Aviation Crash Map

Piper PA-28-180 N3470R

12 April 2010 · Three Rivers, Michigan, United States · No injuries

Summary

On 12 April 2010 at about 00:30 local time, a Piper PA-28-180 registered N3470R was involved in an accident near Three Rivers, Michigan, 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 00:30
Classification
Accident
Location
Three Rivers, Michigan, United States
Nearest airport
Three Rivers Municipal (HAI)
Coordinates
41.9597, -85.5933
Aircraft
Piper PA-28-180
Registration
N3470R
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Instructional
Phase of flight
Not recorded
Route
Three Rivers → Three Rivers
Aircraft damage
Substantial
Weather
VMC
Light
Dusk
NTSB number
CEN10LA210

People

Nobody was injured.

On board Died Serious Minor Uninjured
2 0 0 0 2

Probable cause

The pilot's inability to maintain directional control during landing due to the failure of the left main landing gear torque link as a result of fatigue.

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

Read the full NTSB narrative

During a touch-and-go landing, the airplane veered to the left and the flight instructor attempted to correct to the right thinking the student applied the left brake. However, the airplane continued to veer to the left and the right wing struck the terrain. The airplane continued off the runway and came to rest in a field. Examination of the airplane revealed that the left aft spar was bent and fractured, the left main landing gear separated, and the main landing landing gear torque link was fractured. An NTSB Materials Laboratory examination of the torque link revealed the fracture face contained crack arrest marks typical of fatigue cracking that emanated from multiple origins at the surface of the wall on both sides of the link. The fatigue origin areas contained no evidence of gouge damage or corrosion damage. The fatigue cracks were the result of lateral stress produced during landing and taxi operations. Hardness testing of the material produced values greater than the minimum hardness value.

Quoted verbatim from the NTSB record.

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All 9,402 records for this type

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