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An image of the Museum's Dauntless during its recovery in September 1994. Note the severely crushed wing leading edges. (image via A&T Recovery)

Center Section Wing Leading Edges:

Back in October 2023, the team at Pioneer Aero Ltd. began rebuilding the wing leading edges for the SBD's center section. As the image above reveals, this structure absorbed significant impact damage when the Dauntless ditched into Lake Michigan during January 1944. Consequently, very few of its components survived in restorable condition, so the restoration team has been working hard to manufacture replacements. They tackled the spar web assemblies first, then proceeded to the ribs and leading edge skins; components outlined in the A-24 illustrated parts manual image below.

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An illustration describing the various assemblies which form the leading edge structure under the skin in the wing center section for the SBD and A-24.

Leading Edge Ribs:

In January, Hadon Smith formed the base shapes for each of the left and righthand leading edge ribs. These components lie between Station 10 and Station 56 on either side of the wing; Station 10 being 10" from the aircraft's center line, with Station 56 being 56" from the same axis. The SBD's original ribs were too badly crushed to even serve as templates for their remanufacture, so the restoration team had to rely upon the Douglas Aircraft lofting drawings to determine the appropriate shapes to apply. Using these documents, Pioneer Aero's engineers created profiles for each rib out of  card stock, which they then used as a template for cutting out the necessary forming blocks for shaping replacement components. The images below reveal some of the steps in this process.

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A complete set of newly-formed ribs for the center section wing leading edge. This image shows the components prior to the installation of lightening holes and cutouts for the passage of stringers. (image via Pioneer Aero Ltd.)

Trial Fitting:

Once the ribs had received their lightening holes, Hadon Smith trial-fitted them against the newly-shaped leading edge skin to ensure they lined up properly. He then clecoed each rib to the leading edge spar and nestled this assembly into the leading edge skin again so he could precisely mark off and remove a cutout for the wheel well. The nose spar has since been painted with primer and mostly riveted together. Hadon also cut slots into each rib for the leading edge stringers. With the ribs now fully-formed, he then sent the parts off for heat treating to bring them up to the correct tensile strength and hardness.

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Trial-fitting the leading edge ribs in the righthand leading edge center section skin. For reference, the Station 10 rib (10” from the aircraft centerline) is at the top edge of the image. The ribs with curved cutouts towards the middle of the image are shaped this to make room for the wheel well. (image via Pioneer Aero Ltd.)
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The righthand leading edge spar web near the end of its rebuild. (image via Pioneer Aero Ltd.)