the sixth stage wheel which separated. The failure was initiated due to a casting inclusion in the wheel which was not detected during the manufacturing process.

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 engine power(total) - mech failure/malfHover
Compressor assembly,rotor disc - failure,totalCause
Compressor assembly,casting - fatigueCause
Maintenance,rebuild/remanufacture - improperManufacturerCause
In flight collision with objectDescent - emergency
Object - building(nonresidential)Cause
In flight collision with terrain/waterDescent - emergency
Terrain condition - water

Analysis

The acft experienced an eng failure during a sling load pick up on an offshore platform. During the autorotation, the left skid and float struck a handrail on the rig and separated. The acft impacted the water, nose low, and rolled over as a result of the separated float. Investigation revealed that the eng failure was a result of a 6th stage compressor wheel fatigue failure. The wheel fatigue originated at a casting inclusion that had not been detected during the manufacturing process.

Aircraft

Registration
N22704
Reported as
Bell 206B-III
Category
Helicopter
Serial number
3614
Airframe hours
8,213
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Destroyed
Flight
Other work use · Part 133
Registered owner
Petroleum Helicopters, Inc
Airworthiness certificate
Standard, Utility
Last inspection
AAIP · December 18, 1988 · 45 hours before
Departed
S.T. 151
Destination
S.T. 151
Flight plan
Company VFR
Airport
151 · S. Tim 151

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
40
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
3,522 total · 1,431 in this make and model · 3,143 as pilot in command · 134 in the last 90 days · 55 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 16 knots
Visibility
10 statute miles
Lowest ceiling
10,000 ft broken
Temperature
79 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
300, 15 nm away

FAA reports on this event · 1

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