Accident Diamond DA40F Diamond Star N419FP,
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ASN Wikibase Occurrence # 188745
 
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Date:Monday 18 July 2016
Time:11:05
Type:Silhouette image of generic DA40 model; specific model in this crash may look slightly different    
Diamond DA40F Diamond Star
Owner/operator:Utah State University
Registration: N419FP
MSN: 40.FC019
Year of manufacture:2006
Total airframe hrs:6201 hours
Engine model:Lycoming O-360-A4M
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Destroyed
Category:Accident
Location:Cache County near Hyrum, between Mount Sterling -   United States of America
Phase: En route
Nature:Private
Departure airport:Logan, UT (LGU)
Destination airport:Logan, UT (LGU)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The private pilot was practicing flight maneuvers required to obtain a commercial pilot certificate during daytime visual flight rules weather conditions. A witness saw the airplane flying in slow counterclockwise circles while descending with the engine power at idle. He reported strong gusting winds at the time. Radar data showed the airplane completing four counterclockwise orbits and then beginning a descending clockwise orbit. The last two data points indicate a rapid, vertical descent greater than 6,000 ft per minute. Wreckage and impact signatures revealed that the airplane impacted the ground in a nose-low, near-vertical attitude with little to no forward movement, consistent with an aerodynamic stall/spin. Examination of the airframe and engine found no abnormalities that would have precluded normal operation.

Weather conditions in the accident area included strong gusty winds, low-level wind shear, clear air turbulence near the terrain, and possible mountain wave activity at mountain top level. The weather information that the pilot obtained before departure indicated wind at 6 knots and no gusts. No records were located to indicate that the pilot had obtained an official weather briefing before departure, thus he may not have been aware of the gusting winds and the potential for low-level wind shear and turbulence which could have contributed to his failure to maintain aircraft control. The radar data, the witness's description, and the damage to the airplane are consistent with the pilot exceeding the airplane's critical angle of attack while maneuvering, resulting in the airplane entering an aerodynamic stall with a subsequent spin and descent to ground impact.

Probable Cause: The pilot's exceedance of the airplane's critical angle of attack while maneuvering in turbulence and gusty wind conditions, which resulted in an aerodynamic stall/spin.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR16FA144
Status: Investigation completed
Duration: 1 year and 8 months
Download report: Final report

Sources:

NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N419FP

Location

Images:


Photo: NTSB

Revision history:

Date/timeContributorUpdates
18-Jul-2016 22:38 Geno Added
19-Jul-2016 13:52 Geno Updated [Registration, Cn, Source, Damage]
04-Mar-2018 17:30 Anon. Updated [Narrative]
15-Mar-2018 20:12 ASN Update Bot Updated [Time, Location, Nature, Departure airport, Destination airport, Source, Damage, Narrative]
15-Mar-2018 20:38 harro Updated [Source, Narrative, Photo, ]

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