DEN89LA059

NTSB accident investigation · Bell 206B III · Park City, UT · January 8, 1989

Accident · No injuriesLimited investigationFinal report
Date
January 8, 1989, 14:27 local (21:27 UTC)
Place
Park City, UT
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Standing
Aircraft
N16733Bell 206B III
Weather
Visual (VMC) · Day
Status
Completed · report January 11, 1990
Report
Approved by Office Director
FAA report
19890108001319A
Case key
17662

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 selection of an unsuitable landing site by the pilot, resulting in tail rotor contact with the terrain and shearing of the tail rotor driveshaft.

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.

On ground/water encounter with terrain/waterStanding - idling rotors
Terrain condition - snow coveredFactor
Terrain condition - uphillFactor
Unsuitable terrain or takeoff/landing/taxi area - selectedPilot in commandCause
Clearance - not maintainedPilot in commandCause
Loss of control - in flightHover
Rotor drive system,tail rotor drive shaft - sheared
Directional control - not possible
On ground/water encounter with terrain/waterLanding - flare/touchdown
Autorotation - performed

Analysis

The commercial plt flew a rescue team to a mountain avalanche area. The team deplaned and during the unloading procedure the helicopter settled backwards into loose snow. The plt added collective pitch and attempted to hover. As the helicopter left the ground, an uncommanded right spin began. The plt performed a hovering autorotation 30 feet away from the ground personnel. At touchdown the tail boom entered deep snow and the acft came to rest nose high. The plt discovered the tail rotor shaft had broken forward of the tail rotor gear box. A post accident investigation showed evidence that the tail rotor blades entered loose snow and were subjected to rapid deceleration. The shaft had sheared under applied torque.

Aircraft

Registration
N16733
Reported as
Bell 206B III
Category
Helicopter
Serial number
2138
Airframe hours
3,439
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Other work use · Part 91
Operator
Avman Inc, doing business as Helicopter Svcs
Registered owner
Avman, Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · December 2, 1988 · 31 hours before
Departed
NONE
Destination
NONE
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
43
Certificates
Flight instructor, Commercial, Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
7,404 total · 2,663 in this make and model · 7,280 as pilot in command · 107 in the last 90 days · 33 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 10 knots, gusting 15
Visibility
50 statute miles
Lowest ceiling
None
Temperature
19 °F
Altimeter
30.00 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 N16733 · 2

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