N7810T

Substantial
None

CESSNA 172AS/N: 47410

Accident Details

Date
Saturday, October 3, 2009
NTSB Number
WPR10LA004
Location
Payson, AZ
Event ID
20091003X74020
Coordinates
34.256668, -111.339164
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The stress corrosion cracking of the nose gear landing fork, which resulted in the fork's failure during landing.

Aircraft Information

Registration
N7810T
Make
CESSNA
Serial Number
47410
Engine Type
Reciprocating
Year Built
1960
Model / ICAO
172AC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ADAMSON DON R
Address
1423 LINGO RD
Status
Deregistered
City
LONOKE
State / Zip Code
AR 72086-8485
Country
United States

Analysis

On October 3, 2009, at 0900 mountain standard time, a Cessna 172A, N7810T, was landing at Payson Airport, Payson, Arizona, when the nose landing gear fork separated during landing and the pilot lost control of the airplane. The student pilot was operating the airplane under the provisions of 14 Code of Federal Regulations Part 91. The student pilot, who was also the registered owner of the airplane, was not injured. The airplane was substantially damaged. Visual meteorological conditions prevailed and no flight plan was filed. The flight departed from Payson Airport about 0800.

According to the student pilot, he was conducting his second or third landing. As the airplane touched down, the nose gear separated, the airplane veered to the left, and then impacted the runway. The right wing sustained substantial damage. The student pilot indicated that the previous owner of the airplane had landed on unimproved terrain quite frequently.

The nose landing gear fork was submitted to the National Transportation Safety Board Materials Laboratory for further examination. According to the metallurgist, the part was manufactured using 2014 series aluminum, and the fracture surface had two distinct regions. One portion of the fracture was a relatively flat area with evidence of corrosion, and the remainder of the fracture consisted of slanted irregular surfaces with a shiny crystalline appearance. The metallurgist indicated that the appearance of corrosion was consistent with slow crack growth over time. Scanning electron microscope examination of the corrosion crack revealed no fracture features consistent with fatigue. Further examination revealed that the propagation of the crack appeared to be intergranular with cracks branching into adjacent grains. Although no single origin was positively identified, the metallurgist indicated that the crack appeared to have originated from a point on the surface of the bolt hole bore and propagated upwards and outwards. It was not possible to determine if the crack would have been visible to the unaided eye during a routine inspection.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR10LA004