MIA83LA199

NTSB accident investigation · Bell 206B · Stuart, FL · August 4, 1983

Accident · No injuriesLimited investigationFinal report
Date
August 4, 1983, 19:45 local (23:45 UTC)
Place
Stuart, FL
Injuries
4 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N51DCBell 206B
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830804040599A
Case key
30925

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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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/malfCruise - normal
Turbine assembly,shaft - corrodedCause
Turbine assembly,shaft - failure,totalCause
Turbine assembly,turbine wheel - overspeedFactor
Turbine assembly,turbine wheel - failure,totalFactor
Forced landingLanding - flare/touchdown
Autorotation - performedPilot in command

Analysis

While in cruise flt at aprx 600 ft AGL, a catastrophic failure of the engine's 3rd stage turbine occurred. The plt related that he observed an engine chip detector light, which was followed almost immediately by fire in the engine. He made a successful autorotative landing. The fire was extinguished by use of hand fire fighting equipment. Fire damage was limited to the engine area. The engine was shipped to the manufacturer's facility for examination. According to their report, the failure occurred due to what appeared to be an oil type corrosion from the I.d. surface of the inner power turbine shaft; corrosion weakened the shaft by reducing the wall thickness which resulted in it fracturing & allowing the 3rd stage turbine wheel to separate from the 4th stage turbine sheel & overspeed; the 3rd stage wheel then experienced an uncontained burst failure as a result of the overspeed.

Aircraft

Registration
N51DC
Reported as
Bell 206B
Category
Helicopter
Serial number
2732
Airframe hours
6,329
Engine
Allison 250-C20B, 317 horsepower, turbo shaft
Damage
Substantial damage
Fire
In-Flight
Flight
Personal · Part 91
Registered owner
Sundance Helicopter Svc., Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · February 4, 1983 · 1 hours before

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
43
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
5,820 total · 5,200 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
100° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 73 °F
Altimeter
30.00 inHg
Observed at
VRB

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 N51DC · 1

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