DEN07LA155

NTSB accident investigation · Bell 47G-3B-1 · Avondale, CO · September 12, 2007

Accident · No injuriesLimited investigationFinal report
Date
September 12, 2007, 13:30 local (19:30 UTC)
Place
Avondale, CO
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N360SSBell 47G-3B-1
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 2007
Report
Approved by Office Director
Parties
FAA Flight Standards District Office
FAA report
20070912021869A
Case key
66631

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 failure to attain translational lift and his improper flare. A contributing factor in this accident was the sudden wind shift.

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 flightTakeoff
Lift-off - performedPilot in command
Translational lift - not attainedPilot in commandCause
Weather condition - sudden windshiftFactor
In flight collision with terrain/waterLanding
Flare - improperPilot in commandCause
Terrain condition - downhill

Analysis

The pilot took off downhill with no wind. The wind shifted to the west to a tailwind of 10 to 12 knots. The pilot said he was "unable to gain effective translational lift" and he attempted to land with a forward speed of 5 to 6 mph. He attempted to stop the helicopter but in doing so, "the tail skid struck the ground at the same time the skids did. Then the aircraft lurched forward, causing the main rotor to come in contact with the tail boom." The tail boom was severed and the skids were broken torsionally from the airframe.

Factual narrative

On September 12, 2007, approximately 1330 mountain daylight time, a Bell 57G-3B-1, N360SS, piloted by a commercial pilot, was substantially damaged during a hard landing near Avondale, Colorado. Visual meteorological conditions prevailed at the time of the accident. The aerial application flight was being conducted under the provisions of Title 14 CFR Part 137 without a flight plan. The pilot, the sole occupant on board, was not injured. The flight was originating at the time of the accident.

According to the pilot's statement, he was crop dusting a field approximately 17 miles south of Pueblo. He took off downhill with no wind. The wind shifted to the west to a tailwind of 10 to 12 knots. The pilot said he was "unable to gain effective translational lift" and he attempted to land with a forward speed of 5 to 6 mph. He attempted to stop the helicopter but in doing so, "the tail skid struck the ground at the same time the skids did. Then the aircraft lurched forward, causing the main rotor to come in contact with the tail boom." An examination of the helicopter revealed the tail boom was severed and the skids were broken torsionally from the airframe. The helicopter came to rest upright.

Aircraft

Registration
N360SS
Reported as
Bell 47G-3B-1
Category
Helicopter
Serial number
3696
Airframe hours
7,396
Engine
Lycoming TVO-435-B1A, 265 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Registered owner
Olathe Spray Service, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · August 1, 2007 · 30 hours before
Departed
NONE · Avondale, CO
Destination
NONE · Avondale, CO

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
61
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
October 1, 2006
Seat
Left
Flight hours
27,532 total · 1,768 in this make and model · 353 in the last 90 days · 88 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 10 knots, gusting 12
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 28 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.