ERA24LA141 · Cirrus Design Corp SR22
Tta Holdings Cirrus Design Corp SR22 · Accident: loss of engine power (total) en route
From St Simons Island Airport (SSI) to W H 'Bud' Barron Airport (DBN)
Narrative check · The NTSB narrative appears to contradict this record's location. Values are shown as recorded, not corrected; compare with the narrative.
Event
- NTSB case
- ERA24LA141
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- 0
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Cirrus Design Corp SR22
- Aircraft type
- Cirrus SR22
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N469GB
- Operator
- Tta Holdings
- Onboard fatalities
- Unknown
- Route
- From St Simons Island Airport (SSI), St. Simons, GATo W H 'Bud' Barron Airport (DBN), Dublin, GA
- Aircraft age
- About 9 years (built 2015)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · climb to cruise
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Loss of engine power (total)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft oper/perf/capability
- Aircraft › Aircraft power plant
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
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.
Probable cause
A total loss of engine power due to the unseating and subsequent failure of the No. 4 piston connection rod bushing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA24LA141
- Event ID
- 20240318193950
- Case number
- ERA24LA141
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, cause areas. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: cb2005d10570cb288b49e9bd0167f54d3b6e548e1727f9a2312aaf2bd36658a1; retrieved 2026-09-16T18:36:01.276Z.