Aviation Crash Map

W10 TAILWIND N456TW

31 May 2023 · Penrose, Colorado, United States · No injuries

Summary

On 31 May 2023 at about 15:30 local time, a W10 TAILWIND registered N456TW was involved in an accident near Penrose, Colorado, United States. 2 people were 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 15:30
Classification
Accident
Location
Penrose, Colorado, United States
Nearest airport
Fremont County (1V6)
Coordinates
38.4316, -105.1127
Aircraft
W10 TAILWIND
Registration
N456TW
Category
Airplane
Year built
2007
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN23LA211

People

Nobody was injured.

On board Died Serious Minor Uninjured
2 0 0 0 2

Probable cause

The failure of the right rudder pedal stop due to an inadequate weld, which resulted in a loss of control on the ground.

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

Read the full NTSB narrative

The pilot, who was in the right seat, stated the left-seat pilot had just completed three uneventful full-stop landings, and then he took over the controls and was flying from the right seat. During the takeoff roll, he applied equal pressure to both rudder pedals. Suddenly, the right pedal broke forward, and the airplane veered off the left side of the runway. The left-seat pilot was unable to assist in controlling the airplane before it struck a berm. The airplane came to rest upright with the main landing gear collapsed, which resulted in substantial damage to the right side of the fuselage and engine mounts. Postaccident examination revealed that the right seat’s right rudder pedal stop, a U-shaped metal rod welded to the rudder pedal torque tube, broke at the weld, and the right pedal was beyond the normal forward limit. The weld appeared to have inadequate penetration into the base material, which resulted in a failure of the weld that allowed the rudder pedal to extend beyond the normal forward limit.

Quoted verbatim from the NTSB record.

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