Aviation Crash Map

Albright Stan KITFOX SUPER SPORT N960WM

18 October 2012 · Twin Bridges, Montana, United States · No injuries

Summary

On 18 October 2012 at about 20:40 local time, a Albright Stan KITFOX SUPER SPORT registered N960WM, operated by Charles W d'Autremont, was involved in an accident near Twin Bridges, Montana, United States. One person was on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 20:40
Classification
Accident
Location
Twin Bridges, Montana, United States
Nearest airport
Twin Bridges (K7S1)
Coordinates
45.5336, -112.3025
Aircraft
Albright Stan KITFOX SUPER SPORT
Registration
N960WM
Category
Airplane
Engines
1
Operator
Charles W d'Autremont
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Twin Bridges → Twin Bridges
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
WPR13CA018

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

The airplane builder’s failure to rig the flight controls correctly, which resulted in a loss of control after takeoff.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot attempted to perform a full-flap soft-field takeoff in the experimental light sport airplane. The pilot had flown about 16 hours in the accident airplane in the 4 months since he purchased it from the airplane builder; however, this was his first attempt at full-flap soft-field takeoff in this airplane. As the airplane left the ground, it rolled abruptly to the right. The right wing tip struck the ground, and the airplane cartwheeled, coming to rest pointing in the opposite direction of intended travel. The right wing and fuselage were substantially damaged. Postaccident examination revealed that the airplane's flaperons were misrigged and that the resultant difference in flaperon deflection was more extreme in the full flap position. In the full flap position with a full left control deflection input, the right flaperon moved 3 degrees more and the left flaperon 3 degrees less than they would have if properly rigged. The asymmetric nature of the flaperon deflections induced an adverse yaw to the right despite the pilot's corrective control inputs. Examination of the airplane maintenance logbook revealed that the airplane builder performed the most recent annual airworthiness inspection 4 1/2 months before the accident.

Quoted verbatim from the NTSB record.

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