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Engineering Design Approval/PMA

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  • Engineering Design Approval/PMA

    We have just received (last Friday) Engineering Design Approval to take serviceable tail brace wire nipples for BC-12D, F-19, F-21 and F-22 series airplanes and drill and re-thread to 10-32 as per MIL-S-8879, Class B thread.

    We also received PMA to manufacture new 3/16 stainless steel tail brace wires to fit the reworked nipples. The threads on the new wires are rolled, not cut.

    The cost of reworking all 8 nipples and the 4 new PMA'd wires (with check nuts) is $264.00 (US) plus postage and ins. We can also export to Canada and other countries and supply the FAA 8130-3 Authorized Release Form.

    If you are interested, give us a call at (907) 688-3715 or email your inquiry to [email protected]. We accept Visa and MasterCard (Do not email CC numbers direct. The site is not secure yet). Fax no. is (907) 688-5031.

    We don't have much else for the Taylorcraft right now but we can make parts as necessary under 21.303(b)(2), owner produced part. Check the FAR.

    You can also check out our website http://www.burlac.com

    Thank you for your time to read this.

    Burl A.Rogers
    Manager/Member
    Burl's Aircraft, LLC
    Last edited by AV8R2; 08-02-2005, 11:14.

  • #2
    Re: Engineering Design Approval/PMA

    Sorry I forgot to say in above post (now edited) but the threads are rolled, not cut, on the new wires.

    FYI:

    We use L.M. Fette rolling die heads. The finest in the world. We can also do 1/4-28 wires. (small float wires, etc.)

    All our wires can be made up to 120" in length.

    Burl

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