CEN19LA222

NTSB accident investigation · Stinson 108 · Clinton, AR · July 13, 2019

Accident · Serious injuriesClass 3 · LimitedFinal report
Date
July 13, 2019, 11:20 local (16:20 UTC)
Place
Clinton, AR
Injuries
2 serious, 1 minor
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N9651KStinson 108
Defining event
Takeoff: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Central Region
Parties
FAA FSDO
FAA report
20190713011399A
Case key
99832

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

A partial loss of engine power for undetermined reasons.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Fluids: fuelAircraft › Fluids/misc hardware · Fluid conditionStinson 108-2: 1 caseAll aircraft: 1,695 cases
Engine (reciprocating)Aircraft › Aircraft power plant · Unknown/Not determinedStinson 108-2: 3 casesAll aircraft: 497 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The airplane had been stored in a hangar and not flown for 3 years. On the day of the accident, the pilot departed on a flight to a nearby airport, where he added 100 low-lead aviation fuel to the automotive fuel already contained in the wing tanks and subsequently departed on the return flight. About 150 ft above ground level after takeoff, the engine lost partial power. The airplane descended and impacted terrain, resulting in substantial damage to the left wing and fuselage. A fuel sample from the carburetor revealed some contamination; however, the contaminant was not identified. Although it is possible that the loss of engine power was the result of fuel contamination, the engine was not examined following the accident and a mechanical failure could not be ruled out; therefore, the reason for the partial loss of engine power could not be determined based on the available information.

Factual narrative

On July 13, 2019, about 1120 central daylight time, a Stinson 108 airplane, N9651K, was substantially damaged when it was involved in an accident near Clinton, Arkansas. The pilot sustained minor injuries, and the passengers were both seriously injured. The airplane operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to information obtained from a Federal Aviation Administration (FAA) inspector, the airplane had been stored in a hangar and not flown for about 3 years. The pilot checked the fuel and then departed for a nearby airport. After landing, the pilot estimated that the airplane’s left tank had 8 gallons of automotive fuel and the right wing had 16 gallons of automotive fuel. The age of the fuel could not be determined. The pilot added 12 gallons of 100 low-lead fuel to the left tank and 4 gallons to the right tank, and subsequently departed to the origin airport. During the initial climb after takeoff, when the airplane was about 150 ft above ground level, the pilot perceived that the airplane’s performance was reduced and recalled that the tachometer read 1,850 rpm, which was lower than expected. The airplane settled and the pilot flared the airplane before the collision with terrain to minimize impact forces. The airplane collided with the ground and came to rest against trees, resulting in substantial damage to the left wing and fuselage. The FAA inspector took a fuel sample from the carburetor and found contaminants in the fuel. When poured into a glass jar, several particles settled to the bottom of the jar. The fuel sample was not secured and was not available for further testing. The engine was not examined.

Aircraft

Registration
N9651K
Reported as
Stinson 108 (2)
Category
Airplane
Serial number
108-2651
Built
1947
Engine
Franklin 6A4165 SERIES, 165 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Departed
CCA · Clinton, AR
Destination
2A2 · Clinton, AR
Airport
CCA · Clinton Muni

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
66
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Unknown
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
2,000 ft overcast
Temperature
82 °F, dew point 73 °F
Altimeter
30.00 inHg
Observed at
KCCA
METAR
METAR KCCA 131535Z AUTO VRB04KT 10SM OVC020 28/23 A3000 RMK AO2=

Docket · 3

The files NTSB released with the investigation on February 2, 2022, on NTSB’s docket system: statements, records, photos and specialists’ reports. 979 KB in all.

FAA reports on this event · 1

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