Mooney Aircraft CORP. M20 accident near Lakeway, Texas, February 12, 2023
On February 12, 2023 at about 3:58 pm local time, a 1997 Mooney Aircraft CORP. M20, registered N304MA, was substantially damaged in an accident during approach (VFR pattern downwind) near Lakeway, Texas. It was a personal flight under general aviation rules (Part 91). No one was hurt; 1 person was 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 detonation and preignition in the No. 6 cylinder.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- February 12, 2023 · about 3:58 pm local time
- Place
- Lakeway, Texas · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Mooney Aircraft CORP. M20 K, built 1997
- Registration
- N304MA · registry record · serial 25-2004
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
Before purchasing the airplane, the pilot had an inspection performed. One of the findings on the inspection stated that, “spark plugs are worn past limits.” There were no indications that the magneto timing was checked during the inspection. The pilot reported that the airplane had been run with a lean mixture in the past. After the pilot purchased the airplane, he flew the airplane on a cross-country flight to relocate it to his home base. While in flight, the engine had a low manifold pressure reading and then the engine sustained a total loss of power. The pilot attempted to fly to the nearest airport, but instead performed a forced landing to a golf course. During the forced landing sequence, the airplane impacted trees and a wood fence, and came to rest near a diesel generator. The airplane sustained substantial damage to the fuselage and to both wings. Examination of the airframe revealed no mechanical anomalies. Examination of the engine revealed a hole in the corner of the No. 6 piston; however, the No. 6 cylinder was intact. The No. 6 piston had eroded crown material and a darkened periphery. The engine case was found intact. The top spark plugs from the Nos. 3, 5, and 6 cylinders and the bottom spark plugs from the Nos. 3 and 5 cylinders were found in a “worn out - normal condition.” The right magneto timing was found at 22°, when it is supposed to be at 20°. The left magneto timing was found at 15°, when it is supposed to be at 20°. The oil breather tube was found intact, and the slot was not blocked. Engine oil was found splattered in and around the oil breather tube area, including traveling rearward on the area underneath the oil breather tube. No anomalies were noted with the turbocharger system or the propeller. It is likely a total loss of engine power occurred when the No. 6 piston developed a hole from burn through, consistent with detonation and preignition signatures consisting of combustion deposits and excessive temperature exposure. The hole in the piston likely allowed exhaust gases, caused by the detonation and preignition, to force engine oil out of the oil breather tube. The combination of the engine being previously run with a lean mixture, worn spark plugs, and incorrect magneto timing, likely lead to the preignition and detonation and a subsequent total loss of engine power.
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
- Loss of engine power (partial) during enroute
- Loss of engine power (total) during approach (VFR pattern downwind) defining event
- Attempted remediation/recovery during enroute
- Attempted remediation/recovery during approach (VFR pattern downwind)
- Off-field or emergency landing during approach (VFR pattern final)
- Evacuation during post (impact)
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Failure
- Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Incorrect use/operation
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: helicopter; instructor: instrument helicopter; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
- Flight time: 5,377.8 hours in all; 7 in this make and model; 27.1 in the last 90 days; 12.7 in the last 30 days; 3,337.5 as pilot in command; 2,898.3 on instruments
- Last flight review: April 14, 2022
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 2,763.7 hours
- Last inspection: annual inspection, October 8, 2022; 31.3 hours since
- Maximum gross weight: 3,130 lb
- Seats: 4
- Landing gear: retractable
- Engine: Continental Motors TSIO-360-MB (piston); 2,763 hours total
The flight
- Departed from: 1T7 Spring Branch TX at 3:32 pm
- Destination: CKV Clarksville TN
- Flight plan: VFR
Weather at the time
- Light: daylight
- Wind: from 250° at 4 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 46°F (8°C), dew point 32°F (0°C)
- Altimeter: 30.21 inHg
- Observation at 9:55 am from KRYW, 8 miles away
Weather report (METAR): KRYW 121555Z AUTO 25004KT 10SM CLR 08/00 A3021 RMK AO2 T00821003
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
22 documents, released by the NTSB on September 11, 2024. 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.
