CHI94LA024

NTSB accident investigation · Piper PA-28-181 · Woonsocket, SD · October 26, 1993

Accident · FatalLimited investigationFinal report
Date
October 26, 1993, 09:50 local (14:50 UTC)
Place
Woonsocket, SD
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N39952Piper PA-28-181
Weather
Visual (VMC) · Day
Status
Completed · report July 25, 1994
Report
Approved by Office Director
FAA report
19931026040719A
Case key
9420

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

the pilot misjudging the airplane's clearance under the wires. Factors related to the accident were the performance of a low pass and the wires which were contacted.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

In flight collision with objectManeuvering
Object - wire,transmissionFactor
Low pass - performedPilot in commandFactor
Clearance - misjudgedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The airplane was observed flying low over farm fields approximately 1 1/2 miles southeast of the accident site. Witnesses driving along a four lane highway observed the airplane flying parallel, and over the highway. They observed the airplane fly low over another vehicle prior to colliding with powerlines crossing the road. The airplane collided with the ground and exploded into flames. The vehicle the airplane was flying low over was occupied by the pilot's friends.

Factual narrative

History of flight

On October 26, 1993, at 0950 central daylight time (CDT), a Piper PA-28-181, N39952, registered to the Fagerholt Brothers Farming Association of Hoople, North Dakota, and piloted by a private pilot, was destroyed when it collided with power lines and terrain. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 flight was not operating on a flight plan. The single occupant in the airplane was fatally injured. The flight departed Mitchell, South Dakota, at 0920 CDT.

N39952 departed Mitchell, South Dakota, with full fuel tanks. As the airplane was taxiing for takeoff, the pilot advised the unicom radio at the airport that he was departing Runway 30 and heading north toward Huron, South Dakota. A witness located approximately one mile east and one mile south of the accident site stated she observed the airplane flying at an altitude that a crop duster would fly at while traveling from field to field. She stated its wings were rocking.

Another witness driving on the four lane highway that N39952 crashed next to said he thought it was a low flying highway patrol airplane. This witness stated he estimated its altitude to be approximately 150 to 200 feet above the ground. Two occupants in a Chevrolet Suburban were acquainted with the pilot. These two individuals were driving north on the four lane highway when they observed the airplane pass over their vehicle in level flight. They stated N39952 passed overhead and collided with a wire crossing the highway. The witnesses said it was their impression that N39952's vertical stabilizer struck a wire before its descent to the ground.

Wreckage and impact information

The wreckage was located about 85 feet east of U.S. Highway 37, approximately 14 nautical miles south-southeast of the Huron Regional Airport, Huron, South Dakota. The airplane was at the north end of an irregularly shaped burned grass area measuring approximately 100' X 40'. The airplane was approximately 90 percent burned. The outer two-thirds of the right wing was found inverted and, along with the engine, survived the fire. The propeller remained attached to the engine. One blade was bent aft, approximately 80 degrees. This blade was gently curved forward outboard of the bend's origin point. The second blade was bowed forward; no other bending damage was observed on the propeller blade.

On December 8, 1993, N39952's engine was examined during disassembly. According to the Federal Aviation Administration's Principal Maintenance Inspector's report, "The tear-down revealed no indication of any engine malfunction or related accessory malfunction. The overall condition of the power plant was normal."

Medical and pathological information

The autopsy on the pilot was conducted by LCM Pathologists, P.C. of Sioux Falls, South Dakota. The Federal Aviation Administration's Civil Aeromedical Institute, located in Oklahoma City, Oklahoma, did the toxicological examination. The results of its examination were negative except 48.600 (ug/ml, ug/g) of acetaminophen was detected in the urine sample.

Aircraft

Registration
N39952
Reported as
Piper PA-28-181
Category
Airplane
Serial number
28-7990021
Engine
Lycoming O-360-A4M, 180 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Operator
Fagerholt Brothers Farming Asc
Registered owner
Fagerholt Brothers Farming Asc
Airworthiness certificate
Standard, Normal
Departed
MHE · Mitchell, SD
Destination
HON · Huron, SD

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Unknown
Seat
Left
Toxicology
Performed
Flight hours
934 total · 846 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 15 knots, gusting 21
Visibility
10 statute miles
Lowest ceiling
4,100 ft overcast
Temperature
39 °F, dew point 30 °F
Altimeter
30.00 inHg
Observed at
HON, 15 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.