FTW98TA072

NTSB accident investigation · Bell 206B-III · Reserve, NM · December 18, 1997

Accident · Serious injuriesFinal report
Date
December 18, 1997, 16:25 local (23:25 UTC)
Place
Reserve, NM
Injuries
2 serious, 1 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N124DABell 206B-III
Weather
Visual (VMC) · Day
Status
Completed · report June 9, 1999
Report
Approved by Office Director
FAA report
19971218039109A
Case key
20683

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 pilot's inadvertent loss of tail rotor effectiveness. A factor was the high density altitude weather condition.

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 control - in flightManeuvering
Loss of tail rotor effectiveness - inadvertentPilot in commandCause
Weather condition - high density altitudeFactor
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - mountainous/hilly

Analysis

The helicopter was under contract by the New Mexico Game and Fish Department for the purpose of elk herd evaluation. The right front seat passenger said that they were flying northbound, approximately 180 to 200 feet above the ground, in an attempt to split a heard of elk, for counting purposes. He said that the helicopter was traveling at less than 10 knots, the pilot initiated a turn, and within 3 to 5 seconds, they rotated to the ground. The pilot stated that he thought they were traveling north at approximately 100 feet agl and approximately 30 knots when he initiated the right turn. He further stated that 'once the turn got started, I couldn't stop it, even with full left pedal.' The pilot reported that he believed the wind was from the west at approximately 5 to 10 knots (the density altitude was calculated to be 9,043 feet). He said that when the accident happened, 'I heard nothing unusual nor felt anything.' According to FAA AC 90-95, unanticipated right yaw can be brought about by low airspeeds, high power regimes, left crosswinds or tailwinds, and right turning maneuvers.

Factual narrative

On December 18, 1997, approximately 1625 mountain standard time, a Bell 206B-III helicopter, N124DA, was substantially damaged during impact with the ground following loss of aircraft control near Reserve, New Mexico. The airline transport rated pilot received minor injuries and his two passengers were seriously injured. The helicopter was owned by MSI Helicopters Inc., Albuquerque, New Mexico, and operated by Aero West Management, Albuquerque, New Mexico, under Title 14 CFR Part 91 (see attached). Visual meteorological conditions prevailed for the local flight which originated from Reserve, New Mexico, approximately 2 hours before the accident. A company VFR flight plan had been filed.

The helicopter was under contract by the New Mexico Game and Fish Department for the purpose of elk herd evaluation. The field project began on December 10 when the helicopter was flown from Albuquerque to Reserve. During the next 8 days, approximately 58 hours of flight time was accrued accomplishing the project's goals. On the day of the accident, the first flight started at approximately 0800 from Apache Creek. The pilot and his passengers were finishing the third flight for the day when the accident occurred.

The right front seat passenger said that they were flying northbound, at approximately 180 to 200 feet above the ground for elk counting purposes. He said that the helicopter was traveling at less than 10 knots when the pilot initiated a turn (in an attempt to split a herd of elk) and within 3 to 5 seconds, they rotated to the ground. The pilot stated that he thought they were traveling north at approximately 100 feet agl and approximately 30 knots when he initiated the right turn. He further stated that "once the turn got started, he couldn't stop it, even with full left pedal."

The pilot reported that he believed the wind was from the west at approximately 5 to 10 knots (the density altitude was calculated to be 9,043 feet). He said that when the accident happened, "he heard nothing unusual nor felt anything." The helicopter impacted the ground and rolled onto its right side. Approximately 4 hours later, rescue teams reached their location.

According to FAA Advisory Circular 90-95, dated December 26, 1995, entitled "Unanticipated Right Yaw in Helicopters," it states that "all single main rotor helicopters at airspeeds less than 30 knots have a certain degree of vulnerability to unanticipated right yaw." This event can be brought about by low airspeeds flight regimes, high gross weights or high density altitudes (high power demands), left crosswinds or tailwinds, and right turning maneuvers (see attached).

Aircraft

Registration
N124DA
Reported as
Bell 206B-III
Category
Helicopter
Serial number
2052
Airframe hours
10,200
Engine
Allison 250-C20, 425 horsepower, turbo shaft
Damage
Substantial damage
Flight
Aerial observation · Part 91
Operator
Aero West
Registered owner
Msi Helicopters Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · November 5, 1997 · 51 hours before
Departed
NONE
Flight plan
Company VFR

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
52
Certificates
Commercial, Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
11,810 total · 3,500 in this make and model · 10,864 as pilot in command · 150 in the last 90 days · 50 in the last 30 days · 8 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 4 knots
Visibility
25 statute miles
Lowest ceiling
20,000 ft overcast
Temperature
50 °F, dew point 16 °F
Altimeter
29.00 inHg
Observed at
GUP, 140 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.