N571AC

HISTORY OF FLIGHTOn February 8, 2014, about 1945 eastern standard time, a Robinson R44 II, N571AC, was substantially damaged when it impacted trees after takeoff from Wakulla County Airport (2J0), Panacea, Florida. The private pilot and one passenger were fatally injured, and another passenger sustained serious injuries. The helicopter was registered to Capital Helicopters, LLC, and was operated by a flight school. Night visual meteorological conditions prevailed and no flight plan was filed for the flight, which was destined for Tallahassee Regional Airport (TLH), Tallahassee, Florida. The personal flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91.

According to the surviving passenger, the pilot planned to fly three passengers to 2J0 for dinner and return directly to TLH, which was a common flight for the pilot. On the day of the accident, the fourth occupant became ill and elected to stay home. The pilot and two passengers departed TLH about 1720 bound for 2J0. They flew a scenic route along the waterfront and landed at the north end of the airport. The pilot and his passengers finished dinner about 1935 and were then driven to the airport, which was located about 1 mile north of the restaurant. After a preflight inspection, the pilot started the helicopter and announced his position and intentions over the common traffic advisory frequency. The surviving passenger heard the pilot say, "here we go" and seconds later they impacted trees and came to rest inverted in shallow water.

Two witnesses observed the helicopter prior to the accident. One of the witnesses recalled seeing the helicopter parked at the end of runway 36 earlier that day with the tail facing north.

Witnesses who lived in the vicinity of the accident site were interviewed separately shortly after the accident and were asked to describe the weather and lighting conditions that prevailed at the time. The witnesses consistently described the lighting conditions as "dark" or "very" dark and overcast. The surviving passenger recalled a "thin misty fog" that was present at the time of the accident. A witness who lived about 1 mile south of the accident site described the weather conditions at the time of the accident as a dark night, overcast, with no fog. He also stated that the accident site was very dark and added there were no lights from the sky, airport or street that reached the accident site.

According to the surviving passenger, the pilot had requested that she sit in the left rear seat to "even out the weight and balance." A few seconds after takeoff, the passenger observed trees ahead of the helicopter and called out to the pilot prior to impact.

The surviving passenger also remarked that the pilot was "probably trying to fly the fastest route home" as he was intent on returning home to spend time with his daughter and had been gone longer than planned.

An employee at the restaurant where the pilot and two passengers had dinner, reported that the group arrived about 1815. According to a receipt, none of the three patrons consumed alcoholic beverages. The customers paid their bill promptly and then exited the restaurant. The restaurant owner drove the customers to the airport. PERSONNEL INFORMATIONThe pilot, age 49, held a private pilot certificate with a rating for rotorcraft-helicopter. His most recent Federal Aviation Administration (FAA) second-class medical certificate was issued on April 5, 2012 with the limitation, "must wear corrective lenses for near and distant vision." The pilot did not possess an instrument rating.

The pilot obtained most of his flight training for his private pilot certificate through Tallahassee Helicopters. After he received his private pilot certificate in 2012, he continued to rent helicopters from the flight school.

According to the pilot's logbook, as of February 1, 2014 the pilot had accumulated 334.8 total hours of flight experience, 309 hours of which were in helicopters. The pilot recorded at least 189.2 hours of flight experience in the accident helicopter make and model. He had also accumulated 22.6 total hours of night flight experience and only one hour of night flight experience in the preceding 11 months. AIRCRAFT INFORMATIONThe accident helicopter was based at TLH and operated by Tallahassee Helicopters. According to FAA records, the accident helicopter was manufactured in 2005. The helicopter was powered by a Lycoming IO-540-AE1A5 245 hp engine and driven by a two-blade main rotor system. The helicopter's most recent 100-hour inspection was completed on November 15, 2013; at the time it had accumulated 946.4 hours total time in service (TTIS). At the time of the accident the helicopter had accumulated 997.3 TTIS. METEOROLOGICAL INFORMATIONA review of airports within a 50 nautical miles radius of the airport showed similar meteorological conditions.

The following weather observations were recorded at TLH, which was located about 24 nautical miles from the accident site, at an elevation of 83 feet msl:

At 0053, calm wind; visibility 10 statute miles; clear skies; temperature 11 degrees C, dew point 8 degrees C; altimeter 30.15 inches of mercury.

A representative of the National Weather Service (NWS) based in Tallahasee, Florida stated there were no weather reporting facilities closer than 24 nautical miles from the accident site that captured visibility and cloud ceilings at the time of the accident.

According to the U.S. Naval Observatory, on the date of the accident, sunset occurred at 1820 and civil twilight ended at 1845. The moon rise was recorded at 1320, and was observed in transit at 2019 and set at 0320 on the following day. About 68% of the moon disc was illuminated at the time of the accident. AIRPORT INFORMATIONThe accident helicopter was based at TLH and operated by Tallahassee Helicopters. According to FAA records, the accident helicopter was manufactured in 2005. The helicopter was powered by a Lycoming IO-540-AE1A5 245 hp engine and driven by a two-blade main rotor system. The helicopter's most recent 100-hour inspection was completed on November 15, 2013; at the time it had accumulated 946.4 hours total time in service (TTIS). At the time of the accident the helicopter had accumulated 997.3 TTIS. WRECKAGE AND IMPACT INFORMATIONThe accident site was located in a marsh area bordered by trees about 350 feet from the helicopter's departure point. The initial impact point was identified by several damaged tree limbs about 50 feet above the ground, which were about 25 feet from the helicopter's final resting location. The wreckage path was oriented about 340 degrees magnetic and extended from the initial impact point to where the main wreckage came to rest. The main wreckage was inverted in water and oriented on a northerly heading. The middle wire of a three strand power line, also located in the wreckage path, was severed during the accident and repaired before NTSB investigators arrived on scene. There were no indications of pre or postimpact fire.

The wreckage was subsequently recovered from the accident scene and examined at a nearby law enforcement facility.

The tailboom remained attached to the fuselage and was severed about three feet from the tail rotor section. The severed tail section consisted of the tailboom structure, horizontal stabilizer, the upper and lower vertical stabilizers, and the tail rotor. The forward 10-foot section of the tailboom was canted to the left. There was no visible damage to both tail rotor blades, which also remained attached to the tail rotor gearbox. The horizontal and upper vertical stabilizers were intact, and the lower vertical stabilizer exhibited some compression damage.

The main rotor mast was impact separated from the helicopter and co-located with the main wreckage. For reference purposes, the two main rotor blades were arbitrarily designated "A" and "B". Blade "A" was bent about 45 degrees downward and segmented into thirds with most of the blade spar still intact and attached to the main rotor hub. The remaining 10 inches of "Blade A" blade spar were not recovered. The middle third section of the blade was partially separated and the remaining outboard third of the blade was fracture-separated parallel to the blade chord. Blade "B" was bent down about 30 degrees and remained intact to the blade tip. The skin and honeycomb section of the remaining 2 feet of blade had separated. Both blades exhibited compression and impact damage.

The drive belts were broken, but exhibited no signs of rolling. Both the upper and lower actuator bearings rotated freely and the sprag clutch locked and free-wheeled normally. The main rotor gearbox was detached from the airframe, broken into several pieces, and rotated freely.

The engine starter ring gear exhibited linear scoring that was parallel in direction to the gear's rotation. The aft surface of the upper sheave displayed circular scoring and the upper drive belt sheave exhibited multiple scores across its grooves that were consistent with machining marks.

Examination of the flight control system revealed separations consistent with overload on multiple push-pull tubes. There were additional separations within the cyclic stick assembly, cyclic torque tube, and the Blade "B" pitch change link. Control continuity for the cyclic, collective, and anti-torque systems was established and all separations were consistent with overload fractures. All separations in the tail rotor driveshaft were consistent with bending overload. Main and tail rotor gearbox continuity was confirmed.

Both fuel bladder tanks were separated from the main wreckage. The fuel caps remained attached to their respective fuel tanks. The fuel lines were torn at the line outlets, but intact from the tear to the engine. Fuel line continuity was confirmed through the vent lines in the mast fairing, vent fittings on both tanks, interconnect hose, vent hoses and main tank rollover...