ANC90FA117

NTSB accident investigation · Bell 206L-1 · Farewell, AK · July 14, 1990

Accident · Serious injuriesField investigationFinal report
Date
July 14, 1990, 09:00 local (17:00 UTC)
Place
Farewell, AK
Injuries
5 serious
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N300AHBell 206L-1
Weather
Visual (VMC) · Day
Status
Completed · report May 10, 1993
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19900714025549A
Case key
5302

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

An internal engine failure due to a thermal fatigue failure of the 1st stage turbine wheel as a result of overtemperature. The high rough/uneven terrain prevented a successful autorotation.

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/malfApproach - vfr pattern - final approach
Turbine assembly,turbine wheel - overtemperatureCause
Turbine assembly,turbine wheel - failure,totalCause
Hard landingLanding - flare/touchdown
Weather condition - high density altitudeFactor
Terrain condition - high terrainFactor
Terrain condition - rough/unevenFactor

Analysis

While approaching a remote mountaintop site to land, at about 100 ft AGL and 40 mph, the engine lost all power as a result of a contained engine failure, and the helicopter made a hard landing. Engine teardown revealed that the 1st stage turbine wheel had failed due to thermal fatigue which originated on the trailing edge o.d. rim surface. In addition, both the 1st and 2nd stage turbine wheel airfoils exhibited evidence of overtemperature operation. The fuel control was properly set. There was no evidence of an internal engine oil fire. Fast engine shutdowns can also result in overtemperatures if sufficient cool down time at idle power is not allowed before the engine is shutdown. The turbine outlet temperature gauge did not incorporate the 'overtemperature light' feature.

Aircraft

Registration
N300AH
Reported as
Bell 206L-1
Category
Helicopter
Serial number
45519
Airframe hours
6,380
Engine
Allison 250-C28B, 500 horsepower, turbo shaft
Damage
Substantial damage
Fire
On-Ground
Flight
Part 135
Operator
Alaska Helicopters, Inc.
Last inspection
100 hour · July 7, 1990 · 12 hours before
Departed
SVW · Sparrevohn Afs, AK
Flight plan
Company VFR
Airport
NONE

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
50
Certificates
Commercial, Flight instructor
Medical
Class 2, Valid Medical--w/ waivers/lim
Flight hours
4,641 total · 330 in this make and model · 4,487 as pilot in command · 36 in the last 90 days · 12 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
40 statute miles
Lowest ceiling
6,500 ft overcast
Temperature
52 °F, dew point 48 °F
Altimeter
30.00 inHg
Observed at
MCG, 55 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.