Amateur-built M18 accident near Meridian, California, August 6, 2010
On August 6, 2010 at about 4:00 pm local time, a amateur-built M18, registered N70461, was substantially damaged in an accident during takeoff near Meridian, California (Sanborn Airport). It was an aerial application (crop spraying) flight under agricultural flying rules (Part 137). 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
Long-term deterioration of multiple engine fuel vaporizers that led to material failure of multiple turbine blades, which resulted in a complete loss of engine power. Contributing to the accident were the exceedance of specified engine inspection intervals and the unsuitable forced landing location.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 6, 2010 · about 4:00 pm local time
- Place
- Meridian, California · Sanborn Airport · map
- Type
- Accident
- Injuries
- 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built M18 UNDESIGNAT
- Registration
- N70461 · registry record · serial 1Z013-50
- Damage
- Substantial damage
- Flight
- Aerial application (crop spraying) flight · agricultural flying rules (Part 137)
The NTSB's narrative final · quoted from the NTSB record
The turboshaft-powered aerial application airplane had just departed the airstrip when the pilot/owner heard a loud "crack," and the engine stopped developing power. He executed a forced landing in a water-filled rice paddy adjacent to the airstrip. After touchdown, the airplane nosed over onto its back. The non-U.S. designed airplane was originally manufactured and delivered with a reciprocating engine. About 18 years before the accident, that engine was replaced with a U.S. military turboshaft engine via a Federal Aviation Administration (FAA) field approval. About 15 years after the engine change, and 3 years before the accident, the FAA mandated that piston-to-turbine engine conversions required the use of either an amended Type Certificate or a Supplemental Type Certificate, and that field approvals were no longer appropriate. Detailed examination of the engine revealed that most of the power turbine blades were severely damaged or missing. Material analysis of the turbine components revealed that the first stage turbine blades failed due to short-term exposure to excessively high temperatures and that other turbine blades failed due to impact damage from the thermally-failed first stage blades. The combustor was equipped with multiple fuel vaporizers, nearly all of which exhibited significant long-term thermal damage. None of the vaporizers were within the operable damage limits specified by the maintenance guidance. The damaged fuel vaporizers altered the combustor exit temperature profiles, which precipitated the first stage turbine blade failures. Maintenance records indicated that the 600-hour inspection interval of the engine hot section had been exceeded at least twice in the 14 years preceding the accident, and that, at the time of the accident, the engine had exceeded the hot section overhaul interval by about 300 hours. In-service records for the failed components could not be located. Although they did not contribute to the accident, multiple irregularities with the airplane's maintenance documentation were discovered during the investigation.
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 (total) during takeoff defining event
- Off-field or emergency landing during emergency descent
- Nose over/nose down during landing (landing roll)
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Combustion section › Not serviced/maintained
- cause Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Combustion section › Damaged/degraded
- cause Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Turbine section › Damaged/degraded
- factor Environmental issues › Physical environment › Runway/land/takeoff/taxi surfa › Soft › Contributed to outcome
- factor Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Combustion section › Not inspected
Pilot
- Certificate: commercial pilot
- Ratings: single-engine land; rotorcraft: helicopter
- Flight time: 20,610 hours in all; 205 in this make and model; 100 in the last 90 days; 60 in the last 30 days
- Last flight review: January 19, 2009
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: sngl
- Injury: minor injuries
The aircraft
- Airframe total time: 6,108 hours
- Last inspection: annual inspection, April 19, 2010; 140 hours since
- Maximum gross weight: 9,260 lb
- Seats: 1
- Landing gear: fixed
- Engine: Lycoming T53-L-7A (turboprop); 0 hours total
The flight
- Departed from: 38CN Meridian CA at 4:00 pm
- Destination: 38CN Meridian CA
- Flight plan: not recorded
Weather at the time
- Light: daylight
- Wind: from 180° at 4 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 64°F (18°C), dew point 54°F (12°C)
- Altimeter: 29.80 inHg
- Observation at 10:53 pm from MYV, 15 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
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.
