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Thread: KF IV trailing edge fail

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  1. #1

    Join Date
    May 2010
    Location
    Melbourne Australia
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    10

    Default KF IV trailing edge fail

    I returned from a flight and found that the trailing edge on the starboard side haste failed. It has come from the rivet on the second rib from the fuselage and appears to have been from flexing over the years. Is this a common failure? What is the best way to race/repair this? Thanks in anticipation.

  2. #2
    Senior Member Dave S's Avatar
    Join Date
    Oct 2008
    Location
    St Paul, MN
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    1,836

    Default Re: KF IV trailing edge fail

    Rob,

    I believe in your profile it says you have a model IV?...Correct?

    Not at the rib which holds the flaperon bracket?....correct?

    If you have any photos you can post of the failed part and surrounding structure I think it would help list members who have some ideas. Sometimes it is difficult to get a good photo but they sure help if it is possible.

    Sincerely,

    Dave S

  3. #3

    Join Date
    Jan 2014
    Location
    Australia
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    93

    Default Re: KF IV trailing edge fail

    Hi Ausfox,

    I'm also keen to see any photos etc, I see you're also in my part of the world :-)

  4. #4

    Join Date
    May 2010
    Location
    Melbourne Australia
    Posts
    10

    Default Re: KF IV trailing edge fail

    Starboard wing, not involved with flaperon hanger. Started at the rivet where the trailing edge is riveted to the rib.


    I will get the photos on the site eventually

    Thanks



    Last edited by Ausfox; 08-05-2014 at 11:44 PM. Reason: Add text

  5. #5
    Senior Member HighWing's Avatar
    Join Date
    May 2009
    Location
    Goodyear, AZ
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    1,743

    Default Re: KF IV trailing edge fail

    I had this happen on my first Model IV. My fix was to drill three small diameter holes along the edge at the rib. I then drilled a hole in a stout piece of wood to accept an eye bolt. The wood and eyebolt were positioned between the adjacent ribs with appropriately dimensioned spacers, then safety wire was laced between the eyebolt and the holes on the trailing edge. Tightening the eyebolt pulled out the wrinkles. As the permanent fix, a thick epoxy mix was then injected into an the drilled holes to fill the space between the aft end of the rib and the inner surface of the trailing edge.

    This was not an uncommon occurrence apparently as the book was edited.to advise filling the space during wing construction to prevent possible collapse.
    Lowell Fitt
    Goodyear, AZ


    My You Tube Channel

  6. #6

    Join Date
    Jan 2014
    Location
    Australia
    Posts
    93

    Default Re: KF IV trailing edge fail

    hmm... Interesting and a little concerning, Just wondering how many hrs did your air frames have?

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