Overview:

In celebration of our 90th SBD Restoration Update, we thought our readers might enjoy seeing the extensive progress which Pioneer Aero has made in rebuilding the fuselage structure lying between Fuselage Frame #1 and Spar #1 in the Wing Center Section jig.

An illustration from page  39 of the SBD's Erection & Maintenance Manual showing the locations of each Fuselage Frame and its corresponding Station Number. As readers may recall, the Station Number is the distance (in inches) between any given structural member and the datum it is referenced against. For the fuselage, this datum is the forward face of Fuselage Frame #1—hence the reason why that subassembly is assigned Station #0. Note that the rudder also has station numbers assigned to it—these refer to the distance (in inches) between upper face of each horizontal rib relative to the aircraft's centerline.
An illustration from page 39 of the SBD's Erection & Maintenance Manual showing the locations of each Fuselage Frame and its corresponding Station Number. As readers may recall, the Station Number is the distance (in inches) between any given structural member and the datum it is referenced against. For the fuselage, this datum is the forward face of Fuselage Frame #1—hence the reason why that subassembly is assigned Station #0. Note that the rudder also has station numbers assigned to it—these refer to the distance (in inches) between upper face of each horizontal rib relative to the aircraft's centerline.

Fuselage Frame #1: Middle and Lower Sections

Fuselage Frame #1 is the forward-most structural bulkhead in the SBD's fuselage. As discussed in Restoration Update #74, this structure comprises three primary sections (lower, middle & upper) with the interior gap between them sealed by the fire wall. During the aircraft's original construction, the lower and middle sections were riveted together before being mounted in the Wing Center Section, since the aircraft's lower forward fuselage is integral to that major subassembly. They are reunited with their topmost element, however, only during final reassembly with the upper fuselage.

Pioneer's Craig Cunha refurbished/remanufactured most of the parts for Fuselage Frame #1's lower section earlier this year, but the newly-made middle section only recently arrived following heat treating. With its return, Cunha could continue rebuilding Fuselage Frame #1. Before he could begin, however, he first needed to straighten a minor twist in the middle section. Such warping is not unusual following the heat treating process—considering that the part is baked in an oven not far below its melting point, then rapidly cooled (quenched) to retain the superior mechanical properties its high-temperature crystalline state permits. Deformations are usually correctable without much difficulty, so long as the rework occurs reasonably soon after heat treating (i.e. before age hardening is complete).

With the middle section once again in its correct shape, Cunha trimmed the flange to its final dimensions then attached the part to the Frame's lower section. He then laid out the precise positions for the engine bearer attachment brackets on the frame, then marked, drilled and reamed the holes to the appropriate size.

Cunha then positioned the Fuselage Frame #1 subassembly on the SBD's Wing Center Section datum plate, with the engine bearer mounts and temporary bolts holding the it in place. He also added a new cross beam to the jig to hold the middle section (Fuselage Frame sides) in their correct locations.

The forward face of Fuselage Frame #1. Here, the refabricated lower section is being trial-fitted to the middle section. Care has been taken to achieve a smooth transition between the edges of these two sections. This will help ensure a smooth fuselage skin each side once fitted. The holes for the engine bearer bolts have been drawn at each end of the join line; note the red dots at their center. Note also the two primer painted pieces towards the bottom of the image; these are the two pockets (original to B-22) which cover a cutout in the fuselage frame to allow space for the inboard extremities of the wing leading edges on the opposite side of the frame. (image via Pioneer Aero Ltd.)
The forward face of Fuselage Frame #1. Here, the refabricated lower section is being trial-fitted to the middle section. Care has been taken to achieve a smooth transition between the edges of these two sections. This will help ensure a smooth fuselage skin each side once fitted. The holes for the engine bearer bolts have been drawn at each end of the join line; note the red dots at their center. Note also the two primer painted pieces towards the bottom of the image; these are the two pockets (original to B-22) which cover a cutout in the fuselage frame to allow space for the inboard extremities of the wing leading edges on the opposite side of the frame. (image via Pioneer Aero Ltd.)
The aft face of Fuselage Frame #1 is seen here being positioned on the datum plate for the SBD’s Wing Center Section jig for alignment checking. The holes for the engine bearer bolts had been drilled at this point, and the mounting brackets clecoed in position. The plumb bob (seen at the bottom of the photo) and its associated string indicate the location for the jig’s upper center line. There is also a string line for the lower center line; a laser line projected through the jig allows the center line drawn on the frame the be positioned precisely. (image via Pioneer Aero Ltd.)
The aft face of Fuselage Frame #1 is seen here being positioned on the datum plate for the SBD’s Wing Center Section jig for alignment checking. The holes for the engine bearer bolts had been drilled at this point, and the mounting brackets clecoed in position. The plumb bob (seen at the bottom of the photo) and its associated string indicate the location for the jig’s upper center line. There is also a string line for the lower center line; a laser line projected through the jig allows the center line drawn on the frame the be positioned precisely. (image via Pioneer Aero Ltd.)

Structure Between Fuselage Frame #1 & Spar #1:

With the lower sections of Fuselage Frame #1 positioned properly in the SBD's Wing Center Section jig, it was then possible to trial-fit and complete the internal structure linking this frame to Spar #1. This included the two ribs which comprise the Bomb Displacing Gear supports. Regular readers will remember that we covered the restoration of these components last October in Update #59—well, the time had arisen for Craig Cunha to locate them precisely against adjacent structure and drill them off. The bomb aiming window support bracket assembly (covered in Update #74) could then be positioned between these two ribs (and the support bracket on Spar #1), then drilled off.

The righthand Bomb Displacing Gear mounting bracket which attaches its rib to Fuselage Frame #1 is an original item from B-22, although its opposite on the lefthand side had to be refabricated. These two brackets were positioned and drilled off to their respective ribs and Fuselage Frame #1.

And finally, the SBD's righthand inboard leading edge assembly was temporally refitted to the Wing Center Section jig to confirm its clearance with Fuselage Frame #1. Some of the images below show just how tightly it squeezes into this section of the Dauntless!

The main ribs seen here linking Fuselage Frame #1 to Spar #1 serve as the Bomb Displacing Gear mounts. Fabricated many months ago, they are seen here during trial-fitting, being drilled off against adjacent structure. The bomb window support bracket assembly (also previously fabricated) which sits between the two bomb displacing gear ribs was also positioned and drilled off against the ribs and support bracket on Spar #1 at this time too. (image via Pioneer Aero Ltd.)
The main ribs seen here linking Fuselage Frame #1 to Spar #1 serve as the Bomb Displacing Gear mounts. Fabricated many months ago, they are seen here during trial-fitting, being drilled off against adjacent structure. The bomb window support bracket assembly (also previously fabricated) which sits between the two bomb displacing gear ribs was also positioned and drilled off against the ribs and support bracket on Spar #1 at this time too. (image via Pioneer Aero Ltd.)
This closeup shows the aft end of the bomb window support bracket assembly which sits between the two Bomb Displacing Gear ribs. With these ribs in position, it was possible to drill-off the final holes which hold this subassembly to Spar #1. (image via Pioneer Aero Ltd.)
This closeup shows the aft end of the bomb window support bracket assembly which sits between the two Bomb Displacing Gear ribs. With these ribs in position, it was possible to drill-off the final holes which hold this subassembly to Spar #1. (image via Pioneer Aero Ltd.)
Here we can see that the SBD’s inboard righthand wing leading edge has been temporarily fitted to the Wing Center Section. Pioneer performed this task to confirm its clearance with Fuselage Frame #1. (image via Pioneer Aero Ltd.)
Here we can see that the SBD’s inboard righthand wing leading edge has been temporarily fitted to the Wing Center Section. Pioneer performed this task to confirm its clearance with Fuselage Frame #1. (image via Pioneer Aero Ltd.)
A closeup of Fuselage Frame #1 showing why it needed a bulged pocket in the forward face (as discussed in Update #74) to accommodate the inboard extremity of the wing’s leading edge—in this case, the righthand leading example, which is seen here temporarily fitted to verify its fit. (image via Pioneer Aero Ltd.)
A closeup of Fuselage Frame #1 showing why it needed a bulged pocket in the forward face (as discussed in Update #74) to accommodate the inboard extremity of the wing’s leading edge—in this case, the righthand leading example, which is seen here temporarily fitted to verify its fit. (image via Pioneer Aero Ltd.)
A view of the lower forward fuselage with the Bomb Displacing Gear structure and the righthand wing leading edge trial fitted. The relationship between the two subassemblies is clearly revealed via this perspective. (image via Pioneer Aero Ltd.)
A view of the lower forward fuselage with the Bomb Displacing Gear structure and the righthand wing leading edge trial fitted. The relationship between the two subassemblies is clearly revealed via this perspective. (image via Pioneer Aero Ltd.)

Bomb Displacing Gear Support Ribs & Fuselage Frame #1:

After the parts described in the previous section were trial-fitted and drilled off against one another, it was time to disassemble them for primer painting the individual parts. Once the paint had cured, each of the separate subassemblies was riveted together, then clecoed back onto the Wing Center Section jig to await the eventual addition of other components for trial fitting and drilling off.

The lower and middle sections of Fuselage Frame #1 (forward face) after being clecoed together in preparation for riveting. Note the various small components which have also been clecoed in place, including the circular doublers (bare aluminum) for the engine mount attachment fittings. (image via Pioneer Aero Ltd.)
The lower and middle sections of Fuselage Frame #1 (forward face) after being clecoed together in preparation for riveting. Note the various small components which have also been clecoed in place, including the circular doublers (bare aluminum) for the engine mount attachment fittings. (image via Pioneer Aero Ltd.)
A reverse-side view of the structure pictured in the previous image. (image via Pioneer Aero Ltd.)
A reverse-side view of the structure pictured in the previous image. (image via Pioneer Aero Ltd.)
Another view of the Bomb Displacement Gear support ribs during trial-fitting. The stringers on either outside of the ribs help form a continuous, smooth contour between the forward end of the Bomb Fairing and Fuselage Frame #1. Note: the rectangular opening between the ribs is where the bomb aiming window is located. (image via Pioneer Aero Ltd.)
Another view of the Bomb Displacement Gear support ribs during trial-fitting. The stringers on either outside of the ribs help form a continuous, smooth contour between the forward end of the Bomb Fairing and Fuselage Frame #1. Note: the rectangular opening between the ribs is where the bomb aiming window is located. (image via Pioneer Aero Ltd.)