N765DC

Substantial
None

Diamond Aircraft Industries DA 20-C1S/N: C0165

Accident Details

Date
Sunday, March 9, 2008
NTSB Number
SEA08LA090
Location
Spanish Fork, UT
Event ID
20080317X00319
Coordinates
40.141387, -111.661109
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The fatigue failure of the nose wheel fork assembly attachment stud/bolt during takeoff initial climb, and the collapse of the nose gear during landing.

Aircraft Information

Registration
Make
DIAMOND AIRCRAFT INDUSTRIES
Serial Number
C0165
Engine Type
Reciprocating
Model / ICAO
DA 20-C1
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
DA20-C1

Registered Owner (Current)

Name
N765DC LLC
Address
242 N 400 E
City
PAYSON
State / Zip Code
UT 84651-1839
Country
United States

Analysis

On March 9, 2008, about 1620 mountain daylight time, a Diamond Aircraft Industries DA 20-C1, N765DC, was substantially damaged during landing following an in-flight separation of the nose wheel at the Spanish Fork Airport (U77), Spanish Fork, Utah. The private pilot and his passenger were not injured. The airplane was registered to and operated by Airgyro Aviation LLC of Spanish Fork under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the local personal flight that departed from U77 about five minutes prior to the time of the accident.

The pilot reported that during the initial climb after takeoff from runway 30 he heard a "loud bang" originating from the rear of the airplane and he decided to circle around the airport and land. During the landing roll, as the nose of the airplane settled, the nose wheel strut folded aft into the fuselage resulting in structural damage to the airframe.

Examination of the airplane revealed that the nose wheel fork assembly and tire had separated from the nose wheel strut during takeoff. The nose wheel fork assembly attachment stud/bolt was sent to the NTSB Office of Research and Engineering, Materials Laboratory Division for further examination.

The examination revealed that the fracture surface of the stud/bolt had an area of flat fracture bordered by smoothly curving crack-arrest markings consistent with fatigue cracking. The fatigue cracking appeared to have propagated through an estimated 60 percent of the cross section of the stud/bolt, with the remaining cross section fractured with overstress signatures. Substantial oxidation and/or corrosion of the fracture surface was observed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08LA090