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Accidents · NTSB ERA24LA141 · Final report

Cirrus Design CORP SR22 accident near Winokur, Georgia, March 16, 2024

On March 16, 2024 at about 7:30 pm local time, a 2015 Cirrus Design CORP SR22, registered N469GB, was substantially damaged in an accident during enroute (climb to cruise) near Winokur, Georgia. It was a personal flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A total loss of engine power due to the unseating and subsequent failure of the No. 4 piston connection rod bushing.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
March 16, 2024 · about 7:30 pm local time
Place
Winokur, Georgia · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Cirrus Design CORP SR22, built 2015
Registration
N469GB · registry record · serial 4234
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

About 30 minutes into the flight, without warning, the airplane’s engine made a “loud noise” and stopped producing power. This was immediately followed by oil spraying onto the windscreen. Unable to divert to the closest airport due to distance and with no suitable places to land, the pilot deployed the whole airframe parachute system. The airplane came to rest between several trees and the airframe was substantially damaged. The pilot and passenger egressed the airplane without injury. Postaccident examination of the engine revealed a hole in the crown of the engine crankcase near the Nos. 3 and 4 cylinders. Further examination revealed the No. 4 piston connecting rod detached, with pieces found in the crankcase and oil sump. Additionally, the connecting rod bushings on all of the remaining piston connecting rods showed various signs of migration out of their respective locations; all bushings showed signs of chips and damage. Given these findings, it is likely that the bushings unseated themselves and migrated outward, resulting in imbalance, vibration, and the eventual failure of the No. 4 bushing and the subsequent total loss of engine power. A critical service bulletin (CSB) existed for the bushings that included augmented oil change procedures and inspections; however, the CSB was not adhered to, nor was it required to be due to the nature of the operation. The mechanic who had been maintaining the airplane assumed the procedures he was adhering to were sufficient, as they included routine oil changes at more frequent than recommended intervals, examination of the oil filter internal element, and having a laboratory analyze the engine’s used oil for the previous 14 months. The accident occurred 15 hours after the most recent oil change and the oil analysis report. Additionally, communications between the laboratory and mechanic, had indicated no substantive anomalies or other concerns indicating an imminent failure.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Loss of engine power (total) during enroute (climb to cruise) defining event

The NTSB's findings

  • Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Failure
  • Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Damaged/degraded
  • Aircraft › Aircraft oper/perf/capability › Aircraft capability › Climb capability › Attain/maintain not possible
  • Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Effect on equipment

Pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 1,119 hours in all; 405 in this make and model; 28 in the last 90 days; 8 in the last 30 days; 1,119 as pilot in command
  • Last flight review: November 9, 2023
  • Medical certificate: BasicMed (waiver time limited special)
  • Seat: left
  • Injury: no injuries

Passenger

  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 1,507 hours
  • Last inspection: annual inspection, November 8, 2023
  • Maximum gross weight: 3,600 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Continental IO-550 (piston); 1,507 hours total
  • Operator: Tta Holdings LLC

The flight

  • Departed from: SSI St. Simons GA at 7:00 pm
  • Destination: DBN Dublin GA

Weather at the time

  • Light: daylight
  • Wind: from 290° at 8 knots
  • Sky: clear
  • Temperature: 77°F (25°C), dew point 64°F (18°C)
  • Altimeter: 2996.00 inHg
  • Observation at 3:30 pm from AYS, 18 miles away

Weather report (METAR): METAR KAYS 161735Z AUTO 29008KT 10SM CLR 25/18 A2996 RMK AO2 T02490178=

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Photographs from the investigation 7 pictures from the NTSB's docket, as the NTSB released them

The NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.

Documents from the investigation the NTSB's docket: the evidence folder behind the report

9 documents, released by the NTSB on August 20, 2025. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.