ANC92FA044

NTSB accident investigation · Bell 214B-1 · Hobart Bay, AK · March 6, 1992

Accident · Serious injuriesField investigationFinal report
Date
March 6, 1992, 11:30 local (15:30 UTC)
Place
Hobart Bay, AK
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N314RMBell 214B-1
Weather
Visual (VMC) · Day
Status
Completed · report December 9, 1993
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19920306005209A
Case key
5641

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

The NTSB’s determination of the probable cause, and any contributing factors.

Fatigue failure of the compressor assembly impeller, and inadequate quality control by the manufacturer. A factor which contributed to the accident was the mountainous/hilly terrain.

Analysis

The helicopter was hovering approx 200 ft above the log which was being attached to the cargo hook. The pilots heard a loud bang followed by a loss of engine power. The helicopter autorotated into steep uneven terrain, the only area available. Examination of the engine revealed fatigue failure of the centrifugal impeller encompassing a 60 deg arc. This section separated from the engine and helicopter. Analysis of the impeller showed that the cooling holes, associated only with the T5508D engine, did not have the prescribed radius, and cracks were found emanating from the other cooling holes. The engine records show that the impeller had 5592.0 cycles when installed in this engine in April 1991. The component service life limit of the impeller is 16,600 cycles.

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,impeller - fatigueCause
Inadequate quality controlManufacturerCause
Forced landingLanding - flare/touchdown
Autorotation - performedPilot in command
In flight collision with terrain/waterLanding - flare/touchdown
Terrain condition - none suitableFactor
Terrain condition - mountainous/hillyFactor

Aircraft

Registration
N314RM
Reported as
Bell 214B-1
Category
Helicopter
Serial number
28041
Airframe hours
8,116
Engine
Lycoming T5508D, 2,950 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 133
Operator
Rocky Mountain Aerologging Inc
Registered owner
Rocky Mountain Helicopters Inc
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · March 4, 1992 · 17 hours before
Flight plan
Company VFR

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
46
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
13,000 total · 3,500 in this make and model · 12,000 as pilot in command · 208 in the last 90 days · 56 in the last 30 days · 8 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
99 statute miles
Lowest ceiling
None
Temperature
45 °F
Altimeter
29.00 inHg

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 N314RM · 2

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