Center Flap Progress:
Jayden Malloy is making solid progress rebuilding the SBD’s central wing flap, an effort which began back in February of this year. While he had to refabricate numerous new ribs for this key component, Molloy was able to save all of the doublers. The latter components rivet to each rib, adding strength over the spar cut outs. To ensure that each rib (with its doubler) matched up properly with the original spar, Jayden had to remanufacture the right angle attaching brackets. While these brackets may seem simple to construct, the addition of a joggle allowing the part to overlap the rib doubler made the process more complicated.
Stiffener Extrusions:
Jayden also cut, formed and installed new stiffeners. A series of these modified extrusions straddle the flap’s entire length adding strength to the structure. Thankfully, he was able to also refurbish a couple of original examples from the donor flap. These new components also required joggling at each end (in most cases) in order to overlap other components mounted to the flap’s perforated skin properly. As with the rib angles, this effort required the use of a specialized press die tool
Perforations:
As noted previously, the SBD’s set of dive flaps is one of the type’s most distinctive features, with its numerous perforations being a prominent detail. After restoring or remanufacturing numerous parts for the dive bomber’s center flap, Jayden Malloy began cutting and shaping each of these perforations. This flap spans the entire 11’ width of the SBD’s wing center section, so Molloy had to repeat this process many times over - 81 in total!
Cutting & Flanging:
Molloy used a fly cutter to make sure each hole was placed at the correct location and with the appropriate diameter. A fly cutter is a tool which fits on a drill press. There is a drill bit at its center, to position the hole precisely, while a cutting blade is set on an arm at a specific radius extending from the center to set the hole size. Jayden used this technique to cut out half of the holes in a checkered pattern across the flap skin. He then de-burred the hole edges, followed by a light sanding, to prevent any crack propagation during the flanging process. By cutting a set of holes in a checkerboard pattern to begin with, Molloy ensured that the skin retained sufficient structural integrity when flanges were pressed into each of them (i.e. the aluminum would not pull away from adjacent holes, distorting the sheet). After forming flanges for each of the first set of holes, Molloy then cut and flanged each of the remaining holes to form the complete set.
Forming the Flap Trailing Edge:
The flap’s trailing edge has to be folded up. Because the aft two radii are close together, it was impossible to use a traditional sheet metal brake to place the second fold at the correct angle. As a result, Jayden had to manually adjust the flange with special pliers to ensure that both folds were placed at the correct angle relative to one another. This will ensure that when it is installed it will not buckle the skin, warping the flap.