SMN structural monitoring systems plc

2013 Fatal Eddy Current test fail legal update

  1. 21,281 Posts.
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    FWIW ..
    Such a sad story
    Is SMN’s CVM testing something that might have been applied to this area of a Dromader model plane if it had been approved earlier?
    And does anyone out there know please what FAA certificate had been granted pre 2016?

    cheers




    According to the late Ken Davey, the inventor of CVM technology - it was a fatal wing shear that set him on the path to inventing CVM tech;
    — The fatal plane crash in 1968 was caused because  metal fatigue cracks had not been identified.
    http://www.walpole.org.au/wp-content/uploads/2019/01/August-17-Walpole-Weekly-2.pdf
    Walpole Weekly August 17, 2016 :

    “… Ken told the Weekly that in December 1968 when he was a pilot for McRobertson Miller Airlines (MMA), Flight 1750, a Vickers Viscount, crashed on approach to the Port Hedland airport.
    On board were two pilots, two air hostesses and twenty-two passengers. None of the occupants survived the impact.
    Ken said that he had flown to Port Hedland as a passenger on that plane the day before.
    “I knew the crew that perished”, he said.


    Detailed investigation revealed that two fracture surfaces showed that metal fatigue had caused cracks to grow across the lower boom of the right wing's main spar.
    With so much of the lower boom affected the wing could no longer support the weight of the aircraft, the lower boom suddenly broke in two and the outer half of the right wing separated from the inner half.

    Ken said, “Over the following years I thought of ways of preventing such a terrible accident and developed an idea for a structural monitoring system and I was granted International Patents.”
    Ken explained that in association with Perth financier, Mr Paul Kristensen of Capital Technologies, he set up a company in 1995.
    “I developed the device to the stage of completing lab tests at the Aeronautical and Maritime Research
    Laboratories”, Ken explained.


    In order to raise further capital, the now ASX- listed company Structural Monitoring Systems (SMS) was formed.
    Ken explained that his invention took 21 years to develop to the stage of being accepted by major airlines and aircraft manufacturers.


    The invention has attracted world-wide interest in the aviation industry.
    Ken said that his CVM system was used in fatigue tests to certify the fuselage of the Airbus A380.
    The technology is now the first airborne crack detection system in the world achieving certification for use by the Federal Aviation Authority of the USA on passenger carrying aircraft…”an
    Last edited by sabine: 11/04/23
 
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