LAX92LA319

NTSB accident investigation · Bell UH-1B · Hayfork, CA · July 28, 1992

Accident · Minor injuriesLimited investigationFinal report
Date
July 28, 1992, 08:00 local (15:00 UTC)
Place
Hayfork, CA
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N89NWBell UH-1B
Weather
Visual (VMC) · Day
Status
Completed · report September 14, 1993
Report
Approved by Office Director
FAA report
19920728027929A
Case key
27705

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 main rotor drive shaft due to the improper installation by company maintenance personnel of an 'o' ring seal, which allowed the packing grease to escape and caused the over temperature failure of the drive shaft. A factor in the accident was the lack of suitable terrain in which to perform an autorotation.

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/malfunctionHover
Lubricating system,oil seal - looseCause
Lubricating system,oil seal - leakCause
Maintenance,installation - improperCompany maintenance personnelCause
Rotor drive system,engine to transmission drive - overtemperatureCause
Rotor drive system,engine to transmission drive - failure,totalCause
Forced landingDescent - emergency
Autorotation - initiatedPilot in command
Terrain condition - none suitableFactor
Terrain condition - mountainous/hillyFactor
Terrain condition - tree(s)Factor
In flight collision with terrain/waterDescent - emergency

Analysis

The pilot had just dropped off a load of logs and was en route back to the cutting area when he heard a loud bang concurrent with a left yaw and a rapid loss of rotor speed. The pilot entered an autorotation and collided with trees during the descent. Examination revealed that the main rotor drive shaft had failed. Examination of the shaft revealed evidence of a loss of grease from the shaft's boot, which resulted in an overheating condition and catastrophic failure of the unit. The 'o' ring, which provides the grease seal for the shaft boot, was found deformed with evidence that grease had been slung from the boot. The main rotor drive shaft had been removed for maintenance and replaced three days and 6 hours prior to the accident. The maintenance instructions call for a new 'o' ring to be installed when the drive shaft and boot are reassembled. Acording to the bell laboratory, the 'o' ring appeared to have not been replaced.

Aircraft

Registration
N89NW
Reported as
Bell UH-1B
Category
Helicopter
Serial number
62-4576
Airframe hours
5,496
Engine
Lycoming T53-L110, 1,100 horsepower, turbo shaft
Damage
Substantial damage
Flight
Other work use · Part 133
Operator
Northwest Helicopters, Inc.
Registered owner
Northwest Helicopters, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · July 27, 1992 · 6 hours before

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
41
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
13,000 total · 3,000 in this make and model · 12,700 as pilot in command · 300 in the last 90 days · 73 in the last 30 days · 7 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
20 statute miles
Lowest ceiling
None
Temperature
81 °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.