ATL90LA042

NTSB accident investigation · Bell TH-1 · Creola, AL · December 20, 1989

Accident · No injuriesLimited investigationFinal report
Date
December 20, 1989, 08:20 local (14:20 UTC)
Place
Creola, AL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N106SRBell TH-1
Weather
Visual (VMC) · Day
Status
Completed · report October 7, 1992
Report
Approved by Office Director
FAA report
19891220052119A
Case key
8191

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

On this page

Probable cause

The loss of engine power due to a #21 bearing failure. The bearing failed as a result of inadequate maintenance. A factor in the accident was the pilot operating the helicopter within the avoid operating envelope.

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
Turbine assembly,shaft bearing - contaminationCause
Turbine assembly,shaft bearing - seizedCause
Maintenance - inadequateOther maintenance personnelCause
Forced landingLanding - flare/touchdown
Autorotation - performedPilot in command
In flight collision with terrain/waterLanding - flare/touchdown
Proper altitude - not maintainedPilot in commandFactor

Analysis

The engine failed while the pilot was hovering at 110 ft during an external load operation. The pilot released the load and autorotated into a swampy area. Engine teardown showed evidence of seizure and heavy wear at the #21 bearing assembly roller/shaft interface. Metallurgical exam revealed a breakdown of the tungsten carbide and cobalt coating repair. The detonation gun (dgun) repair buildup on the bearing/seal journal, seo T53-LO-R0035, was used in 1969, and canceled in 1970. The procedure was not approved or practiced by Lycoming, and the manufacturer recommended that parts repaired iaw the seo not be installed in engines. The pilot was operating within the 'avoid operation' area of the airspeed velocity chart.

Aircraft

Registration
N106SR
Reported as
Bell TH-1
Category
Helicopter
Serial number
157806
Airframe hours
8,403
Engine
Lycoming T53-L13B, 1,100 horsepower, turbo shaft
Damage
Substantial damage
Flight
Other work use · Part 91
Registered owner
Scott Paper Company
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · November 29, 1989 · 80 hours before
Departed
Mt Vernon, AL
Destination
Mobile, AL

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
42
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 1, Valid Medical--no waivers/lim.
Flight hours
15,534 total · 3,629 in this make and model · 296 in the last 90 days · 56 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 10 knots
Visibility
10 statute miles
Lowest ceiling
3,000 ft overcast
Temperature
39 °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.