Lawrence Klimek
Mooney M20J/201, N201DG
Aviation Accident Final Report - National Transportation Safety Board
The National Transportation Safety Board traveled to the scene of this accident
Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Philadelphia, Pennsylvania
Investigation Docket - National Transportation Safety Board:
Location: Cape May, New Jersey
Accident Number: ERA19FA184
Date & Time: May 29, 2019, 11:15 Local
Registration: N201DG
Aircraft: Mooney M20J
Aircraft Damage: Substantial
Defining Event: Miscellaneous/other
Injuries: 1 Fatal
Flight Conducted Under: Part 91: General aviation - Personal
Analysis
The pilot was seen by multiple witnesses flying low just above the ocean surface near the shoreline. One witness stated that he saw the airplane flying about 10 ft above the ocean when it contacted the water, climbed about 100 to 200 ft, then entered a steep dive and impacted the water in a near-vertical attitude.
Postaccident examination of the wreckage revealed no pre-impact mechanical deficiencies that would have precluded normal operation of the airplane. Following a death investigation, the state medical examiner classified the manner of death as suicide.
Probable Cause and Findings
The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's intentional flight into water as an act of suicide.
Findings
Personnel issues Suicide - Pilot
Factual Information
History of Flight
Maneuvering-low-alt flying Miscellaneous/other (Defining event)
On May 29, 2019, at 1115 eastern daylight time, a Mooney M20J, N201DG, was destroyed when it was involved in an accident near Cape May, New Jersey. The commercial pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
In a written statement, a witness described seeing the airplane flying parallel to the beach about 10 ft above the water. He stated that it appeared "stable and in control but then dipped, hit the water, and skipped up out of control." The airplane entered a steep climb to around 100 to 200 ft above the water, “stalled, turned downward, and plunged almost straight into the water." The witness estimated the pitchup attitude of the airplane after it contacted the water at 65° to 70° and its nose-down attitude at 75° to 80° during the descent.
A Federal Aviation Administration (FAA) aviation safety inspector stated that reports of a low-flying airplane travelling along the beach from north to south were received from several towns north of Cape May. Witnesses reported that the airplane would dive to the surface, fly low along the beach, and climb again.
One witness forwarded a video of the airplane as it passed her position on Diamond Beach, about 5 miles, or about 2.5 minutes, north of the accident site. The airplane was near the shoreline, about 10 ft above the wave break, and the sound of the engine was smooth and continuous throughout. At one point, the airplane descended below the horizon line. About 20 seconds into the 30-second video, the airplane began a steep climb. The airplane was about 200 ft above the surface when the video ended.
State and local law enforcement attempted recovery of the pilot in the days following the accident but were hampered by the strong current, low visibility, and storms. On June 1, 2019, a commercial underwater salvage operator recovered the pilot along with the wreckage.
Pilot Information
Certificate: Commercial
Age: 58,Male
Airplane Rating(s): Single-engine land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Unknown
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: BasicMed Without waivers/limitations
Last FAA Medical Exam: September 20, 2018
Occupational Pilot: No
Last Flight Review or Equivalent:
Flight Time: 333 hours (Total, all aircraft), 17 hours (Total, this make and model), 6 hours (Last 30 days, all aircraft)
The owner/operator of the airplane stated that the pilot had "returned" to flying in October 2018. Training and rental records revealed that, since that time, the pilot had completed online FAA flight review training, received 17 hours of dual instruction, and had accrued 44.1 total hours of flight experience.
Aircraft and Owner/Operator Information
Aircraft Make: Mooney
Registration: N201DG
Model/Series: M20J No Series
Aircraft Category: Airplane
Year of Manufacture: 1977
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 24-0110
Landing Gear Type: Retractable - Tricycle
Seats: 4
Date/Type of Last Inspection: February 13, 2019 Annual
Certified Max Gross Wt.: 2899 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 5233.2 Hrs as of last inspection
Engine Manufacturer: Lycoming
ELT: Installed, not activated
Engine Model/Series: IO360-A3B6D
Registered Owner:
Rated Power: 200 Horsepower
Operator: On file
Operating Certificate(s) Held: Pilot school (141)
Meteorological Information and Flight Plan
Conditions at Accident Site: Visual (VMC)
Condition of Light: Day
Observation Facility, Elevation: KWWD,23 ft msl
Distance from Accident Site: 5 Nautical Miles
Observation Time: 10:56 Local
Direction from Accident Site: 18°
Lowest Cloud Condition: Clear
Visibility 10 miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 7 knots /
Turbulence Type Forecast/Actual: /
Wind Direction: 260°
Turbulence Severity Forecast/Actual: /
Altimeter Setting: 29.75 inches Hg
Temperature/Dew Point: 30°C / 20°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Robbinsville, NJ (N87)
Type of Flight Plan Filed: None
Destination: Robbinsville, NJ (N87)
Type of Clearance: None
Departure Time:
Type of Airspace: Class G
Wreckage and Impact Information
Crew Injuries: 1 Fatal
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 Fatal
Latitude, Longitude: 38.925556,-74.943054(est)
All major components of the airplane were recovered except for the left wing. The roof, left wing, and empennage were separated from the fuselage. The fracture surfaces displayed features consistent withoverload failure. Flight control continuity was confirmed from the cockpit area, through several breaks, to all available flight control surfaces. The fracture surfaces at the breaks displayed features consistent with overstress. The leading edge of the right wing was uniformly crushed aft along its entire span.
The engine was rotated by hand at the propeller and powertrain continuity was confirmed to the accessory section. Thumb compression was confirmed on all cylinders. Examination of the top spark plugs from each of the 4 cylinders revealed signatures consistent with normal wear and saltwater immersion. The single-drive dual magneto was destroyed by impact and saltwater immersion. The engine-driven fuel pump was removed, and when actuated by hand, pumped fluid from the output port. The fuel supply line was removed at the inlet port to the fuel manifold, where trace amounts of fuel were detected.
The propeller was attached at the hub, and all 3 blades displayed similar aft bending.
Medical and Pathological Information
The Office of the Chief State Medical Examiner, Woodbine, New Jersey, performed an autopsy on the pilot. The cause of death was listed as "blunt trauma of head, neck, trunk, and extremities," and the manner of death as "suicide."
The FAA Forensic Sciences Laboratory performed toxicological testing on the pilot. Ethanol was detected in concentrations and distribution consistent with postmortem production. No tested-for drugs were identified.
Photograph of Hudson Engineers real time scanning sonar showing the sonar tripod in the center, the diver at approximately 100 and the wreckage at approximately 3:00
Photograph of the sonar image of the aircraft on the sea floor.
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