ATL91FA013

NTSB accident investigation · Bell 47J-2 · Gatlinburg, TN · November 1, 1990

Accident · Serious injuriesField investigationFinal report
Date
November 1, 1990, 14:00 local (19:00 UTC)
Place
Gatlinburg, TN
Injuries
1 serious, 2 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N49DABell 47J-2
Weather
Visual (VMC) · Day
Status
Completed · report December 14, 1992
Report
Approved by Office Director
FAA report
19901101048849A
Case key
8296

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 accident was inadequate maintenance of the helicopter, allowing a tail rotor drive shaft bearing to exceed wear limits. This resulted in high loads on the tail rotor drive shaft, and the resulting fatigue failure of the drive shaft.

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 drive system,tail rotor drive shaft bearing - wornCause
Rotor drive system,tail rotor drive shaft - fatigueCause
Maintenance,inspection - inadequateCompany maintenance personnelCause
Misc eqpt/furnishings,seat belt - improper
Loss of control - in flightCruise - normal
In flight collision with objectDescent - uncontrolled
Object - tree(s)
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The two passengers reported that they heard a 'pop' sound, followed by the helicopter starting a clockwise spin to the right. The helicopter descended into the trees on the side of a steep slope. Investigation revealed that the tail rotor drive shaft failed immediately forward of the tailboom extension tube. The drive shaft failed from fatigue cracking, propagating at a high rate, suggesting high loads. The t/r drive shaft forward bearing housing outer diameter dimension and the inner diameter of the tailboom extension tube were worn beyond replacement limits and should have been replaced according to the bell maintenance and overhaul manual. The passenger three-place bench seat had been altered so that the individual seat belts had been modified into one single long belt. The belt could be opened only on the left side of the belt; the buckle on the right side of the belt was taped closed with silver duct tape.

Aircraft

Registration
N49DA
Reported as
Bell 47J-2
Category
Helicopter
Serial number
1825
Airframe hours
8,972
Engine
Lycoming VO-540-B1B3, 260 horsepower, reciprocating
Damage
Destroyed
Flight
Part 91
Operator
Pigeon Forge Helicopters, Inc.
Registered owner
Pigeon Forge Helicopters, Inc
Last inspection
Annual · October 7, 1990 · 85 hours before
Departed
NONE · Pigeon Forge, TN

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
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Front
Toxicology
Performed
Flight hours
8,448 total · 8,370 as pilot in command · 385 in the last 90 days · 120 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
15 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 43 °F
Altimeter
30.00 inHg
Observed at
TYS, 26 nm away

FAA reports on this event · 1

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