ANC92FA040

NTSB accident investigation · Bell 214B-1 · Hobart Bay, AK · February 23, 1992

Accident · FatalField investigationFinal report
Date
February 23, 1992, 15:30 local (19:30 UTC)
Place
Hobart Bay, AK
Injuries
6 fatal, 5 serious
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N814RMBell 214B-1
Weather
Visual (VMC) · Day
Status
Completed · report August 26, 1993
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19920223003299A
Case key
5640

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 NTSB’s determination of the probable cause, and any contributing factors.

Separation of the tail rotor and 90 degree gearbox due to the pilot's failure to follow procedures/directives which resulted in the external load cable becoming entangled in the tail rotor. Factors were the turbulent weather and the lack of suitable terrain for a forced landing.

Analysis

The pilot in command had a mechanic attach a 30 foot choker cable to the external cargo hook so that when he came to a hover to pick up passengers, the cable would touch the ground and dissipate the static electricity. After picking up the last timber cutters, en route to base camp, the helicopter flew through turbulence and a passenger in the cabin yelled. The pilot turned to look at the passenger, looked forward, heard a bang and experienced a yaw. The tail rotor and 90 degree gearbox separated from the helicopter and he autorotated into tall trees. Subsequent examination showed the marks in the tailrotor blade matched the socket shape at the end of the cable.

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
External load sling/harness - entangledCause
Rotor drive system,tail rotor gearbox(90 deg) - separationCause
Procedures/directives - not followedPilot in commandCause
Weather condition - turbulenceFactor
Forced landingDescent - emergency
In flight collision with objectDescent - emergency
Object - tree(s)
Terrain condition - none suitable

Aircraft

Registration
N814RM
Reported as
Bell 214B-1
Category
Helicopter
Serial number
28067
Airframe hours
6,675
Engine
Lycoming T-5508D, 2,930 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 133
Operator
Rmh Aerologging
Registered owner
Rmh Aeromedical, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · February 20, 1992 · 12 hours before
Departed
Field Site, AK

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
51
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
16,335 total · 7,811 in this make and model · 16,335 as pilot in command · 243 in the last 90 days · 172 in the last 30 days · 10 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 20 knots
Visibility
3 statute miles
Lowest ceiling
3,000 ft overcast
Temperature
43 °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.