Loss of control Accident Avid Flyer N430WT,
ASN logo
ASN Wikibase Occurrence # 189057
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Tuesday 2 August 2016
Time:20:45
Type:Silhouette image of generic AVID model; specific model in this crash may look slightly different    
Avid Flyer
Owner/operator:Private
Registration: N430WT
MSN: 145
Year of manufacture:1984
Total airframe hrs:249 hours
Engine model:Bombardier 532 UL
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Near Miller Airport (C40), Bluffton, IN -   United States of America
Phase: Take off
Nature:Private
Departure airport:Bluffton, IN (C40)
Destination airport:Bluffton, IN (C40)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The student pilot was operating a personal, local flight in the nonregistered, experimental amateur-built airplane with one passenger onboard. The student stated that, while the airplane was climbing through 500 ft above ground level after takeoff, there was an uncommanded left roll. He reported that the airspeed was 60 knots (which is above the stall speed of 40 mph listed in the airplane’s specifications). He applied right control input to the control stick, which did not counter the left roll. The airplane entered a left spiral descent, and the pilot pulled back on the control stick and applied right rudder until the airplane impacted terrain. He reported that the airplane’s engine was at full throttle during the flight and that it did not experience a loss of engine power.
A postaccident examination of the airframe, including the flight controls, revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The investigation could not determine the reason for the loss of roll control.

Probable Cause: The loss of roll control during climb for reasons that could not be determined because postaccident examination of the airframe revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN16LA300
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=430WT

Location

Revision history:

Date/timeContributorUpdates
04-Aug-2016 00:23 Geno Added
04-Aug-2016 04:54 Geno Updated [Aircraft type, Registration, Cn, Operator, Source, Damage, Narrative]
19-Aug-2017 14:56 ASN Update Bot Updated [Time, Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org