DFW08LA140

NTSB accident investigation · Robinson Helicopter R22 Marine · Austin, TX · May 10, 2008

Accident · No injuriesLimited investigationFinal report
Date
May 10, 2008, 12:15 local (17:15 UTC)
Place
Austin, TX
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N8316DRobinson Helicopter R22 Marine
Defining event
Maneuvering-low-alt flying: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report December 8, 2008
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20080510836329A
Case key
68002

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 maintain rotor RPM while maneuvering at a low altitude, which resulted in a loss of control.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot and pilot rated passenger were operating a single-engine helicopter equipped with pontoons over a lake for the purpose of photographing recreational boats. Several witnesses observed the helicopter flying erratic and at a low altitude over the boats before it impacted the water and rolled inverted. The pilot stated that they were tracking a boat approximately 100 feet above the ground level. The boat was traveling to the south and they were flying to the north with a tail wind. He said that he executed a right hand turn and noticed that the rotor RPM had begun to decrease, the rotor RPM horn came on, and the governor light began to flash. The pilot immediately began to execute a low rotor RPM recovery by lowering the collective, increasing engine power, and continuing to turn into the wind but was unable to recover RPM before hitting the water. The helicopter hit the water and bounced back up with a bit of a wave. When the helicopter came back down, a wake from one of the boats they had been tracking washed over the floats, which caused the helicopter to roll to the front and flip over. The governor controller was examined and no anomalies were noted.

Factual narrative

On May 10, 2008, at 1215 central daylight time, a Robinson R22 Mariner, N8316D, a single-engine helicopter, sustained substantial damage when it collided with the water while maneuvering over Lake Travis, in Austin, Texas. The certified commercial pilot and the pilot rated passenger were not injured. The helicopter was registered to a private company and operated by Boat Pix, West Palm Beach, Florida. No flight plan was filed for the flight that departed Austin-Bergstrom International Airport (AUS), Austin, Texas, around 1030, and was destined for Lake Travis. Visual meteorological conditions prevailed for the business flight conducted under 14 Code of Federal Regulations Part 91.

Several witnesses observed the helicopter flying at a low altitude over the boats on Lake Travis. One witness said, "The Boatpix helicopter was flying around another boat and then headed our way. He traveled directly over our boat and veered to the starboard. He was about 50 feet off the water - when he passed he rose up then circled behind us. When he passed the boat his angle of attack was pretty steep. He took a hard right bank turn - came down low and back at us - following from our stern - came down to the water and bounced the pontoons onto the water. It started to dig in the water and I turned to shield myself." The next time the witness saw the helicopter it was upside down in the water.

Another witness was driving a ski boat when he first noticed the helicopter performing what he described as "aeronautic maneuvers." He said, "These [maneuvers] appeared to be dangerous because they were 6-8 feet off the water, then they would pull up sharply and bank right." The witness then observed the helicopter fly directly over him followed shortly after by the sound of a "slapping" noise. He then saw the helicopter's two pontoons floating in the water.

In a written statement, the pilot stated that he and the pilot rated passenger were tracking a boat approximately 100 feet above the ground level. The boat was traveling to the south and they were flying to the north with a tail wind. He said, "I executed a right hand turn and noticed that the rotor RPM had begun to decrease, the rotor RPM horn came on, and my governor light began to flash. I immediately began to execute a low rotor RPM recovery by lowering the collective, rolling on more throttle, and continuing to turn into the wind. I tired to recover the RPM but noticed we would not recover RPM before hitting the water." The pilot told the pilot rated passenger that they were not going to recover and he attempted to use the remaining rotor RPM to slow the descent. The helicopter hit the water and bounced back up with a bit of a wave. When the helicopter came back down, a wake from one of the boats they had been tracking washed over the floats, which caused the helicopter to roll to the front and flip over.

The pilot rated passenger provided a similar account of the accident sequence in a separate written statement.

The helicopter was towed to the shore and recovered. The governor controller (part number: B286-2, serial number 1415) was removed and sent to Robinson Helicopter Company where it was examined under the supervision of the Safety Board on May 21, 2008. When examined, there was no visible external damage to the unit. It was installed on a calibrated test bench and subjected to the acceptance test protocol in Robinson Helicopter Company Process Specification RPS-59. The controller assembly met all acceptance criteria for a new or factory overhauled until, which applies to a controller returned from the field. The controller was not unsealed for a visual inspection of the internal components because it met the above acceptance criteria.

The pilot held a commercial pilot certificate and certified flight instructor rating for helicopters. His last second class FAA medical was issued on March 10, 2008. He reported a total of 895.4 hours, of which 871 hours were in the same make and model as the accident helicopter.

Weather at Austin-Bergstrom International Airport, about 23 miles west of Lake Travis, at 1153, was reported as wind from 190 degrees at 12 knots gusting 17 knots, visibility two miles and haze, clouds broken at 1,800 feet, overcast clouds at 2,200 feet, temperature 79 degrees Fahrenheit, dew point 41 degrees Fahrenheit, and a barometric pressure setting of 29.75 inches of Mercury.

Aircraft

Registration
N8316D
Reported as
Robinson Helicopter R22 Marine
Category
Helicopter
Serial number
2481M
Engine
Lycoming 0-320 SERIES, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Operator
Boat Pix
Registered owner
Marinephoto Helicopter LLC
Airworthiness certificate
Standard, Normal
Departed
AUS · Austin, TX
Destination
Lake Travis, TX
Airport
None

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
28
Injuries
None
Certificates
Flight instructor, Commercial
Instrument ratings
Helicopter
Medical
Class 2, With waivers/limitations
Last flight review
August 5, 2007
Seat
Left
Flight hours
895 total · 871 in this make and model · 668 as pilot in command · 257 in the last 90 days · 116 in the last 30 days
Role
Co-pilot
Age
32
Injuries
None
Certificate
Private
Medical
Class 3, Without waivers/limitations
Last flight review
August 20, 2007
Seat
Right
Flight hours
199 total · 183 in this make and model · 122 as pilot in command · 34 in the last 90 days · 32 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 12 knots, gusting 17
Visibility
2 statute miles
Lowest ceiling
1,800 ft broken
Temperature
79 °F, dew point 72 °F
Altimeter
29.75 inHg
Observed at
AUS, 23 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.

Other investigations on N8316D · 1

Matched to the same aircraft by N-number and date.