Loss of control Accident Van's RV-7A N724WD,
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ASN Wikibase Occurrence # 140359
 
This record has been locked for editing.

Date:Saturday 10 December 2011
Time:12:58
Type:Silhouette image of generic RV7 model; specific model in this crash may look slightly different    
Van's RV-7A
Owner/operator:Private
Registration: N724WD
MSN: 70742
Year of manufacture:2006
Total airframe hrs:340 hours
Engine model:Subaru EJ-25
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Surprise, AZ -   United States of America
Phase: En route
Nature:Private
Departure airport:Glendale, AZ (GEU)
Destination airport:Glendale, AZ (GEU)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
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.

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


Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR12FA059
Status: Investigation completed
Duration: 2 years and 6 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
10-Dec-2011 15:44 RobertMB Added
10-Dec-2011 18:09 RobertMB Updated [Aircraft type, Registration, Cn, Source]
18-Dec-2011 22:24 Geno Updated [Time, Aircraft type, Departure airport, Destination airport, Source]
29-Aug-2016 06:45 junior sjc Updated [Aircraft type, Narrative]
03-Sep-2016 19:47 junior sjc Updated [Source]
04-Sep-2016 07:11 junior sjc Updated [Narrative]
21-Dec-2016 19:26 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
18-Oct-2017 10:02 junior sjc Updated [Location, Nature, Destination airport, Source]
27-Nov-2017 17:38 ASN Update Bot Updated [Aircraft type, Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative]

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