Loss of control Accident Velocity STD/RG-E N112TH,
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ASN Wikibase Occurrence # 173796
 
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Date:Friday 13 February 2015
Time:09:00
Type:Silhouette image of generic VELO model; specific model in this crash may look slightly different    
Velocity STD/RG-E
Owner/operator:Private
Registration: N112TH
MSN: SRE042
Year of manufacture:2007
Total airframe hrs:79 hours
Engine model:Superior IO-360
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Sebastian Municipal Airport (X26), Sebastion, FL -   United States of America
Phase: Take off
Nature:Private
Departure airport:Sebastian, FL (X26)
Destination airport:Whiteville, NC (CPC)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot had recently purchased the experimental, amateur-built airplane. He received 3.6 hours of familiarization training in another airplane by the same manufacturer during the 2 days before the accident while maintenance and inspections were performed on his airplane. Once the work was completed, the pilot departed on the accident flight. Witnesses reported that, immediately after rotation, they observed the right cabin door open. The airplane briefly maintained the runway heading and then began a “slow, lingering” left turn. One witness described the engine sound as increasing and decreasing between idle and full power. The airplane rolled left, then wings level, then left again before it descended to the ground. The airplane impacted trees near the airport perimeter; the right wing separated, and the fuselage was substantially damaged. Immediately after the accident, the pilot reported that he was taking off and that “the door blew open.” The pilot subsequently reported that the airplane “pitched up violently” on takeoff and would not respond to nose-down pitch trim.
Examination of the airplane revealed flight control continuity from the cockpit area to the flight control surfaces. The latch mechanism on the right cabin door was found intact and fully functional. The pitch trim was found in a nearly full nose-up setting, and, when activated, the pitch trim motor ran through its full range at its normal rate. The pilot reported that there were no mechanical deficiencies with the airplane that would have precluded normal operation.

Probable Cause: The pilot’s loss of airplane control after takeoff, which resulted in collision with terrain. Contributing to the accident was the pilot’s failure to properly secure the cabin door and trim the airplane for takeoff, which resulted in the cabin door opening and the nose pitching up suddenly at liftoff.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA15LA130
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=112TH

History of this aircraft

Other occurrences involving this aircraft
9 September 2010 N112TH Private 0 Wooster, Ohio sub
Fuel exhaustion

Location

Revision history:

Date/timeContributorUpdates
13-Feb-2015 15:51 gerard57 Added
13-Feb-2015 16:35 Geno Updated [Time, Aircraft type, Location, Phase, Departure airport, Source, Narrative]
14-Feb-2015 17:38 Geno Updated [Aircraft type, Registration, Cn, Source, Narrative]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
01-Dec-2017 12:34 ASN Update Bot Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]

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