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Accidents · NTSB WPR12FA059 · Final report

Amateur-built RV7 - A accident near Surprise, Arizona, December 10, 2011

On December 10, 2011 at about 7:58 pm local time, a 2006 amateur-built RV7 - A, registered N724WD, was substantially damaged in an accident during enroute (cruise) near Surprise, Arizona (Glendale Municipal airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

An electrical or engine electronic problem, which resulted in a loss of engine power, followed by a low-altitude stall.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
December 10, 2011 · about 7:58 pm local time
Place
Surprise, Arizona · Glendale Municipal · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built RV7 - A Donahoe, built 2006
Registration
N724WD · no longer on the register · serial 70742
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot, who was also the owner and builder, was flying his experimental amateur-built airplane powered by a converted automobile engine back to his home airport after a brief personal out-and-back flight. Light winds and daylight visual meteorological conditions prevailed. Radar and GPS data showed that the return portion of the flight followed an essentially straight track in the direction of the pilot's home airport at an altitude of about 1,500 feet above ground level with a groundspeed of about 100 knots. When the airplane was about 12 miles from the airport, the groundspeed decreased to about 60 knots over a period of about 25 seconds. The airplane then entered a descent of about 800 feet per minute, which it maintained for the next minute. Shortly after the start of that descent, the transponder was switched to the emergency code of 7700. About 25 seconds later, the pilot transmitted a "mayday" call to the approach controller. He stated that he had a problem, and several seconds later, transmitted that he was "going down." In the radio call, the pilot named the component that he thought was causing the problem, but the transmission quality prevented a positive determination of exactly what the pilot said. The descent rate then increased rapidly, and the airplane impacted terrain several seconds later. The damage to the rudder stop, rudder, elevator trim tab link, and elevator trim tab was inconclusive as to whether it occurred in flight or on impact. Propeller damage indicated that the propeller was not rotating or was rotating with little engine power. However, no preimpact mechanical problems with the engine, propeller gearbox, or propeller were identified. The reconstructed flight path was consistent with a significant deceleration at a near-constant altitude, followed by a descent to maintain flying speed, followed by a loss of control and/or aerodynamic stall at low altitude, from which the airplane did not recover. The airplane had slowed and started to descend when the pilot took the deliberate actions of squawking 7700 and transmitting a radio distress call. He attempted to describe the problem that he perceived. During that time, the data suggests that the airplane was still controllable and was under control. Shortly thereafter, as evidenced by the significantly increased descent rate and the pilot's transmission that he was going down, control was lost, and the airplane impacted the ground. The limited propeller damage, coupled with the engine's dependence on electricity and its electronics for continued operation, suggest that the deceleration could have been a result of an engine power loss for electrical or electronic reasons that could not be determined during postaccident examination. The specific reason for the stall could not be determined; however, the pilot may have been distracted by the emergency or the radio calls. The investigation was unable to determine the accuracy of the airspeed indicator or stall speed values. Further, the airplane does have a limited natural stall warning and no stall warning system to alert the pilot to an impending stall, particularly if he was distracted.

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 (total) during enroute (cruise) defining event
  2. Loss of control in flight during emergency descent

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Failure
  • factor Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 713 hours in all; 340 in this make and model
  • Last flight review: January 27, 2011
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 340 hours
  • Last inspection: condition inspection, July 15, 2011
  • Maximum gross weight: 1,800 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Subaru EJ-25 (piston); 340 hours total

The flight

  • Departed from: GEU Glendale AZ at 7:26 pm
  • Destination: GEU Glendale AZ
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 080° at 5 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 20,000 ft
  • Temperature: 66°F (19°C), dew point 19°F (-7°C)
  • Altimeter: 30.10 inHg
  • Observation at 7:47 pm from GEU, 9 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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.