ERA25LA043

NTSB accident investigation · Cessna 310K · Alcoa, TN · November 9, 2024

Accident · No injuriesClass 4 · LimitedFinal report
Date
November 9, 2024, 11:04 local (16:04 UTC)
Place
Alcoa, TN · Off runway
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Taxi
Aircraft
N143MGCessna 310K
Defining event
Taxi-from runway: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20241109017389A
Case key
195478

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 failure of the left engine throttle control shaft bushing during taxi, resulting in a full asymmetric power condition and a taxiway excursion.

Findings · 1

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.

Engine fuel and control: fuel control/carburetorAircraft › Aircraft power plant · Fatigue/wear/corrosionCessna 310K: 2 casesAll aircraft: 195 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 pilot reported that his approach and landing were normal. After exiting the runway, while on a taxiway, the airplane “swerved to the right and seemed to accelerate.” Unable to control braking and steering, the airplane departed the taxiway to the right and proceeded through a steep depression before colliding with a wind sensor pole. The pilot secured the airplane and was met by first responders. The airplane’s right wing and fuselage were substantially damaged during the accident sequence. Postaccident examination of the airplane revealed that the brass splined bushing on the left engine throttle control shaft was stripped, which resulted in an uncontrollable, full power application to that engine. The wheel brakes were examined and no anomalies were found; the brakes held the airplane in place with the left engine at full power during a test run.

Aircraft

Registration
N143MG
Reported as
Cessna 310K
Category
Airplane
Serial number
310K0134
Built
1965
Airframe hours
4,588
Engines
Cont Motor IO-470-VO(9), 260 horsepower, reciprocatingCont Motor IO-470-VO(8), 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 2, 2024
Departed
H10 · St Louis, MO
Destination
Same as departure
Flight plan
IFR
Airport
TYS · McGhee Tyson Airport, runway 5L, 10,000 × 150 ft, concrete
Equipment
Auto-pilot, Stall warning system, ADS-B

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
79
Injuries
None
Certificates
Flight instructor, Airline transport, Commercial, Private
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
February 15, 2024
Seat
Left
Restraint
Lap only
Flight hours
18,400 total · 4,000 in this make and model · 16,000 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
50° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
64 °F, dew point 50 °F
Altimeter
30.18 inHg
Observed at
TYS, 1 nm away
METAR
KTYS 091553Z 05006KT 10SM CLR 18/10 A3018 RMK AO2 SLP216 T01830094 $

Docket · 5

The files NTSB released with the investigation on April 22, 2025, on NTSB’s docket system: statements, records, photos and specialists’ reports. 19.9 MB 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.