N2601Q

Substantial
Fatal

Cessna 182S/N: 18257801

Accident Details

Date
Tuesday, September 22, 2020
NTSB Number
ERA20LA329
Location
Lincolnton, GA
Event ID
20200922X91109
Coordinates
33.769581, -82.454462
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's loss of airplane control while maneuvering at a low altitude.

Aircraft Information

Registration
N2601Q
Make
CESSNA
Serial Number
18257801
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
182C182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MATTISON COLEN FLOYD
Address
PO BOX 714
Status
Deregistered
City
LINCOLNTON
State / Zip Code
GA 30817-0714
Country
United States

Analysis

On September 22, 2020, at 1712 eastern daylight time, a Cessna 182 airplane, N2601Q, was substantially damaged when it was involved in an accident in Lincolnton, Georgia. The private pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

A review of Federal Aviation Administration (FAA) tracking data revealed that the pilot departed Cherokee County Regional Airport (CNI), Canton, Georgia, about 1530. He flew to Barrow County Regional Airport (WDR) Winder, Georgia, and remained there for about 30 minutes. He then departed for his home airport, a private field in Lincolnton, Georgia, at 1638.

About 1710, the airplane approached a field and pond located on land owned by the pilot’s family, about 3 miles south of the private airport. A witness who was mowing the grass surrounding the pond reported that the airplane flew “low” toward him and then over the pond in the pilot’s “standard ‘I’m home’ fly by.”  Another witness, who was also mowing around the pond, reported that the airplane “buzzed the pond” at an altitude less than 60 ft above the ground. The airplane then “pulled up to normal flying altitude” and circled in a left turn before it approached the pond a second time. The witness estimated that, as the airplane approached the pond, its altitude was less than 50 ft above the ground. At one point, the airplane flew between two groups of trees with its right wing pointing “almost straight up in the air.” The airplane impacted the ground at the edge of the pond, and briefly became airborne again before it impacted the water and came to rest partially submerged. The second witness did not observe the impact due to trees obstructing his view; however, he reported that the sound of the engine was “steady” until he heard a “thump” followed by a “shoosh,” which he surmised was the impact with the ground and then the water.

The FAA tracking data revealed that the airplane approached the area of the pond from the west at a recorded pressure altitude of 500 ft (the field elevation in the area varied from 400 to 500 ft above mean sea level). After passing the pond, the airplane turned left about 270° before the recorded data ended when the airplane was about 0.1 nautical mile northwest of the pond. During the first half of the turn, the airplane climbed to an altitude of 1,000 ft and then descended to 500 ft at the last data point.

Examination of the accident site by two FAA inspectors revealed that the airplane sustained severe impact and crush damage forward of the empennage. Both wings were separated from the fuselage and sustained leading edge damage. The engine remained attached to the fuselage. The propeller assembly (both blades and hub) was separated from the flange. One propeller blade was twisted and bent about mid-span, the other blade was slightly bent near the root and slightly twisted near the tip.

A follow-up examination of the wreckage revealed that the flaps were retracted, and the elevator trim tab was found deflected about 5° trailing edge up (airplane nose down). Flight control continuity was confirmed from the cockpit controls to the control surfaces through cable separations that were consistent with either cuts made by recovery personnel or tension overload. The engine was impact-damaged, and the starter, magnetos, intake, and exhaust components were all separated from the engine and missing. Rust was found inside the cylinders, which precluded manual rotation of the engine crankshaft.

FAA Forensic Sciences Laboratory toxicology testing detected the antidepressant citalopram in the pilot’s liver tissue and its active metabolite, n-desmethylcitalopram, in his cavity blood and liver tissue. Although citalopram carries a warning that its use may impair mental or physical ability for performing hazardous tasks, it is an FAA-approved antidepressant medication with a special issuance medical certificate. The allergy medication cetirizine was detected in the pilot’s cavity blood and liver tissue but was not quantified. Certirizine can have sedating effects, and the FAA provides guidance on wait times before flying after taking this medication. The nonimpairing gastroesophageal reflux medicine pantoprazole (commonly marketed as Protonix) was detected in his cavity blood.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA20LA329