CHI95DTK01

NTSB accident investigation · Gay RV-4 · Lennox, SD · January 8, 1995

Accident · FatalFinal report
Date
January 8, 1995, 16:00 local (22:00 UTC)
Place
Lennox, SD
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N29PGGay RV-4
Weather
Visual (VMC) · Day
Status
Completed · report January 19, 1996
Report
Approved by Office Director
FAA report
19950108000189A
Case key
9712

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 adequate altitude while performing aerobatic maneuvers. The pilot's impairment of judgment and performance due to drugs was a factor.

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 terrain/waterManeuvering
Aerobatics - performedPilot in command
Altitude - inadequatePilot in commandCause
Impairment(drugs)Pilot in commandFactor
Use of inappropriate medication/drugPilot in command

Analysis

A witness reported that the airplane was flying low altitude aerobatic maneuvers in the vicinity of the accident site. Radar tracking data, available above an altitude of approx 800 ft AGL, also shows a VFR target conducting low altitude aerobatic maneuvers. Examination of the wreckage revealed no evidence of preimpact aircraft or engine malfunction. The airplane had come to rest 132 ft from the first impact with the ground. Toxicological tests revealed 0.031 ug/ml brompheniramine and 0.012 ug/ml diphenhydramine in the blood specimen. Therapeutic levels are 0.016-0.070 and 0.100 respectively. Brompheniramine and diphenhydramine (antihistamines) are active ingredients in many nonprescription cold and allergy medications, and can cause drowsiness.

Factual narrative

History of flight

On January 8, 1995, about 1600 central standard time, a Gay RV-4 airplane, N29PG, was destroyed when it impacted the terrain while maneuvering near Lennox, South Dakota. The solo private pilot sustained fatal injuries. The personal flight originated in Sioux Falls, South Dakota at 1537 and was conducted under 14 CFR Part 91. The planned destination was Lennox, South Dakota. A flight plan was not filed and visual meteorological conditions prevailed.

During a personal interview on January 11, 1995, a witness stated that between 1555 and 1600, she observed a blue and white airplane heading south. It climbed, did a spiral turn, and then came back down heading north "at a lower altitude than most airplanes fly."

Radar tracking data provided by the Minneapolis Air Route Tracking Control Center shows the airplane departed southbound from Sioux Falls at 1537. The target maneuvered in a series of aerobatic maneuvers in the vicinity of the accident site. Radar coverage was available down to an altitude of approximately 2,100 feet MSL. The elevation of the accident site was approximately 1,300 feet MSL.

Wreckage and impact information

Post accident examination revealed compression of the lower nose and right wing. Both elevator counterweights and the right aileron were separated. The weighted leading edge of both ailerons were distorted. The wreckage path followed a heading of 085 degrees with a distance of 105 feet between the first two ground scars. The aircraft came to rest 132 feet from the first impact on a heading of 187 degrees.

All of the prop bolts were sheared off at the inboard end of the propeller extension. The outboard face and leading edge of both propeller blades exhibited rotational damage. The right main wheel assembly was torn off its attachment point. Both wheel bearings and the wheel retaining nut were intact on the strut. The main wing spar below and to the right of the pilots seat was distorted.

All of the flight control surfaces and flight controls were intact and operational. No evidence of preimpact malfunction was discovered.

Inspection of the engine revealed the left magneto impulse coupling operated normally. Spark from all leads was confirmed on both magnetos. The carburetor was separated in an aft direction, however, remained attached to its linkages. The inlet fuel fitting was broken. Fuel was found in the fuel line from the firewall to the engine driven fuel pump. All spark plugs were normal. There was no evidence of an engine malfunction prior to impact.

Medical and pathological information

Autopsy of the pilot was conducted on January 1, 1995, by LCM Pathologists, P.C., 1212 S. Euclid Ave., Sioux Falls, South Dakota. The results of FAA toxicological testing were negative for all tests conducted except for 0.031 (ug/ml, ug/g) Brompheniramine and 0.012 (ug/ml, ug/g) Diphenhydramine detected in the blood specimen. Brompheniramine and Diphenhydramine were detected in the urine specimen.

According to a NTSB National Resource Specialist, the therapeutic level for Diphenhydramine is approximately .100 (ug/ml, ug/g) and the therapeutic level for Brompheniramine is .016 to .070 (ug/ml, ug/g). Brompheniramine and Diphenhydramine are listed in the Physicians' Desk Reference as active ingredients in many nonprescription cold and allergy medications.

Aircraft

Registration
N29PG
Reported as
Gay RV-4
Category
Airplane, amateur-built
Serial number
1605
Airframe hours
749
Engine
Lycoming O-320-E2G, 150 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Kevin M. Falon
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · May 14, 1994 · 158 hours before
Departed
FSD · Sioux Falls, 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
43
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
914 total · 113 in this make and model · 914 as pilot in command · 23 in the last 90 days · 7 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 3 knots
Visibility
12 statute miles
Lowest ceiling
6,500 ft broken
Temperature
7 °F, dew point 1 °F
Altimeter
30.00 inHg
Observed at
FSD, 18 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.