Aviation Crash Map

Wight CARBON CUB CCK-1865 N625EX

13 August 2016 · Wasilla, Alaska, United States · No injuries

Summary

On 13 August 2016 at about 02:00 local time, a Wight CARBON CUB CCK-1865 registered N625EX was involved in an accident near Wasilla, Alaska, 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 02:00
Classification
Accident
Location
Wasilla, Alaska, United States
Nearest airport
Todds Strip Airport (5AK5)
Coordinates
61.5006, -149.6725
Aircraft
Wight CARBON CUB CCK-1865
Registration
N625EX
Category
Airplane
Year built
2016
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Summit → Wasilla
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
ANC16LA059

People

Nobody was injured.

On board Died Serious Minor Uninjured
2 0 0 0 2

Probable cause

The failure of the tailwheel suspension assembly during landing due to preexisting fatigue fractures in the suspension system, which resulted in a loss of directional control.

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

Read the full NTSB narrative

The airline transport pilot was conducting a personal cross-country flight in the experimental amateur-built, tailwheel-equipped airplane. The pilot reported that, while landing on a turf and gravel airstrip, the airplane veered sharply left as the tailwheel touched down. Despite applying full right rudder and brake controls, the pilot was unable to correct the airplane's track, and the right wing and horizontal stabilizer impacted the ground. The pilot stated that, after the airplane stopped, he was unable to straighten the tailwheel with the rudder control inputs because the tailwheel was bent. Postaccident metallurgical examination of the tailwheel suspension system revealed fractures within the welds of the assembly and a fatigue fracture at the bolt hole for mounting the tailwheel. The crack fracture surfaces exhibited orange and dark red corrosion, suggesting that the cracks were preexisting, and the fracture surfaces were consistent with overstress. The assembly also exhibited general twisting deformation, primarily as the result of deformation in the pivot bracket.

Quoted verbatim from the NTSB record.

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