ANC84LA089

NTSB accident investigation · Bell 205A-1 · Talkeetna, AK · June 12, 1984

Accident · No injuriesLimited investigationFinal report
Date
June 12, 1984, 14:30 local (22:30 UTC)
Place
Talkeetna, AK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N58116Bell 205A-1
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19840612024259A
Case key
4303

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

On this page

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.

Airframe/component/system failure/malfunctionCruise - normal
Rotor system,main rotor blade - fatigueCause
Rotor system,main rotor blade - failure,partialCause
Rotor system,main rotor blade - corrodedCause
Rotor system,main rotor blade - crackedCause
Forced landingLanding - flare/touchdown
Terrain condition - mountainous/hillyFactor

Analysis

The plt had just picked up an external 'sling' load of 2700 lbs of back-fill in a cement bucket. At 900 ft AGL the acft started a vertical vibration. As collective was bottomed a large piece of one main rotor blade separated. The plt said he jettisoned the load and the 100 ft line and landed the acft in a mountain side clearing. During the post accident examination a portion of the main rotor blade about 32 inches long was found missing. This failure started with a crack on the blade. While on the ground the drooping of the blade would tend to close and mask the crack on the bottom of the blade where it would more readily have been seen. A general aviation airworthiness alert stated that fractures on helicopter blades occur at locations where blade damage existed. Damage ranging from scratches, dents, nicks or corrosion pits became a potential point for stress to concentrate and propagate into cracks leading to blade failure.

Aircraft

Registration
N58116
Reported as
Bell 205A-1
Category
Helicopter
Serial number
30133
Airframe hours
4,388
Engine
Lycoming T53-13, 1,250 horsepower, turbo shaft
Damage
Substantial damage
Flight
Other work use · Part 133
Registered owner
Alaska Helecopter, Inc.
Airworthiness certificate
Standard, Utility
Last inspection
100 hour · May 30, 1984 · 50 hours before
Departed
Gold Creek, AK
Flight plan
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
43
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
9,430 total · 450 in this make and model · 9,400 as pilot in command · 400 in the last 90 days · 200 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
100 statute miles
Lowest ceiling
None
Temperature
68 °F, dew point 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 N58116 · 1

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