Aviation Crash Map

EVO13 LANCAIR EVOLUTION N3WB

15 February 2015 · San Carlos, California, United States · No injuries

Summary

On 15 February 2015 at about 19:45 local time, a EVO13 LANCAIR EVOLUTION registered N3WB, operated by WR Brody, LLC, was involved in an incident near San Carlos, California, United States. 3 people were on board and nobody was injured. The aircraft was slightly damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 19:45
Classification
Incident
Location
San Carlos, California, United States
Nearest airport
San Carlos (SQL)
Coordinates
37.5092, -122.2464
Aircraft
EVO13 LANCAIR EVOLUTION
Registration
N3WB
Category
Airplane
Year built
2013
Engines
1
Operator
WR Brody, LLC
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
San Diego → San Carlos
Aircraft damage
Minor
Weather
VMC
Light
Day
NTSB number
WPR15IA105

People

Nobody was injured.

On board Died Serious Minor Uninjured
3 0 0 0 3

Probable cause

The collapse of the nose landing gear (NLG) due to the separation of the right trunnion pin from the NLG strut as a result of reverse-bending fatigue.

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

Read the full NTSB narrative

The pilot reported that, during the landing roll, the nose landing gear (NLG) began to shimmy, which quickly became severe. The pilot applied back pressure on the control stick to reduce the weight on the NLG; however, the NLG collapsed about 2 to 3 seconds later. The airplane then skidded on the runway for about 1,000 ft before coming to a stop upright. A postincident examination of the NLG revealed that the right trunnion pin had separated at the base of the pin where it connected to the NLG strut arm. The fracture surface had unified crack fronts, consistent with fatigue crack progression. The fatigue cracks initiated from multiple origins on opposite sides of the trunnion pin, consistent with reverse-bending fatigue. Although the reverse bending could have resulted from the exceedance of the lateral limits of the tow bar parameters during ground towing operations, it could not be determined if such an exceedance occurred before the incident. The event that precipitated the reverse bending could not be determined.

Quoted verbatim from the NTSB record.

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