Amateur-built RV7 - UNDESIGNAT accident near Belfair, Washington, February 10, 2015
On February 10, 2015 at about 9:30 pm local time, a 2011 amateur-built RV7 - UNDESIGNAT, registered N513BW, was substantially damaged in an accident during enroute (cruise) near Belfair, Washington. It was a personal flight under general aviation rules (Part 91). 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A total loss of engine power during cruise flight due to the fatigue failure of the engine crankshaft. Contributing to the accident was the unapproved repair and improper inspection of the engine crankshaft.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- February 10, 2015 · about 9:30 pm local time
- Place
- Belfair, Washington · map
- Type
- Accident
- Injuries
- 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built RV7 - UNDESIGNAT UNDESIGNAT, built 2011
- Registration
- N513BW · registry record · serial 70192
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot reported that the airplane was at 1,500 ft mean sea level as he was returning to the departure airport when the engine "abruptly quit." When all attempts to restart the engine failed, the pilot chose to land on a gravelly split. During the landing roll, the airplane's small tires sunk into the gravel, which resulted in the airplane nosing over. A postaccident examination of the engine revealed that the crankshaft had fractured adjacent to the aft radius of the No. 3 rod journal. Examination of the crankshaft revealed that it failed due to fatigue cracking that had initiated at locations on either side of a preexisting longitudinal crack. The radius also contained several circumferential cracks, including ones in the region corresponding to the relative location of the fatigue origins of the fracture. Examination also revealed that the No. 3 rod journal had been chromium-plated to regain lost material; however, according to the engine manufacturer, chromium plating on bearing journals was not an approved repair. Although the fatigue did not initiate in the plating, it did start near the edge of the replating in an area likely reworked (ground) following the unapproved plating. The multiple circumferential cracks noted in the radius likely resulted from the repair grinding and may have contributed to the fatigue initiation. A review of the engine logbooks revealed that the engine had been overhauled and subsequently inspected by the "magnaflux method" three times in a 14-month period about 15 years before the accident, during which the extensive cracking would have been present, indicating that the magnaflux inspections of the crankshaft were not effectively performed.
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 enroute (cruise) defining event
- Off-field or emergency landing during emergency descent
- Nose over/nose down during landing (landing roll)
The NTSB's findings
- cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Failure
- cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Incorrect service/maintenance
- factor Personnel issues › Task performance › Maintenance › Repair › Maintenance personnel
- Environmental issues › Physical environment › Terrain › Rough terrain › Contributed to outcome
Pilot
- Certificate: airline transport pilot, flight instructor
- Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 12,960 hours in all; 66 in this make and model; 207 in the last 90 days; 30 in the last 30 days; 3,887 as pilot in command; 75 on instruments
- Last flight review: September 7, 2014
- Medical certificate: Class 1 (with waivers/limitations)
- Seat: left
- Injury: minor injuries
The aircraft
- Airframe total time: 66 hours
- Last inspection: continuous airworthiness programme, January 22, 2015; 66 hours since
- Maximum gross weight: 1,800 lb
- Seats: 2
- Landing gear: fixed
- Engine: Lycoming IO-360 A1A (piston); 0 hours total
The flight
- Departed from: TIW Gig Harbor WA at 9:15 pm
- Destination: PWT Bremerton WA
- Flight plan: none
Weather at the time
- Light: dusk
- Wind: from 190° at 11 knots, gusting 16
- Visibility: 10 statute miles
- Sky: broken clouds at 2,600 ft
- Temperature: 54°F (12°C), dew point 46°F (8°C)
- Altimeter: 30.31 inHg
- Observation at 9:30 pm from PWT, 10 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.
