BFO93FA128

NTSB accident investigation · Taylorcraft BC12-65 · Danbury, CT · July 18, 1993

Accident · FatalField investigationFinal report
Date
July 18, 1993, 15:15 local (19:15 UTC)
Place
Danbury, CT
Injuries
1 fatal, 1 serious
Damage
Destroyed
Phase of flight
Approach
Aircraft
N34009Taylorcraft BC12-65
Weather
Visual (VMC) · Day
Status
Completed · report September 27, 1994
Report
Approved by Office Director
FAA report
19930718024169A
Case key
8752

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

Undetermined.

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 objectApproach - vfr pattern - downwind
Reason for occurrence undeterminedCause
Terrain condition - mountainous/hilly
Object - tree(s)

Analysis

The pilot reported that he was going to remain in the traffic pattern for the flight. He was cleared for takeoff from runway 26, and to report when he was on the downwind leg. No transmissions were received from the pilot after takeoff. The wreckage was located in mountainous terrain below the traffic pattern where an airplane might turn from the crosswind leg to the downwind leg of the pattern. An airplane altitude at that location is about 400 ft above the terrain. The toxicology report indicated that the drugs fluoxetine and norfluoxetine were detected in the pilot's system. The pilot's personal medical records showed that the pilot was prescribed the drug prozac for treatment of mild depression.

Factual narrative

History of flight

On Sunday, July 18, 1993, at 1515 eastern daylight time, a Taylorcraft BC12, N34009, owned and operated by the pilot, collided with trees after turning onto the downwind leg of the Danbury Airport runway 26 traffic pattern. The pilot was fatally injured. The passenger received serious injuries. The airplane was destroyed. Visual meteorological conditions prevailed at the time of the accident. The local personal flight was conducted under 14 CFR Part 91.

According to the official transcription of the Danbury Air Traffic Control tapes, the pilot stated that he was going to remain in the airport traffic pattern for the flight. The tapes revealed that the pilot was cleared for takeoff from runway 26 and was to report when he was on the downwind leg of the pattern. The local air traffic controller received no transmissions from the pilot after takeoff, and stated that he saw the airplane turn onto the crosswind leg of the pattern at about 1,200 feet mean sea level. The local controller stated that when the pilot did not report that he had turned onto the downwind leg, he queried the pilot on the airplane's location. There were no transmissions received from the pilot.

The airplane wreckage was located in mountainous terrain below the traffic pattern where an airplane might turn from the crosswind leg to the downwind leg of the pattern. The airplane struck trees and came to rest on the left side of the engine on sloping, wooded terrain, at an elevation of about 1,200 feet mean sea level.

According to the Danbury Airport Manager, Mr. P. Estefan, the airport's traffic pattern was 1,700 feet mean sea level. Mr. Estefan stated that when the airplane is turned from the crosswind leg to the downwind leg in a standard left hand pattern for runway 26, the airplane's altitude at that location is about 400 feet above the terrain.

The passenger stated that he does not remember the accident, but does remember the flight. He stated that he did not hear anything "unusual" and was looking out the right window for most of the flight. (See attached Record of Interviews for more details.)

The accident occurred during the hours of daylight at 41 degrees 21.1 minutes North latitude and 73 degrees 29.7 minutes West longitude.

Personnel information

The pilot held a Federal Aviation Administration airline transport pilot certificate. According to the pilot's log book and a family member, at the time of the accident, the pilot had accumulated about 3,557 total flight hours, of which about 10 were in a Taylorcraft.

The pilot purchased N34009 on June 9, 1993. According to the previous owner, the pilot and he had flown N34009 on December 6, 1992, for about one and one half hours. The previous owner stated that the flight was local (Milford, Michigan) and "...no performance maneuvers/stalls were performed."

Wreckage and impact information

The airplane wreckage was examined at the accident site on July 19, 1993. The examination of the airframe and engine did not disclose any anomalies.

The airplane came to rest on the left side of the airplane's engine on sloping, wooded terrain, about 10 feet beyond two broken trees. One tree top was separated from the tree and had gash marks of similar size and shapes down its side.

The left wing was bent up 90 degrees from its horizontal position. The wood left wing spar and metal lift attachment were broken at the wing root and the wing strut attachment truss was separated at the fuselage. Metallurgical analysis of the wing strut attachment truss and the wing spar lift attachment was accomplished at the National Transportation Safety Board's Materials Laboratory. Examination of the fracture surfaces with the aid of a bench binocular microscope disclosed only overstress features. (See attached Metallurgist's Factual Report for details.)

The right wing was attached to the fuselage and the wing strut was bent up into the wing. The right wing leading edge had crush marks. Tree bark and green marks were found in the crushed areas. Aileron control continuity was verified throughout the aileron system.

The rudder was in the full nose left position and had traveled beyond the rudder stop. The rudder control cable on the right side was broken at the connector fitting. Microscopic examination of the fractured surface disclosed only overstress features.

The wooden propeller blades were splintered and pieces of the propeller blades were around the accident site.

The engine was examined and continuity was verified. The number four cylinder was cracked and compression in that cylinder could not be verified. The right magneto had a bent armature shaft. No other anomalies were noted.

Medical and pathological information

The autopsy was performed by Dr. Kanfer at the Office of the Medical Examiner, State of Connecticut, located in Farmington, Connecticut. The autopsy revealed no evidence of physical incapacitation or impairment.

The toxicology was performed by Dr. Canfield at the Civil Aeromedical Institute in Oklahoma City, Oklahoma. Negative results were reported for all screened volatiles. The drugs fluoxetine and norfluoxetine were detected in the urine and blood. (See attached National Transportation Safety Board Memorandum for toxicology interpretation.)

An excerpt from the 45th Edition 1991 Physicians' Desk Reference states, "Prozac (fluoxetine hydrochloride) is indicated for the treatment of depression. A major depressive episode implies a prominent and relatively persistent depressed or dysphoric mood that usually interferes with daily functioning. Some general precautions listed for this drug are anxiety, insomnia, altered appetite and weight, activation of mania/hypomania, seizures, and suicide."

Federal Aviation Administration records indicated the pilot was issued a first class medical certificate on January 25, 1993. Review of the pilot's last application for an airmen medical certificate, dated January 25, 1993, showed that he did not disclose the fact that he was being treated, and taking medication, for any disorder. The pilot's personal medical records disclosed that he was first prescribed the drug Prozac on November 12, 1992.

Additional information

The airplane was released to Trudi Bresner of Waccabuc, New York, on September 13, 1993.

Aircraft

Registration
N34009
Reported as
Taylorcraft BC12-65
Category
Airplane
Serial number
2860
Airframe hours
781
Engine
Continental A-75-8, 75 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Raymond A. Walsh
Registered owner
Raymond A. Walsh
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 13, 1993 · 7 hours before
Airport
DXR · Danbury Muni, runway 26, 4,425 × 150 ft

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
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
3,561 total · 13 in this make and model · 1,787 as pilot in command · 13 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
280° at 6 knots
Visibility
20 statute miles
Lowest ceiling
25,000 ft broken
Temperature
84 °F, dew point 52 °F
Altimeter
30.00 inHg
Observed at
DXR, 1 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.