N324WS

Substantial
None

ZENITH STOL CH701S/N: 8836

Accident Details

Date
Sunday, May 31, 2020
NTSB Number
ANC20LA053
Location
Ambler, AK
Event ID
20200601X54009
Coordinates
67.039443, -158.829430
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot’s improper decision to take off from unsuitable terrain, which resulted in impact with uneven terrain, the subsequent failure of the nosewheel fork, and a nose over.

Aircraft Information

Registration
Make
ZENITH
Serial Number
8836
Engine Type
Reciprocating
Year Built
2014
Model / ICAO
STOL CH701
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
CH-701

Registered Owner (Current)

Name
SHRADER DAVID W
Address
PO BOX 1295
City
KOTZEBUE
State / Zip Code
AK 99752-1295
Country
United States

Analysis

On May 31, 2020, about 1233 Alaska daylight time, an experimental amateur-built STOL CH-701 airplane, N324WS, was substantially damaged when it was involved in an accident at the Kobuk Sand Dunes near Ambler, Alaska. The sport pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot, who was also the owner and builder of the experimental amateur-built airplane, stated that he landed the airplane on sand dunes and then shut down for 45 minutes. He then took off, and the airplane hit “some bumps, but nothing significant,” until immediately before it reached the rotation speed of about 45 mph, at which point, the airplane hit a larger bump, which propelled it upward. The airplane then impacted terrain in a “nose high” attitude, followed immediately by the nose landing gear collapsing. Subsequently, the airplane nosed over and then came to rest inverted. The pilot reported that the accident might have been prevented if he had conducted a more “detailed inspection” of the takeoff area and “preflight inspection” of the nosewheel fork.

Examination of the airplane revealed that the rudder and both wing struts sustained substantial damage. The part number 7L2-4J aluminum nosewheel fork had separated from the nose strut in three fragments at two fracture locations, one on each side of the strut attachment, at or near the four attachment bolt holes. The detailed examination revealed that the outer surfaces adjacent to the fractures exhibited outward lip-like deformation and the areas near the fractures on the inside (concave) of the fork exhibited secondary cracking perpendicular to the fractures. One of the fracture’s surface exhibited a dimpled rupture and dull and rough features. All the fracture features were consistent with overstress fracture in upward bending of the nosewheel fork. No evidence of preexisting cracks, wear marks, or corrosion was found. The chemical, electrical, and hardness characteristics of the middle fork fragment were consistent with an AA 6061 aluminum alloy in a T6 temper.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC20LA053