Overview:

While the team at Pioneer Aero has been making great strides with the SBD's larger structural components, they have also focused on some of the myrad smaller components which fit into the fuselage. This update highlights some of these accomplishments, which we hope you enjoy learning about.

Forward Upper Fuselage Progress:

In addition to the stringers, Pioneer’s team has worked on fitting the lefthand upper longeron to the fuselage frames and skins. To begin this process, they trial-fitted the replacement lefthand upper engine mount to the corresponding longeron. As with the righthand longeron, this involved adjusting the angles for the inner and outer folds, then trimming and locating it in the correct spot before drilling. The longeron is now drilled-off against Fuselage Frames #1, #3, #4, #5 and #6. The replacement for Fuselage Frame #2 has also been fitted, and progress has been made fitting and drilling each of the parts which comprise the gun mount structure and instrument panel sides. Some of these parts came from a donor airframe, while the rest are replacements. The replacement lefthand forward skin section has also been drilled-off against the matching frames and stringers.

The replacement lefthand forward skin temporarily mounted in place; it has been drilled to match the fuselage frames and stringers. This is the first of the new fuselage skins to be trial-fitted to the structure. (image via Pioneer Aero Ltd.)
The replacement lefthand forward skin temporarily mounted in place; it has been drilled to match the fuselage frames and stringers. This is the first of the new fuselage skins to be trial-fitted to the structure. (image via Pioneer Aero Ltd.)

Fuselage Frame #1 (Lower Section):

Fuselage Frame #1 comprises three primary sections (upper, middle and lower) with the bottom two being integrated within the SBD's Wing Center Section (see illustration below). The aircraft's firewall mounts within the central ring formed by these three subassemblies.

A drawing showing the forward view of Fuselage Frame #1. The frame comprises three primary sections: upper, middle and lower. The aircraft's firewall sits in the central space between these subassemblies. (image from Page 16 of the A-24 Illustrated Parts Manual)
A drawing showing the forward view of Fuselage Frame #1. The frame comprises three primary sections: upper, middle and lower. The aircraft's firewall sits in the central space between these subassemblies. (image from Page 16 of the A-24 Illustrated Parts Manual)

The lower section of our SBD's original Fuselage Frame #1 was too badly buckled and corroded to be of much use, even as a pattern, however an example from a donor airframe was available to the project. As the image below reveals, even this component was beyond economic repair for airworthy use, however, it did provide several reusable parts.

This image shows the aft face of Fuselage Frame #1 (lower section) from a donor aircraft. While it is damaged, some components are restorable to airworthy condition. (image via Pioneer Aero Ltd.)
This image shows the aft face of Fuselage Frame #1 (lower section) from a donor aircraft. While it is damaged, some components are restorable to airworthy condition. (image via Pioneer Aero Ltd.)

The restoration team refabricated the frame section. After it returned from heat treating, they inked reference lines onto the aft face before positioning angle stiffeners in the appropriate spots and drilling them off. Two of these stiffeners are restored donor components, while three others are replacement parts remade on site.

A view showing the aft face of the newly-fabricated, lower section of Fuselage Frame #1 with a series of reference lines inked on its surface. The restoration team used the original factory drawing also in view to place these lines, which indicate the appropriate locations for various components and holes. (image via Pioneer Aero Ltd.)
A view showing the aft face of the newly-fabricated, lower section of Fuselage Frame #1 with a series of reference lines inked on its surface. The restoration team used the original factory drawing also in view to place these lines, which indicate the appropriate locations for various components and holes. (image via Pioneer Aero Ltd.)

The center section leading edge pocket cutouts were also marked out and cut into the frame; the pockets themselves (refurbished originals from the donor airframe) were then positioned and drilled off. Holes for two sets of system control connections were also marked out and cut into the frame. The team also fabricated and drilled off the bomb aiming window support bracket and its associated hinge. The cowling attach brackets were also fabricated, located and drilled off. The upper edge and holes for the lower engine mounts were then marked out and trimmed to their final size and shape.

The aft face of the lower and middle sections of Fuselage Frame #1 showing most of the associated components (new and original) after they have been drilled off and trial-fitted. (image via Pioneer Aero Ltd.)
The aft face of the lower and middle sections of Fuselage Frame #1 showing most of the associated components (new and original) after they have been drilled off and trial-fitted. (image via Pioneer Aero Ltd.)
A drawing showing the aft view of Fuselage Frame #1, as described in an earlier image. The components protruding from the lower section form the mounting structure for the bomb displacing gear described in a previous article. A window for the pilot to aim the bomb sits in between these longitudinal structural members, with the part labeled #14 holding its rear edge. This assembly, part #2064249, has been refabricated, as described in the following section. (image from Page 18 of the A-24 Illustrated Parts Manual)
A drawing showing the aft view of Fuselage Frame #1, as described in an earlier image. The components protruding from the lower section form the mounting structure for the bomb displacing gear described in a previous article. A window for the pilot to aim the bomb sits in between these longitudinal structural members, with the part labeled #14 holding its rear edge. This assembly, part #2064249, has been refabricated, as described in the following section. (image from Page 18 of the A-24 Illustrated Parts Manual)

Related to the lower section of Fuselage Frame #1, the restoration team has also worked on elements of the structure attaching to its aft face. The drawing above depicts this structure, part of which serves as the mount for the Bomb Displacing Gear we described in a previous article. The mounting structure for this equipment also includes a support assembly for the bomb-aiming window beneath the pilot’s feet. While the original component (part #14 in the drawing above) was too badly damaged to refurbish for airworthy use, Pioneer’s Craig Cunha fashioned a replacement from new metal, as shown in the images below. This component sits aft of the bomb window, supporting its rear edge.

A nice image of the replacement bomb aiming window support assembly. For reference, the edge nearest the camera faces forward in the aircraft. (image via Pioneer Aero Ltd.)
A nice image of the replacement bomb aiming window support assembly. For reference, the edge nearest the camera faces forward in the aircraft. (image via Pioneer Aero Ltd.)

Pilot's Armor Plate:

The SBD has several areas with armored protection, the most important of these being mounted behind the pilot’s seat against the rollover structure (see illustration below). The plate comprises several sections, with the lower element recently receiving treatment from Pioneer Aero’s William Lowen. The original component salvaged from our Dauntless had a heavy layer of corrosion, with significant pitting. Even so, it was still salvageable for use in the aircraft, given that it is not part of the load-bearing structure, nor will it be required - we hope - to withstand enemy bullets!

The SBD has several areas protected by steel armor plates. This particular assembly mounts against the rollover structure behind the pilot's seat. The lower section shown in this illustration is what Pioneer Aero's team recently refurbished for the project. (image via A-24 Illustratd Parts Manual)
The SBD has several areas protected by steel armor plates. This particular assembly mounts against the rollover structure behind the pilot's seat. The lower section shown in this illustration is what Pioneer Aero's team recently refurbished for the project. (image via A-24 Illustratd Parts Manual)

William Lowen removed the bulk of the rust using a composite stripping disc, and then bead-blasted the plate to clean out the pitting. It was then etch-primed and hi-build primed (a spray-on coating which helps fill in the corrosion pitting). Once this is dry and hard, Lowen will sand it back then add further layers of hi-build until the required surface finish is achieved.

The armor plate (forward face) hanging in the paint boot part way through the process of removing the rust mechanically with an abrasive disk. The corrosion pitting is very evident, but since the component is not structural, nor required to fulfill its original job (stopping bullets from hitting the pilot) it is sufficiently intact to be worth refurbishing cosmetically for reuse in the SBD. (image via Pioneer Aero Ltd.)
The armor plate (forward face) hanging in the paint boot part way through the process of removing the rust mechanically with an abrasive disk. The corrosion pitting is very evident, but since the component is not structural, nor required to fulfill its original job (stopping bullets from hitting the pilot) it is sufficiently intact to be worth refurbishing cosmetically for reuse in the SBD. (image via Pioneer Aero Ltd.)
A closeup of the forward side of the armor plate showing the words “SOFT FACE”. The armor plate was only hardened on one face, the side protecting the pilot from incoming bullets. Theoretically, the was to meant to prevent the armor plate from shattering and sending fragments into the pilot when the hard face (on the opposite side) was struck by high-energy projectiles. (image via Pioneer Aero Ltd.)
A closeup of the forward side of the armor plate showing the words “SOFT FACE”. The armor plate was only hardened on one face, the side protecting the pilot from incoming bullets. Theoretically, the was to meant to prevent the armor plate from shattering and sending fragments into the pilot when the hard face (on the opposite side) was struck by high-energy projectiles. (image via Pioneer Aero Ltd.)
Another view of the aft face of the armor plate during the cosmetic restoration process. As is evident, some of the localized pitting is very deep. (image via Pioneer Aero Ltd.)
Another view of the aft face of the armor plate during the cosmetic restoration process. As is evident, some of the localized pitting is very deep. (image via Pioneer Aero Ltd.)
Another view of the front face of the armor plate during the cosmetic restoration process. Note the pitting. (image via Pioneer Aero Ltd.)
Another view of the front face of the armor plate during the cosmetic restoration process. Note the pitting. (image via Pioneer Aero Ltd.)