Thursday, November 24, 2011

Beechcraft 23 Musketeer, N8700M: Accident occurred November 23, 2011 in West Milton, Ohio

http://registry.faa.gov/N8700M

NTSB Identification: CEN12FA082
 14 CFR Part 91: General Aviation
Accident occurred Wednesday, November 23, 2011 in West Milton, OH
Probable Cause Approval Date: 04/10/2013
Aircraft: BEECH 23, registration: N8700M
Injuries: 1 Fatal.

NTSB investigators either traveled in support of this investigation or conducted a significant amount of investigative work without any travel, and used data obtained from various sources to prepare this aircraft accident report.

The non-instrument-rated pilot was conducting the accident flight under visual flight rules without a flight plan in dark, night, instrument meteorological conditions. Radar data depicted that shortly after departure, the airplane performed a series of multi-directional turns at varying altitudes. Several witnesses observed or heard the airplane over their residences complete several turns at a low altitude. Based on the erratic flight of the airplane, the wreckage distribution, which was consistent with a high-speed impact, and the low visibility present at the time of the accident, it is likely that the pilot experienced spatial disorientation and lost control of the airplane. A postaccident examination of the airplane revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. Local law enforcement officers who responded to the accident site reported the clouds were about 700 feet above ground level when they arrived at the accident site. There is no record of the accident pilot receiving an official or "unofficial" weather briefing before departure. Federal Aviation Administration guidance indicated that spatial disorientation can occur when there is no natural horizon or surface reference, such as night flight in sparsely populated areas similar to that of the accident area and conditions.

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

The non-instrument-rated pilot's decision to attempt a flight into instrument meteorological conditions, which resulted in the pilot’s spatial disorientation and subsequent loss of control of the airplane.

HISTORY OF FLIGHT

On November 23, 2011, at 2043 eastern standard time, a Beech 23 single-engine airplane, N8700M, sustained substantial damage when it impacted terrain while maneuvering near West Milton, Ohio. The non instrument-rated private pilot, who was the co-owner and operator of the airplane, sustained fatal injuries. Instrument meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight departed the Phillipsburg Airport (3I7), Phillipsburg, Ohio, at 2038, and was en route to Marion, Ohio.

According to friend of the pilot, the pilot arrived at 3I7 approximately 1400. The pilot and friend spent a few hours together and the pilot prepared to depart 3I7 approximately 2030 to return home. Prior to the flight, the pilot mentioned that the cloud layer was very low and he was going to stay under the controlled airspace near 3I7. The friend noted the pilot departed 3I7 at 2038 according to the time set in her vehicle and had no further communication with the pilot.

A review of the radar data showed the airplane shortly after departure from 3I7 traveling on a northeasterly heading. Approximately 1 mile from 3I7, the data depicted the airplane make a left 360-degree turn and then continue to the northeast. Shortly thereafter, the airplane entered another left 360-degree turn and then a series of sudden left and right turns. During the turns, the airplane's altitude fluctuated between 1,000 and 2,200 feet mean sea level. At 2043, radar contact was lost.

A pilot-rated witness, who was located near the accident site, reported that the airplane sounded like it was very low and made 2 to 3 tight radius circles. During each turn, the engine sounded as it was running at a very high RPM as if the airplane was in a dive, then the airplane would level off before sounding like it was in another dive. On the final turn, the engine was running at a high RPM like it was in a steep dive, and then he heard an impact. The witness described the engine operation as "healthy" until the impact.

Several witnesses located near the accident site heard or observed the airplane near their residences. The witnesses described the airplane as flying low near the tree tops and the engine sound was loud. The witnesses heard the engine and then it suddenly stopped. Several witnesses then called 911 and assisted rescue personnel in locating the airplane.

PERSONNEL INFORMATION

The pilot held a private pilot certificate with an airplane single-engine land rating. He was issued a third class medical certificate on March 11, 2001, with the limitation for corrective lenses.

According to the pilot's logbook, he accumulated 306 total flight hours, 224 flight hours in the accident airplane, and 4.6 hours of simulated instrument flight time. The pilot's most recent flight review was conducted on July 3, 2011, in the accident airplane.

A family member of the pilot reported the pilot was healthy and had no medical issues.

AIRCRAFT INFORMATION

The airplane was a Beech 23, serial number M-484, and manufactured in 1963. It was powered by a 160-horsepower Lycoming O-320-D2B engine and equipped with a Sensenich fixed pitch propeller. The airplane was registered to the pilot on January 9, 2006.

A review of the maintenance records revealed the most recent annual inspection was completed on June 20, 2011, at a total airframe time of 1,854.6 hours.

METEOROLOGICAL INFORMATION

At 1956, the Dayton International Airport (DAY), Dayton, Ohio, automated surface observing system (ASOS), located 8 nautical miles southeast of the accident site, reported the wind from 270 degrees at 7 knots, 8 miles visibility, sky clear, temperature 4 degrees Celsius, dew point 3 degrees Celsius, and an altimeter setting of 30.26 inches of Mercury.

At 2042, the DAY ASOS reported the wind from 250 degrees at 7 knots, 6 miles visibility, mist, sky broken at 700 feet, temperature 3 degrees Celsius, dew point 3 degrees Celsius, and an altimeter setting of 30.26 inches of Mercury.

Local law enforcement officers who responded to the accident site reported the clouds were approximately 700 feet above ground level when they arrived at the accident site.

There is no record of the accident pilot receiving an official or "unofficial" weather briefing before departure.

WRECKAGE AND IMPACT INFORMATION

Postaccident examination of the airplane showed the airplane impacted in a freshly harvested corn field near a tree line. No evidence of tree strikes were noted in the accident area. Impact ground scars were noted directly underneath the leading edges of both wings and the underside of the fuselage. The engine and two-blade propeller were found embedded in the terrain approximately 3 feet in depth. Fragmented sections of the fuselage and wings were located about 25 feet forward of the main wreckage. The main wreckage consisted of the fuselage, both wings, engine, and empennage.

The left wing leading edge was crushed aft and the wing skins were separated from the wing ribs and spars. The aileron and flap remained attached to the wing. The fuel tank was ruptured and fragmented. The wing tip fairing was fragmented. The landing gear was attached and bent aft.

The right wing leading edge was crushed aft and the wing skins were separated from the wing ribs and spars. The aileron and flap remained attached to the wing. The fuel tank was ruptured and fragmented. The wing tip fairing was fragmented. The landing gear was attached and bent aft.

The lower forward fuselage was crushed aft and partially embedded in the terrain. The upper fuselage was bent up and crushed aft. The instrument panel was fragmented and destroyed. The attitude indicator and directional gyro were disassembled to examine the gyro wheels and housings. The gyro wheels were free to move within the housings and radial scoring was noted inside the housings and on the gyro wheels.

The empennage was crushed and bent. The vertical stabilizer was partially bent and the rudder remained attached. The horizontal stabilator was intact and no damage was noted.

Aileron and flap control continuity was confirmed from the cockpit control yoke to the control surfaces. Stabilator and rudder control continuity was confirmed from each control surface to the control yoke and the rudder pedals, respectively.

Internal engine continuity was confirmed and compression was obtained at each cylinder during crankshaft rotation. The spark plugs exhibited signatures consistent with normal operation. The vacuum pump was disassembled; the rotor and vanes were fractured. Both propeller blades displayed s-type bending, and chordwise scratches and polishing were noted on the chambered side of the blades.

MEDICAL AND PATHEOLOGICAL INFROMATION

The Montgomery County Coroner's Office performed the autopsy on the pilot on November 25, 2011. The autopsy concluded that the cause of death was multiple blunt force trauma and the report listed the specific injuries.

The Federal Aviation Administration’s (FAA) Civil Aerospace Medical Institute (CAMI), Oklahoma City, Oklahoma, performed toxicological tests on specimens that were collected during the autopsy. Tests for carbon monoxide and cyanide were not performed. Results were negative for volatiles, and unspecified level of Diphenhydramine was detected in the liver and kidney.

ADDITIONAL INFORMATION

FAA's AC (Advisory Circular) 60-4A, entitled “Pilot’s Spatial Disorientation,” states that disorientation is caused by a lack of visual reference to the natural horizon, and can be brought about by low visibility, night conditions, and reflected light from the anticollision rotating beacon. Disorientation can cause the pilot to inadvertently place the airplane in a dangerous attitude. To avoid becoming disoriented, the Advisory recommends that pilots obtain training and maintain proficiency in aircraft control by reference to instruments, to rely solely on those instrument indications, and to avoid flying in poor or deteriorating weather conditions.


NTSB Identification: CEN12FA082 
14 CFR Part 91: General Aviation
Accident occurred Wednesday, November 23, 2011 in West Milton, OH
Aircraft: BEECH 23, registration: N8700M
Injuries: 1 Fatal.


This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. NTSB investigators either traveled in support of this investigation or conducted a significant amount of investigative work without any travel, and used data obtained from various sources to prepare this aircraft accident report.

On November 23, 2011, at 2044 eastern standard time, a Beech 23 single-engine airplane, N8700M, sustained substantial damage when it impacted terrain while maneuvering near West Milton, Ohio. The non-instrument rated private pilot, who was the co-owner and operator of the airplane, sustained fatal injuries. Instrument meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight departed the Phillipsburg Airport (3I7), Phillipsburg, Ohio, at 2038, and was destined for Marion, Ohio.

According to friend of the pilot, the pilot arrived at 3I7 approximately 1400. The pilot and friend spent a few hours together and the pilot prepared to depart 3I7 approximately 2030 to return home. The friend noted the pilot departed 3I7 at 2038 according to the time set in her vehicle and had no further communication with the pilot.

Several witnesses located near the accident site heard or observed the airplane near their residences. The witnesses described the airplane as flying low near the tree tops and the engine sound was loud. The witnesses heard the engine and then it suddenly stopped. Several witnesses then called 911 and assisted rescue personnel in locating the airplane.

Postaccident examination of the airplane showed the airplane impacted in a freshly harvest corn field near a tree line. No evidence of tree strikes were noted in the accident area. Impact ground scars were noted directly underneath the leading edges of both wings and the underside of the fuselage. The engine and two-blade propeller were found embedded in the terrain approximately 3 feet in depth. Fragmented sections of the fuselage and wings were located approximately 25 feet forward of the main wreckage. The main wreckage consisted of the fuselage, both wings, and empennage.

At 1956, the Dayton International Airport (DAY), Dayton, Ohio, automated surface observing system (ASOS), located 8 nautical miles southeast of the accident site, reported the wind from 270 degrees at 7 knots, 8 miles visibility, sky clear, temperature 4 degrees Celsius, dew point 3 degrees Celsius, and an altimeter setting of 30.26 inches of Mercury.

At 2042, the DAY ASOS reported the wind from 250 degrees at 7 knots, 6 miles visibility, mist, sky broken at 700 feet, temperature 3 degrees Celsius, dew point 3 degrees Celsius, and an altimeter setting of 30.26 inches of Mercury.

Local law enforcement officers who responded to the accident site reported the clouds were approximately 700 feet above ground level.

Clovis Dawson
Dawson’s family has faced tragedy before: His wife, Nancy Fitzgivens, a caseworker for Franklin County Children Services, was stabbed to death in 2001 while visiting a family whose seven children had been taken away.


Watch Video


WEST MILTON -- A local man’s passion ends in tragedy. The single-engine Beechcraft Musketeer flown by 70-year-old Clovis Dawson went down in Miami County Wednesday night.

What caused the crash remains unknown.

The pilot was merely doing what so many people do this time of year: taking time to visit friends. ABC6/Fox28 News’ Dana Jay reports that Dawson took off on a day trip Wednesday.

Sadly, he would never return home.

"He loved to fly. He was quite enthused about aviation."

Dan Stover says he frequently saw Dawson at the Marion Municipal Airport, located about 45 minutes due north of Columbus. He said Dawson found joy in his life.

"He and his son would be in and out quite a bit," said Stover, who manages the Marion airport.

Dawson and his son had two planes.

"They were together quite a lot,” Stover said. “They were pretty close."

Perhaps sadder, still. This most recent tragedy -- Dawson’s fatal plane crash -- isn’t the first time ABC6/Fox28 News has encountered the Dawson family.

ABC6/Fox28 News spoke to Mr. Dawson about 10 years ago. Someone had murdered his wife during the course of her working on a case for Franklin County Children Services.

"The terror that she must have felt fighting for her life,” Dawson said. “We were gonna grow old together."

Dawson, himself, may have felt terror in the final moments of his life, too. Jay reports he flew from Marion to visit a friend in Dayton.

On his way back, Dawson crashed in a field in Miami County, just west of West Milton. Crews on the ground say the plane took a nose dive and crumpled as it ran to ground.

West Milton Fire Chief Denny Frantz says the plane did not burn upon impact and that debris was crumpled.

The crash remained under investigation as of Thursday. Federal investigators are expected to join the the effort already underway by the local fire department in Miami County.

Stover said, "It could be multiple things and really until they do the investigation and get all the details, I wouldn't be able to tell you. There's a lot of things that could cause that."

The pilot of a 1963 Beechcraft plane died in a crash around 8:45 p.m. Wednesday in the vicinity of S. Range Line Road and Emerick Road in Miami County. The victim has been identified as Clovis Dawson, 70, of Columbus.









A Columbus man died in a single-engine plane crash Wednesday night in a wooded area near West Milton.

The Miami County Sheriff’s Department identified the victim as Clovis Dawson, age 70.

Dawson was the pilot of a four-seat 1963 Beechcraft Model 23 airplane that crashed around 8:40 p.m. Wednesday at 6421 South Rangeline Road, said Deputy Mike Marion, a crash reconstructionist.

Dawson’s point of origin and destination are still unknown. At one point his plane was on the ground at Phillipsburg Airport, “but I don’t what time in relation to the crash,” Marion said. The crash site is about three miles northeast of the Phillipsburg Airport.

The cause of the crash has not yet been determined, Marion said. Several witnesses in the area described what they heard to sheriff’s deputies.

“One person said it sounded like the engine was cutting out. Another person who is a former pilot said it sounded like the pilot was manually revving the engine,” Marion said. “Other people said that they heard it above their house and no longer than it took them to get outside to see what was going on is when they heard it crash.”

West Milton Fire Chief Denny Frantz said the plane did not burn upon impact and that debris was crumpled as if it had possibly nose-dived into the ground.

West Milton firefighters who responded had trouble locating the crash scene initially. The plane was found by Laura fire crews nearly a mile from the road in a corn field.

Investigators from the Federal Aviation Administration and National Transportation Safety Board aren’t due at the scene until Friday because of the Thanksgiving holiday. Sheriff’s deputies are securing the crash scene until the federal officials arrive.

Dawson was removed to the Montgomery County Coroner’s office in Dayton for an autopsy. The autopsy results aren’t expected until Friday, a coroner’s office spokesman said.