DEN90FA172

NTSB accident investigation · Aerospatiale SA316B · Meeteetse, WY · August 20, 1990

Accident · Serious injuriesField investigationFinal report
Date
August 19, 1990, 18:00 local (Aug 20, 1990, 00:00 UTC)
Place
Meeteetse, WY
Injuries
3 serious, 4 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N83776Aerospatiale SA316B
Weather
Visual (VMC) · Day
Status
Completed · report December 14, 1992
Report
Approved by Office Director
FAA report
19900819034069A
Case key
17844

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 main rotor head blade dampener failure. A factor in the accident was the subsequent failure of a blade restraining cable.

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 control - in flightCruise
Rotor system,main rotor hub lead-lag stop/damper - failure,totalCause
Cyclic - uncontrolledPilot in command
Rotor system,main rotor hub stop(static/dynamic) - failure,totalFactor
Forced landingDescent - uncontrolled
Terrain condition - open field
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Approximately 2 minutes into the flight, the pilot experienced a slight 1 to 1 vibration through the cyclic. This type vibration is associated with main rotor dampers and the pilot 'stirred' the cyclic in an effort to purge air out of the blade dampers. This eliminated the problem, however, it recurred and could not be eliminated. The vibration increased to the point of loss of control. An emergency landing was attempted with touchdown occurring at about 60 knots. The helicopter came to rest inverted and was largely consumed by post-impact fire. Metallurgical analysis on a failed blade restraining cable revealed a catastrophic failure in a low cycle fatigue mode consistent with a secondary cause, and due to short term vibrations. In addition to fatigue, there was evidence of plastic deformation due to vibratory loads from the damper systems. Fire damage prevented additional failure analysis.

Aircraft

Registration
N83776
Reported as
Aerospatiale SA316B
Category
Helicopter
Serial number
1827
Engine
Turbomeca 316B, 600 horsepower, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Part 135
Operator
Rocky Mountain Helicopter
Registered owner
Unknown
Destination
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
42
Certificates
Commercial, Airline transport, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 1, Valid Medical--w/ waivers/lim
Flight hours
6,635 total · 500 in this make and model · 5,000 as pilot in command · 50 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 10 knots
Visibility
7 statute miles
Lowest ceiling
6,000 ft overcast
Temperature
-0 °F, dew point -0 °F

FAA reports on this event · 1

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