N911GF

HISTORY OF FLIGHT

On March 26, 2016, about 0018 central daylight time, a Eurocopter AS350 B2, N911GF, impacted trees and terrain near Enterprise, Alabama. The airline transport pilot, flight nurse, flight paramedic, and patient being transported were fatally injured. The helicopter, which was registered to Haynes Life Flight LLC and operated by Metro Aviation, Inc., was substantially damaged. The flight was operated under the provisions of Title 14 Code of Federal Regulations (CFR) Part 135 as a helicopter air ambulance flight. Night instrument meteorological conditions (IMC) prevailed for the flight, which operated on a company visual flight rules (VFR) flight plan. The flight departed from a farm field near Goodman, Alabama, about 0017, and was destined for Baptist Medical Center Heliport (AL11), Montgomery, Alabama.

According to the Coffee County Sheriff's Office, on March 25, 2016, about 2309, sheriff's deputies and the Enterprise Rescue Squad were dispatched to a motor vehicle accident (MVA) near Goodman, Alabama. A sheriff's deputy contacted Haynes Ambulance Communication Center (HCC) by cellular phone when he learned that the motor vehicle was overturned and that an unconscious victim was inside.

According to communications records, HCC received the call from the deputy at 2319:10. The pilot of the helicopter, was notified at 2320:38. The helicopter, which was known as "Life Flight 2" and was based at the Troy Regional Medical Center, Troy, Alabama, departed Troy at 2326:57 and arrived at the landing zone (LZ) in a farm field adjacent to the MVA site at 2353:15.

Witnesses stated that, after touchdown, the pilot remained in the helicopter with the engine running. The flight paramedic and flight nurse exited the helicopter and entered the Enterprise Rescue Squad ambulance to help prepare the patient for transport.

Once the patient was ready for transport, the flight nurse, flight paramedic, and several other emergency responders rolled the gurney about 70 yards through a grassy area to the helicopter and loaded the patient on-board. One of the first responders later reported that he noticed that the pilot had something over his eyes "like sunglasses, but it was square looking." Once the patient had been loaded, the flight nurse and flight paramedic also boarded, and, at 0016:45, the helicopter lifted off and turned north toward AL11.

Review of radar data provided by the United States Army from the approach control radar site at Cairns Army Airfield (OZR), Fort Rucker, Alabama, located about 13 nautical miles east of the accident site, indicated that, the helicopter was first identified on radar after takeoff at 0017:35. The helicopter was in a shallow left turn and climbing to 1,000 ft above mean sea level. At 0018:04, the rate of turn began to increase and continued to increase over the next 4 seconds when the helicopter reached a peak altitude of 1,100 ft. The helicopter remained at this altitude and continued the left turn until 0018:28 when the helicopter began a rapid descent. Five seconds later, radar indicated that helicopter had descended through 600 ft. Moments later, the helicopter descended below the floor of the radar coverage area, and radar contact was lost. According to the radar data, the flight lasted about 1 minute.

According to HCC, the helicopter's on-board Skyconnect satellite tracking system updated every 3 minutes, and the pilot was supposed to contact them every 15 minutes. However, after the helicopter lifted off, HCC did not receive the pilot's normal 15-minute check-in, and, when they checked the satellite tracking system, it showed that it had not updated and that the helicopter was still at the LZ. HCC then began to notify authorities that they believed that the helicopter was down somewhere. About 0700, after an extensive search, search parties began to smell what they believed was jet fuel and eventually located the wreckage in a swampy, heavily wooded area.

PERSONNEL INFORMATION

According to Federal Aviation Administration (FAA), Metro Aviation, and pilot records, the pilot held an airline transport pilot certificate with a helicopter rating and type ratings for the Agusta Westland AB-139 and AW-139. He also held a flight instructor certificate with ratings for helicopter and instrument helicopter.

The pilot was hired as a flight instructor in June 2009 by Helicopters of America. He then became their lead flight instructor and worked for them until September 2009 when the company ceased operation. He was then hired by Cloud 9 Helicopters, where he became senior flight instructor.

On April 14, 2011, he was hired by Petroleum Helicopters International (PHI). When hired by PHI, he had accrued 2,448 total hours of helicopter flight experience and had flown the R22, R44, H269, AS355, MD500, MD600, and A109.

At PHI, he flew the AW139 as both a first officer (co-pilot) and a captain (pilot) in both visual flight rules (VFR) and instrument flight rules (IFR) operations. During his tenure at PHI, he accrued an additional 1,889.63 flight hours supporting oil and gas contracts until he left their employment on November 16, 2015.

At the time of the accident, the pilot had been employed by Metro Aviation for about 6 months and had accumulated 90 hours of flight experience in the accident helicopter make and model since he was hired. His total flight experience was 5,301 hours of which 5,265 hours were as pilot in command, 474 hours were at night, and 265 hours were in actual instrument conditions. His flight experience during the 90 days before the accident was 47 hours, including 20 hours in the 30 days before the accident.

Review of Metro Aviation/PHI training records indicated that he had received training in human factors and decision-making, night operations, night vision goggles (NVGs), and inadvertent entry into IMC. He did not meet currency requirements for flight in IMC at the time of the accident.

AIRCRAFT INFORMATION

The helicopter was manufactured in 1998. It was equipped with a three-blade main rotor system and a two-blade tail rotor system and was powered by a Turbomeca Arriel 1D1 engine rated at 641 shaft horsepower. The helicopter was equipped with skid-type landing gear, a night vision imaging system (NVIS), which consisted of NVGs and NVG-compatible lighting, a helicopter terrain avoidance warning system (HTAWS), and an autopilot. The helicopter was not certificated for flight in IMC.

According to Metro Aviation, the helicopter was maintained under an FAA-approved aircraft inspection program. The helicopter's most recent inspection was completed on February 12, 2016. At the time of the accident, the helicopter had accrued 8,923.2 total hours of operation.

METEOROLOGICAL INFORMATION

Videos, Photographs, and Witness Information

Witness statements indicated that fog, mist, and reduced visibility existed at the MVA site at the time of the helicopter's arrival. Witness statements, photographs, and videos also indicated that these conditions were still present when the helicopter lifted off about 23 minutes later.

Review of witness videos and photographs of the accident flight revealed that, during the takeoff sequence, very light to light precipitation was falling in the field surrounding the helicopter. The precipitation was also visible in the helicopter's landing light beams directed forward from the helicopter.

According to one witness, there was slight drizzle around the time of the takeoff, and, although there was no ground fog, there may have been fog above the trees. Another witness stated that there was a heavy mist, and the ceiling was "very low, maybe 100 foot." This witness also stated he could see the tops of the trees, and, by shining his flashlight up, he could easily tell that the fog started about two to three times as high as the nearest tree. Another witness stated that, at the time of the helicopter's departure, the fog was mixed with rain and was "kind of pretty thick." This witness also mentioned that the helicopter flew over the road, which was not far from the LZ, and the witness lost visual contact with the helicopter due to the fog.

Surface Analysis Chart

The National Weather Service (NWS) Surface Analysis Chart for 0100 depicted a stationary front that stretched from the northeastern Gulf of Mexico north-northeastward into southeastern Alabama and northeastward into western South Carolina. A low-pressure center was located in eastern Alabama. The station models around the accident site depicted air temperatures in the low to mid 60's degrees Fahrenheit (°F), with temperature-dew point spreads of 1°F or less, a southeast to east wind below 10 knots, cloudy skies, and fog. Areas near frontal boundaries with low temperature-dewpoint spreads at the surface are typically locations conducive to the formation of low clouds and fog, and, if enough moisture is available, precipitation can also be present.

Surface Observations

Enterprise Municipal Airport (EDN), located 4 miles east-northeast of the accident site, was the closest official weather station to the accident site and had an Automated Weather Observing System (AWOS). EDN weather at 0015 was reported as wind from 120° at 4 knots, 3 miles visibility, drizzle, an overcast ceiling at 300 ft above ground level (agl), temperature of 17°C, dew point temperature of 17°C, and an altimeter setting of 29.97 inches of mercury. EDN weather at 0035 was reported as wind from 120° at 4 knots, 3 miles visibility, drizzle, an overcast ceiling at 300 ft agl, temperature of 17°C, dew point temperature of 17°C, and an altimeter setting of 29.97 inches of mercury.

Observations from other stations near the accident site also indicated low instrument flight rules (LIFR) conditions due to ceilings below 500 ft agl at the accident time.

Satellite Data

Visible and infrared images obtained from the Geostationary Operational Environmental Satellite number 13 indicated abundant cloud cover over ...