CHI98LA102

NTSB accident investigation · Piper PA-32-260 · Mc Cordsville, IN · March 12, 1998

Accident · FatalLimited investigationFinal report
Date
March 12, 1998, 12:41 local (17:41 UTC)
Place
Mc Cordsville, IN
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N55059Piper PA-32-260
Weather
Visual (VMC) · Day
Status
Completed · report July 28, 1999
Report
Approved by Office Director
FAA report
19980312046379A
Case key
10835

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

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Probable cause

The pilot's failure to maintain airspeed and control of the airplane. Factors were his self-induced pressure.

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.

Loss of control - in flightManeuvering
Distance/speed - misjudgedPilot in commandCause
Self-induced pressurePilot in commandFactor
Aircraft control - not maintainedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

During a repositioning flight, the airplane departed controlled flight and impacted the terrain. No pre-existing anomalies were found during a post accident examination of the airplane and engine. A post mortem examination of the pilot and a toxicological examination of specimens from the pilot were negative. The pilot had an appointment at his office at 1300. The distance from the arrival airport to his office was 12.2 miles.

Factual narrative

On March 12, 1998, at 1241 eastern standard time, a Piper PA-32-260, N55059, operated by a private pilot suffered substantial damage during impact with the terrain while maneuvering for a landing on runway 18 (3,072' x 50' dry asphalt), at Brookside Airport, near McCordsville, Indiana. A Witness stated he observed the airplane enter a steep banked turn followed by a departure from controlled flight just prior to ground impact. The instrument rated private pilot sustained fatal injuries. The personal 14 CFR Part 91 flight was operating in visual meteorological conditions. No flight plan was on file. The flight originated at Mt Comfort, Indiana, about 1230.

On March 9, 1998, the accident airplane was parked by the owner/pilot at the Mount Comfort Airport after an Instrument Flight Rules (IFR) flight from Toledo, Ohio. Mount Comfort Airport is about four miles from the Brookside Airport, where the airplane was based. On the day of the accident the pilot of the accident airplane left his (dentist) office to reposition the airplane from Mount Comfort Airport to the Brookside Airport where the airplane was based.

The accident occurred at 1241. According to the "DeLorme Street Atlas." The distance by road from the airport to the pilot's office is 12.2 miles. The "Atlas" indicated the time to travel the shortest route between the airport and his office to be 23 minutes. The pilot had an appointment at his office scheduled for 1300.

A witness stated, "I saw the plane coming from the north. He was a little high in his approach, so he turned east, then he turned north. All of a sudden he started to tip with his wings facing one down and the other up. That's how he went into the ground nose first. He was heading west when he crashed."

The airplane came to rest 417 feet east of the runway and perpendicular to a point 702 feet south of the north end of the runway. Ground scars indicated that the airplane impacted the terrain in a nose low, left wing low attitude. The ground was frozen and the airplane came to rest in an open harvested cornfield.

Both engine and flight control continuity was established. The flaps were found in the full down (40 degree) position. The engine was examined for continuity. It was determined on rotation that there was continuity through the power section and accessory case. Thumb compression was found on all cylinders, and both magnetos sparked on rotation. The propeller, which remained attached to the propeller flange, had chordwise polishing and nicks present on the leading edge of the blades. The engine driven fuel pump was removed and pumped manually. The oil screen was clean. There were no pre-impact anomalies found in the engine or airframe.

The left front (pilot's position) shoulder harness was found frayed at the webbing and stowed (pushed into) a recess, in the vicinity of the inertia reel. The damage to the harness could not be associated with the accident in that the belt webbing displayed wrinkling that was consistent with long term storage in the inertia reel recess. Emergency responders said that the pilot was not restrained by the shoulder harness on their arrival at the accident scene.

An autopsy of the pilot was conducted on March 13, 1998, at the Indiana University School of Medicine. The post mortem examination of the pilot failed to reveal any pre-existing pathology or anomalies other than those associated with the accident.

A toxicological examination of specimens from the pilot was negative for those drugs screened.

The airplane was released to insurance representatives of the pilot/owner on March 25, 1998.

Parties to the investigation were the Federal Aviation Administration, Flight Standards District Office, Indianapolis, Indiana, and Lycoming Engine Company of Williamsport, Pennsylvania.

Aircraft

Registration
N55059
Reported as
Piper PA-32-260
Category
Airplane
Serial number
32-7300031
Airframe hours
6,430
Engine
Lycoming O-540-B4B5, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Scott J. Baldwin
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 18, 1997 · 142 hours before
Departed
MQJ · Mount Comfort, IN
Destination
I21
Airport
I21 · Brookside Airport, runway 18, 3,072 × 50 ft, asphalt

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
41
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
273 total · 198 in this make and model · 236 as pilot in command · 48 in the last 90 days · 30 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
280° at 8 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
23 °F, dew point 10 °F
Altimeter
30.00 inHg
Observed at
IND, 20 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.