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Accidents · NTSB WPR15LA251 · Final report

Dova Aircraft DV-1 accident near San Carlos, California, August 28, 2015

On August 28, 2015, a 2007 Dova Aircraft DV-1, registered N919E, was substantially damaged in an accident during initial climb near San Carlos, California (San Carlos airport). 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 partial loss of engine power due to fuel vapor lock. Contributing to the accident was the absence of a fuel return line.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
August 28, 2015 · cases in 2015
Place
San Carlos, California · San Carlos · cases near this airport · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Dova Aircraft DV-1, built 2007
Registration
N919E · registry record · serial 06/15
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The sport pilot had flown the special light-sport airplane to the airport earlier in the day and refueled. During his first departure attempt, the engine began to operate roughly, and he aborted the takeoff. After another departure attempt with the same results, he aborted the takeoff and taxied the airplane to a mechanic, who suggested that the airplane was experiencing vapor lock in the fuel system and that he let the engine cool down. The pilot waited and then performed an engine run-up, which appeared normal. He reattempted the departure, but the engine experienced a partial loss of power as the airplane began to climb through 50 to 75 ft. The pilot pitched the airplane down into a nose-low configuration and crashed into a field. Postaccident engine examination did not revealed any evidence of preimpact mechanical malfunctions or failures that would have precluded normal operation. Examination of the fuel system revealed that the airplane was not equipped with a mandatory fuel return line, although specified in the engine manufacturer's installation instructions. Manufacturer guidance indicated that the return line prevents malfunctions caused by the formation of vapor lock. A combination electronic flight instrument system and engine monitoring system was installed in the airplane, and the data was downloaded from the unit after the examination. The data showed that during the presumed accident takeoff, the fuel level in one tank was between 0 and .05 gallons and the other was at 10.4 gallons and decreasing. During this time, the fuel flow fluctuated between 1 and 7.1 pounds per square inch, which was consistent with the system containing air bubbles and, with the fuel system not being equipped with any way to vent that air, indicative that a vapor lock scenario was imminent. It is likely that the absence of the fuel return line resulted in the engine losing power due to vapor lock.

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 (partial) during initial climb defining event
  2. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

Pilot

  • Certificate: sport pilot
  • Flight time: 192 hours in all; 94 in this make and model; 8 in the last 90 days; 7 in the last 30 days; 130 as pilot in command
  • Last flight review: October 27, 2013
  • Medical certificate: Sport Pilot
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 330 hours
  • Last inspection: annual inspection, December 12, 2014; 5 hours since
  • Maximum gross weight: 1,320 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 912ULS (piston); 330 hours total

The flight

  • Departed from: SQL San Carlos CA
  • Destination: DVO Novato CA
  • Flight plan: none
  • Runway 30, 2,600 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 290° at 12 knots
  • Visibility: 10 statute miles
  • Sky: scat at 20,000 ft
  • Temperature: 86°F (30°C), dew point 41°F (5°C)
  • Altimeter: 29.97 inHg

Injuries

FatalSeriousMinorNone
Flight crew1

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

5 documents, released by the NTSB on December 6, 2018. 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.

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/WPR15LA251.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.