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Main Wing Spar – The Beginning

April 26, 2010 by Mike 2 Comments

The beginning of the main wing spar for this Stewart S-51 started out with a few 4 x 12 foot sheets of aluminum. After some time doing the layout the pieces were cut and bent as required. As I work for a major airline I was lucky enough to be able to take advantage of the sheet metal shop during some off time.

Main Spar Blanks – Initial Cutting

As the S-51 main wing spars are built up, meaning they are not machined from a big chunk of aluminum billet, all parts need to be made individually from sheet aluminum, then during final assembly they are riveted together into a “C” shape containing the Spar Caps and Spar Web.

Main Wing Spar - Layout and Cutting

 

Bending the Main Spar – Spar Caps

The main spar and spar caps on the S-51 are made from 2024-T3 aluminum that is 0.063 inch thick.

Main Spar - Spar Caps

Wing Stringers

All the wing stringers and spar caps started out as flat aluminum strips.  You can notice to the front of the picture that there is already one piece we have bent. This was a pretty time consuming process and took all evening.

 

IMG_2718 - resize

In the following picture you can see that all the stringers are bent.

IMG_2720 - resize

 

Please comment, I love to hear from my readers.  Thanks again for coming along for this ride, you make my work worthwhile.

 

Filed Under: Main Spar, Wings Tagged With: Main Spar, Wings

Comments

  1. DANIELE BELTRAME says

    April 15, 2020 at 06:25

    HI
    EVEN THE STRINGER AER MADE FROM .063″ ?

    Reply
    • Mike says

      April 30, 2020 at 16:14

      Hi Daniele,
      Thanks for your question. No the stringers are made from 0.040. The main spar web and spar caps is 0.063 and the rear spar web and caps are 0.050. All made from 2024-T3.

      Reply

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Profile Photo 1 Hello - My name is Mike and I'm a true believer that if you can imagine something, it's just a matter of bringing it into reality.

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