ATL94LA180

NTSB accident investigation · Bell UH-1B · Ozark, AL · September 29, 1994

Accident · Minor injuriesLimited investigationFinal report
Date
September 29, 1994, 18:40 local (23:40 UTC)
Place
Ozark, AL
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N41870Bell UH-1B
Weather
Visual (VMC) · Day
Status
Completed · report May 9, 1995
Report
Approved by Office Director
FAA report
19940929035369A
Case key
3452

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 failure of the engines' main bearings because of a lack of lubrication. A factor was the heavily wooded terrain.

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/malfCruise
Engine assembly,bearing - failure,totalCause
Fluid,oil - starvationCause
Forced landingEmergency descent/landing
In flight collision with objectEmergency descent/landing
Object - tree(s)Factor

Analysis

While in cruise, during a positioning flight, the engine chip detector illuminated. A few seconds later it extinguished. Since the terrain was heavily wooded, and the destination airport was about three miles away, the pilot elected to continue toward the airport. Shortly afterwards, the chip light re-illuminated, and the pilot began looking for a landing site. Then the low rotor speed warning horn sounded and the pilot began an autorotation. He was unable to reach an open field, and collided with trees on the edge of the field. During the post accident examination of the engine, the number one, three, and four main bearings were found to have failed because of a lack of lubrication.

Factual narrative

On September 29, 1994, about 1840 central daylight time, a Bell UH-1B, N41870, collided with trees during a forced landing near Ozark, Alabama. The helicopter was operated by Summit Helicopters, Inc. under the provisions of 14 CFR Part 91, and visual flight rules. A flight plan was not filed for the positioning flight. There were no injuries to the commercial pilot, minor injuries to a passenger, and substantial damage to the aircraft. Origination of the flight was Brantley, Alabama, about 1615, on the same day.

The pilot reported that while in cruise flight, the engine chip light illuminated. About five seconds later it extinguished. Since the helicopter was about three miles from the Blackwell Airport, Ozark, Alabama, he elected to continue toward the airport. The chip light re-illuminated and the pilot began searching for a landing site in the heavily wooded terrain. About the same time, the low rotor speed warning horn sounded. An autorotation was established to an open field. The helicopter could not reach the field and collided with trees.

Metal debris was found in the accessory gearbox during a post accident, on-site inspection of the engine. Subsequently, a teardown and inspection of the engine was performed. The number one, three, and four bearings had failed because of a lack of lubrication.

Aircraft

Registration
N41870
Reported as
Bell UH-1B
Category
Helicopter
Serial number
65-12853
Airframe hours
8,119
Engine
Lycoming T53-L-11C, 1,100 horsepower, turbo shaft
Damage
Substantial damage
Flight
Positioning · Part 91
Registered owner
Summit Sales And Leasing, Inc
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Continuous airworthiness · September 5, 1994 · 84 hours before
Departed
NONE · Brantley, AL
Destination
71J · AL

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
47
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
8,300 total · 500 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
7 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 63 °F
Altimeter
29.00 inHg
Observed at
DHN, 12 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.