Aviation Crash Map

Corey CIRRUS VK-30 N7033G

3 June 1996 · Lapeer, Michigan, United States · Fatal

Summary

On 3 June 1996 at about 18:55 local time, a Corey CIRRUS VK-30 registered N7033G was involved in an accident near Lapeer, Michigan, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 18:55
Classification
Accident
Location
Lapeer, Michigan, United States
Coordinates
43.0390, -83.3195
Aircraft
Corey CIRRUS VK-30
Registration
N7033G
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Aircraft damage
Destroyed
Weather
VMC
Light
Not Reported
NTSB number
CHI96FA185

People

1 person died.

On board Died Serious Minor Uninjured
1 1 0 0 0

Probable cause

incomplete cure of the bonding material in the cruise flap, improper material in the cruise flap hinge, and improper welding of the cruise flap push rod end caps. Factors were delamination of the cruise flap, partial failure of the cruise flap hinge, and fatigue failure of the outboard cruise flap push rod.

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

Read the full NTSB narrative

According to witnesses, the accident pilot reported on Unicom that his 'flap bracket had broken.' A pilot who was on the ground near the accident site reported that he observed a 'violent flutter' on the right wing. Examination of the right flap revealed the inboard flap push rod was fractured at the end cap. The push rod welds exhibited 'porosity and secondary cracking indicative of poor welding techniques.' The inboard cruise flap push rod 'exhibited a thumbnail crack, which may have indicated failure by high stress, low cycle fatigue.' The outboard cruise flap hinge was fractured. Examination revealed the hinge was constructed entirely of composite material. The kit manufacturers drawings specify an aluminum core for the hinge. Differential scanning calorimetric analysis of the composite cruise flap skin revealed the vinyl ester matrix material was 'not fully cured.'

Quoted verbatim from the NTSB record.

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All 170,864 records in United States