Accident Details
Probable Cause and Findings
The pilot's continued VFR flight into instrument meteorological conditions (IMC), and his spatial disorientation and loss of control during a subsequent landing. Factors associated with the accident are flat light and whiteout conditions, fog, and snow-covered terrain.
Aircraft Information
Registered Owner (Historical)
Analysis
HISTORY OF FLIGHT
On April 30, 2004, about 1920 Alaska daylight time, a high skid-equipped Bell 206L-3 helicopter, N130AL, sustained substantial damage after colliding with snow-covered terrain, about 56 miles south-southwest of Deadhorse, Alaska. The helicopter was being operated as a visual flight rules (VFR) on-demand charter flight under Title 14, CFR Part 135, when the accident occurred. The helicopter was transporting three research scientists from the University of Alaska campus located in Fairbanks, Alaska. The research team was collecting snow samples at various remote sites from the snow-covered tundra of the North Slope. The contract holder, Veco Polar Resources, Inc., Denver, Colorado, was utilizing Air Logistics of Alaska, Inc, Fairbanks, to provide helicopter support services to the scientific research team. Of the four people aboard the helicopter, the certificated commercial pilot sustained minor injuries, the two surviving passengers sustained no injuries, and the third passenger sustained fatal injuries. Instrument meteorological conditions prevailed at the accident site. Visual meteorological conditions prevailed at the time of departure, and company flight following procedures were in effect. The flight originated about 1600, from the researcher's camp, known as Toolik base camp, located about 95 miles south of Deadhorse.
During an interview with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on May 3, the pilot reported that on the day of the accident, fog delayed the flight's departure from the Toolik base camp until 1600. Before departing the base camp, the pilot contacted the Fairbanks Automated Flight Service Station (AFSS) and obtained a preflight weather briefing. Additionally, he reported that he was able to view satellite weather imagery using a laptop computer at the base camp prior to departure.
The pilot said that after departing from the base camp, the flight proceeded northwest to a series of predetermined landing sites, marked using global positioning satellite (GPS) waypoints. At each of the sites, the researchers would exit the helicopter, collect snow samples, re-board, and then fly to the next site. The pilot said that he was able to reach five of the six sites, but was unable to reach the sixth site due to low fog, reduced visibility, and flat light conditions. He said while attempting to return to the base camp, flying in a southeasterly direction, he encountered an area of very low fog, which reduced his ability to discern a horizon. He said that the visibility deteriorated, and he was unable to discern any topographic features on the surface of the flat, featureless, snow-covered tundra. He elected to make a precautionary landing, and wait for visibility conditions to improve. After remaining on the ground for about 3 minutes, he decided to proceed towards the Toolik base camp. He said that just after takeoff, as the helicopter moved forward, flat light conditions, and worsening fog, contributed to his inability to recognize any topographical features. He reported that while he was attempting to land again, and erroneously believing that the helicopter's skids were already on the ground, he lowered the collective. The helicopter subsequently descended, the landing skids struck the snow-covered tundra, and the helicopter rolled to the right, with the main rotor blades striking the ground. As the main rotor blades struck the tundra, the helicopter continued to roll onto its right side, the main rotor mast sheered off, and one main rotor blade struck the top left portion of the helicopter's cabin. The main rotor blade subsequently sliced through the left side of the helicopter, and struck the passenger that was seated in the front left seat.
The pilot stated that immediately after the accident he contacted the operator's Fairbanks based operations manager using a satellite phone, and informed him of the accident. The helicopter sustained substantial damage to the fuselage, tail boom, and main rotor drive train system. The pilot noted that there were no preaccident mechanical anomalies with the helicopter.
A review of the Fairbanks AFSS telephone conversation tapes from April 30 indicated the pilot called at 0722 and requested a weather briefing for the current conditions at Deadhorse, the terminal forecast for Deadhorse, and the terminal forecast for Deadhorse area. The AFSS specialist provided the current weather conditions at Deadhorse, and the Deadhorse terminal forecast.
According to AFSS telephone conversation transcripts, the accident pilot stated, in part: "Yes, I just want to get the uhh what Deadhorse has right now." The AFSS specialist on duty responded by saying, in part: "Okay, right now they're yucky." The AFSS specialist then provided the pilot with the current conditions at Deadhorse, which included, visibility of 1/4 of a mile in fog, and an indefinite ceiling of 100 feet. The AFSS specialist said: "So, it looks like they expect the fog to hang in there... Unfortunately, unless you want to crawl along on the ground." The accident pilot responded by saying: Yeah, that's what I've done for the last two days." The pilot then said: "OK, I may call back around ten then."
At 1543, the pilot again contacted the Fairbanks AFSS and again asked the AFSS specialist on duty for the current weather conditions at Deadhorse. The AFSS specialist reported current Deadhorse weather conditions as: Wind 070 at 6 knots; five miles visibility in mist; ceiling 300 feet overcast; temperature 25 degrees F; dew point 23 degrees F; altimeter 30.31 inHg.
A complete transcript of the telephone conversations between the accident pilot and the Fairbanks AFSS is included in the public docket for this accident.
CREW INFORMATION
The pilot held a commercial helicopter pilot certificate, and a helicopter instrument rating. In addition, he held a commercial airplane pilot certificate with airplane single-engine land, multiengine land, and an instrument airplane rating.
The most recent first-class medical certificate was issued to the pilot on September 29, 2003.
The pilot was hired by Air Logistics of Alaska on February 23, 2004. After completion of his initial ground and flight training, he satisfactorily completed an initial 14 CFR 135.293/.299 check ride on March 5, 2004, in an Air Logistics of Alaska Bell 206B helicopter.
According to the NTSB Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) submitted by Air Logistics of Alaska, dated May 13, 2004, the pilot's total flight time consisted of 7,200.9 hours, of which 2,000 were accrued in the accident helicopter series. In the past preceding 90 and 30 days prior to the accident, the report lists a total of 69.9 and 23.9 hours, respectively.
During a brief follow-up interview with the NTSB IIC on December 2, 2004, the accident pilot reported that his total flight time in Bell 206L-3 helicopters was 41.5 hours. He said that his time in a Bell 206L-3 helicopter was accumulated while employed by Air Logistics of Alaska, which included training and check ride flight time, as well as revenue producing flight hours. He added that the balance of his helicopter time reported by the operator was accumulated in a Bell 206B, and OH-58 helicopters. An OH-58 helicopter is a military variant of the Bell 206B helicopter. He said that a majority of his recent helicopter flight time was accumulated in US Military, UH-60 Blackhawk helicopters.
At the time of the accident, the pilot was a full-time helicopter pilot for the United States Army. During his time in service with the United States Army, he was stationed in various theaters around the world, including Alaska. He accumulated about 6,144.0 flight hours in helicopters, and about 987.0 hours in airplanes.
AIRCRAFT INFORMATION
The helicopter was a Bell Helicopter Textron 206L-3, equipped with a Rolls Royce 250-C30P engine.
The helicopter was maintained under the operator's Approved Aircraft Inspection Program (AAIP), which requires inspections to be performed approximately every 100 flight hours. The helicopter had accumulated 13,305.8 hours in service at the time of the accident. 1.6 hours had elapsed since the most recent Phase 1 inspection.
METEOROLOGICAL INFORMATION
The closest official weather observation station is located in Nuiqsut, Alaska, which is located about 47 nautical miles northwest of the accident site. On April 30, 2004, at 1853, an Aviation Routine Weather Report (METAR) was reporting, in part: Wind, calm; visibility, 8 statute miles; ceiling and clouds, 700 feet overcast; temperature, 25 degrees F; dew point, 21 degrees F; altimeter, 30.34 inHg.
An AIRMET was issued for mountain obscuration in clouds and precipitation, with instrument meteorological conditions along the northern slopes of the Brooks Range.
In a written statement to the NTSB dated May 1, 2004, the pilot included a description of the weather conditions at the time of the accident. He wrote, in part: "The weather had fog in the area with visibility of approximately 1/2 to 1-1/2 miles."
WRECKAGE AND IMPACT INFORMATION
The National Transportation Safety Board investigator-in-charge, along with three representatives from Air Logistics of Alaska, and a representative from the Federal Aviation Administration (FAA) Fairbanks Flight Standards District Office, attempted to reach the accident site by helicopter on May 1, 2004, but reduced visibility due to fog and flat light conditions prevented the helicopter from reaching the site until the following day.
The topographical features surrounding the accident site consisted of smooth, featureless, and snow-covered tundra. There was a gradual upward slope in the direction of the accident helicopter's preaccident flight path. In addition, there was a set of helicopter skid tracks imprinted in th...
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC04FA049