CHI00LA082

NTSB accident investigation · Ellis Q2 · Shelbyville, IN · February 25, 2000

Accident · FatalLimited investigationFinal report
Date
February 25, 2000, 13:35 local (18:35 UTC)
Place
Shelbyville, IN
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N84DGEllis Q2
Weather
Visual (VMC) · Day
Status
Completed · report July 26, 2001
Report
Approved by Office Director
FAA report
20000225040639A
Case key
48755

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

aircraft control not being maintained by the pilot during the attempted go-around. Factors to the accident were the inadequate preflight by the pilot, which resulted in fuel exhaustion. An additional factor to the accident was the inadvertent stall/mush.

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 engine power(partial) - nonmechanicalGo-around (vfr)
Fluid,fuel - exhaustionFactor
Aircraft preflight - inadequatePilot in commandFactor
Loss of control - in flightDescent - emergency
Aircraft control - not maintainedPilot in commandCause
Stall/mush - inadvertentPilot in commandFactor
In flight collision with terrain/waterDescent - uncontrolled

Analysis

A witness to the accident reported that during an attempted go-around the airplane's engine was missing and running rough. The witness stated that the airplane entered a descending left turn, impacting the terrain in a 30-45 degree left bank. Post accident inspection of the airplane revealed that the main and header fuel tanks had ruptured, but no fuel spill or fuel odor was noted at the accident site. Witnesses/first responders to the accident site reported that there were no fuel odors around the accident site. Inspection of the engine failed to reveal any anomalies that could be associated with any preexisting condition. A fuel receipt was obtained for the accident airplane's last fueling. The date of the fuel receipt was listed as November 28, 1999, and 6.2 gallons of fuel were purchased for the accident airplane.

Factual narrative

On February 25, 2000, at 1335 eastern standard time (est), an Ellis Q2, N84DG, owned and piloted by an airline transport pilot, was destroyed during an in-flight collision with terrain following a loss of control during a go-around from runway 19 (5,000 feet by 100 feet, dry/asphalt) at the Shelbyville Municipal Airport, Shelbyville, Indiana. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR Part 91 and was not on a flight plan. The pilot, the sole occupant, was fatally injured. The local flight originated from the Shelbyville Municipal Airport approximately 20 minutes prior to the accident.

According to a pilot-rated witness, the airplane was on final approach for runway 19 when the airplane began a go-around. The witness described the engine operation, during the go-around, as "missing and running rough". The witness reported that the airplane entered a descending left turn, impacting the terrain in a 30-45 degree left bank.

Post accident inspection of the airplane revealed that the main and header fuel tanks had ruptured, but no fuel spill or fuel odor was noted at the accident site.

Witnesses/first responders to the accident site reported that there were no fuel odors around the accident site.

Inspection of the engine failed to reveal any anomalies that could be associated with any preexisting condition.

A fuel receipt was obtained for the accident airplane's last fueling. The date of the fuel receipt was listed as November 28, 1999, and 6.2 gallons of fuel were purchased for the accident airplane.

An autopsy was performed on the pilot on February 26, 2000, at the Indiana University School of Medicine, Indianapolis, Indiana.

The Federal Aviation Aeromedical Institute, Oklahoma City, Oklahoma, prepared a forensic toxicology report. The test results indicated that there was 0.011 (ug/ml, ug/g) Tetrahydrocannabinol (Marijuana) detected in lung tissue, and that Tetrahydrocannabinol Carboxylic Acid (Marijuana metabolite) was detected in blood and lung tissue.

Aircraft

Registration
N84DG
Reported as
Ellis Q2
Category
Airplane, amateur-built
Serial number
Q2461
Airframe hours
318
Engine
Revmaster 2100, 65 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Ora Merrill Proffitt
Airworthiness certificate
Special, Experimental (Special)
Departed
GEZ
Airport
GEZ · Shelbyville Municipal, runway 19, 5,000 × 100 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
71
Certificates
Airline transport, Commercial, Private
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
12,550 total

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 16 knots, gusting 21
Visibility
10 statute miles
Lowest ceiling
None
Temperature
162 °F, dew point 131 °F
Altimeter
30.00 inHg
Observed at
GEZ

FAA reports on this event · 1

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