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January 13, 2001 · Mooney M20C · N1398W

Somerset, MA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 13, 2001
Injury Outcomes
1 injury (1 serious injury)
Location
Somerset, MA
Aircraft
Mooney M20C
Tail Number
N1398W
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
NYC01LA066

About 8 minutes before sunset, during a low level, northbound flight along a river, the airplane struck high tension cables. Upon cable impact, the airplane lost the vertical stabilizer and rudder, and the pilot was forced to land in the river. After touchdown, the airplane skidded into rocks along the shoreline.

NTSB Probable Cause

The pilot's inadequate visual lookout. A factor was the dusk lighting conditions.

Full Narrative

On January 13, 2001, about 1630 Eastern Standard Time, a Mooney M20C, N1398W, was substantially damaged when it impacted power transmission cables, then force-landed in the Taunton River, in Somerset, Massachusetts. The certificated private pilot was seriously injured. Visual meteorological conditions prevailed at the time of the accident. No flight plan had been filed for the local flight, which originated at Newport State Airport, Newport, Rhode Island. The personal flight was conducted under 14 CFR Part 91. According to a Federal Aviation Administration (FAA) inspector, the airplane was cruising northbound over the Taunton River, in an area that was urbanized on both sides. It passed over the Brada Bridge, then impacted one of two, eight-cable bundles of power transmission cables. The airplane continued northward, over the Brightman Street Bridge, then flew under another set of power cables, before being forced down in the river. After water touchdown, the airplane skidded into rocks along the river's western shoreline. In a later interview with the FAA inspector, the pilot stated that about 15 minutes after takeoff, he noticed that the engine was producing less power, and there was increased vibration. Just after passing the Brada Bridge and "just prior to reaching stall speed," the pilot applied carburetor heat. However, "owing to [a] reduced visibility at dusk, the approaching cable span was not observed in time.... After the cable strike, (approximately 10 seconds) the engine smartly picked up rpms, but by then, directional control of the aircraft was lost." On-scene examination revealed that one of the power cables in the southernmost bundle had been severed. The airplane's propeller had gouge marks on each of the two propeller blades, and both blade tips had been curled backwards. There was impact damage to both wings and the tail, and the cable impact "had clearly removed the rudder." Fuel samples were absent of water and debris, and the carburetor heat had been activated. The airplane's last annual inspection was completed on September 15, 1997. Weather, at airports approximately 15 nautical miles to the northeast and 12 nautical miles to the southwest, about 20 minutes after the accident, included clear skies, winds from the south at 4 to 5 knots, a temperature of 34 degrees Fahrenheit, and a dewpoint of 22 degrees Fahrenheit. Carburetor icing calculations indicated a probability of light icing during glide and while at cruise power settings. According to U.S. Naval Observatory data, sunset occurred at 1638.

Flight

Event TypeAccident
Event Time16:30 EST
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftMooney M20C
Tail NumberN1398W
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-360 · Reciprocating · 180
Seats4

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 54 · Third Class · Serious

Conditions

ConditionsVMC
LightDusk
Wind180° @ 4 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point34 C / 21 C
Altimeter30.29 inHg
Observation Time21:52
Weather SourceWFAC

Appendix: Source Data