DEN02TA100

NTSB accident investigation · Bell 206L-3 · Saguache, CO · August 26, 2002

Accident · Serious injuriesFinal report
Date
August 26, 2002, 16:30 local (22:30 UTC)
Place
Saguache, CO
Injuries
1 serious, 3 minor
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N801HMBell 206L-3
Weather
Visual (VMC) · Day
Status
Completed · report April 1, 2003
Report
Approved by Office Director
Parties
FAA Flight Standards District Office
FAA report
20020826024359A
Case key
55566

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 inadequate in-flight planning and decision making, and the loss of tail rotor effectiveness. A contributing factor was the right quartering tailwind.

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 flightApproach - vfr pattern - final approach
In-flight planning/decision - inadequatePilot in commandCause
Loss of tail rotor effectivenessCause
Weather condition - crosswindFactor
Weather condition - tailwindFactor
In flight collision with objectDescent - uncontrolled
Object - tree(s)

Analysis

The pilot said that smoke coming from the forest fire indicated winds were from the east. He approached the fire from the north, circled in a counterclockwise direction, and began his approach to the landing zone from the west. On approach, the helicopter lost tail rotor effectiveness and spun to the right. A firefighter on the scene recorded the wind from the southwest at 15 knots, but this information was not relayed to the pilot. The helicopter was not equipped with a high altitude tail rotor kit.

Factual narrative

On August 26, 2002, approximately 1630 mountain daylight time, a Bell 206L-3, N801HM, registered to Redding Air Service, Redding, California, and operated by the United States Forest Service (USFS), Golden, Colorado, was substantially damaged when it collided with trees and impacted terrain during landing approach 15 miles west-northwest of Saguache, Colorado. The commercial pilot was seriously injured and three passengers received minor injuries. Visual meteorological conditions prevailed. No FAA flight plan was filed, but a USFS flight plan was filed and the helicopter was being flight followed by the Forest Service. The public use flight, operating under Title 14 CFR Part 135, originated at Salida, Colorado, approximately 1545.

The following is based upon a report submitted by the U.S. Forest Service accident investigator. The pilot reported for duty at 0800. He had been off the previous two days. At midday, the pilot was dispatched to a fire site near Salida and was forced to abandon two landing attempts due to loss of tail rotor effectiveness associated with wind conditions (this landing site was 50 miles north of the accident site). At 1530, the pilot was dispatched to a wildland fire on Trickle Mountain approximately 15 miles northwest of Saguache. The helicopter departed Salida at 1545. On board were three firefighters and various fire fighting tools and equipment. The helicopter arrived on scene at 1620. Upslope smoke indicated the wind was from the east. A firefighter on the ground with a "belt weather kit" measured the wind direction and velocity from the southwest at 15 knots. This information was not relayed to the pilot. The pilot approached the fire from the north and circled in a counterclockwise direction. He sighted a suitable landing site in a saddle (elevation approximately 9,840 feet msl) south of Trickle Mountain and circled again. As he made his landing approach from the west, the helicopter lost tail rotor effectiveness and began to rotate to the right. The pilot added power and the helicopter moved off in a southeast direction and struck several trees. [After reviewing this report, a USFS safety manager said the pilot did not add additional power until after the rotor blades contacted the trees. He added power in an attempt to fly out of the situation.] Rotation increased and the pilot reduced power and collective pitch. The helicopter impacted terrain in a near vertical descent on a southerly heading. The skids collapsed, the fuselage hit the ground, and the helicopter rolled over on its left side and the main rotor blades struck the ground. An 8-foot portion of one rotor blade was hurled 100 feet away. At the time of the accident, the temperature was approximately 78 degrees F. The pilot said the helicopter was not equipped with a high altitude tail rotor kit. Forest Service personnel consulted Bell Helicopter-Textron and learned that there is no high altitude tail rotor kit available for the Bell 206L-III.

Aircraft

Registration
N801HM
Reported as
Bell 206L-3
Category
Helicopter
Serial number
51218
Airframe hours
6,934.1
Engine
Allison A-250-C30P, 650 horsepower, turbo shaft
Damage
Substantial damage
Flight
Public aircraft · Public use
Operator
U.S. Forest Service
Registered owner
Redding Air Service Helicopters
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 21, 2002 · 18.3 hours before
Departed
0V2 · Salida, CO

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Injuries
Serious
Certificate
Commercial
Airplane ratings
Single-engine sea
Medical
Class 1, Valid Medical--no waivers/lim.
Last flight review
February 27, 2002
Seat
Right
Flight hours
9,348 total · 4,495 in this make and model · 173 in the last 90 days · 54 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 15 knots, gusting 24
Visibility
5 statute miles
Lowest ceiling
None
Temperature
82 °F, dew point 21 °F
Altimeter
30.19 inHg
Observed at
GUC, 34 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.