A photograph from back in August 2023 clearly illustrates the pyramidal structure which comprises the Rollover Frame. Referred to in the A-24's Illustrated Parts Manual as the Overturn Structure, this subassembly helps protect the aircrew should an SBD flip onto its back during landing or takeoff. Amongst many other details, Pioneer Aero has recently been working to restore this section of the airframe. (photo via Pioneer Aero Ltd.)
A photograph from back in August 2023 clearly illustrates the pyramidal structure which comprises the Rollover Frame. Referred to in the A-24's Illustrated Parts Manual as the Overturn Structure, this subassembly helps protect the aircrew should an SBD flip onto its back during landing or takeoff. Amongst many other details, Pioneer Aero has recently been working to restore this section of the airframe. (photo via Pioneer Aero Ltd.)

Overview:

In their work on the SBD's upper fuselage, Pioneer Aero's restoration team has made significant progress with the dive bomber's Rollover Frame. This significant subassembly sits between the two crew compartments and attaches to the upper sections of Fuselage Frames #4 and #5 (see illustration below). It is a sturdy, pyramidal structure designed to help protect the SBD's occupants should the aircraft flip over during landing or takeoff.

A depiction of the SBD's Rollover Frame from the aircraft's Illustrated Parts Manual. This structure attaches to upper Fuselage Frames #4 (front) and #5 (reverse), with its four struts bound together at a common node via four attachment forgings, described in the above text.
A depiction of the SBD's Rollover Frame from the aircraft's Illustrated Parts Manual. This structure attaches to upper Fuselage Frames #4 (front) and #5 (reverse), with its four struts bound together at a common node via four attachment forgings, described in the above text.

Rollover Forgings:

As the above illustration reveals, the four struts which provide strength to the Rollover Frame meet at a common node, cinched together with bolts through forged aluminum attachment fittings. All four of these fittings from our SBD's fuselage proved to be restorable, with only minor corrosion issues to remedy. Removing some of this corrosion, however, proved quite challenging!

The bolt holes in each fitting are all counterbored to provide a flat surface for the mounting bolts to press against. But it was at the base of these counterbores where minor corrosion pitting turned up in some instances. Shaving away a thin layer of aluminum would remove this pitting and still leave the part within design tolerances, but for the mounting bolt to function properly, it was critical for the resulting face to remain perfectly orthogonal (i.e. at 90º) to the original bolt hole. While seemingly simple to execute in theory, such a cut was best achieved by using a 'reverse spot facer'. These unusual tools have a shaft which rises up through the bolt hole from the opposite side of the face being machined to ensure that any cutting is precisely orthogonal to the bolt hole. After a short delay waiting for this specialized tool to arrive at their workshop, the team at Pioneer was able to complete the restoration of these critical fittings.

Trial-fitting the upper sections of Fuselage Frames #5 and #6 (aft faces) along with the aft extrusions for the rollover structure onto the fuselage jig. All of these components (barring the doublers) are original to B-22. Note that two of the forged fittings are attached at the top of the Rollover Frame. (image via Pioneer Aero Ltd.)
Trial-fitting the upper sections of Fuselage Frames #5 and #6 (aft faces) along with the aft extrusions for the rollover structure onto the fuselage jig. All of these components (barring the doublers) are original to B-22. Note that two of the forged fittings are attached at the top of the Rollover Frame. (image via Pioneer Aero Ltd.)

Rollover Ribs:

To help stiffen the Rollover Frame, a pair of horizontally-positioned ribs are link Fuselage Frame #4 to Fuselage Frame #5 on either side of the airframe. The original units from B-22 proved to be restorable, with the lefthand example only requiring minor corrosion mitigation. The righthand rib, however, had one area of deeper corrosion. Martin Hedley devised an approved repair technique, which required him to cut away the damaged section from the rib. He replaced the missing material with a custom-made insert riveted against a larger backing plate acting as a stiffener. The following images describe the repair process.

Trial Fitting the Ribs:

To ensure that the ribs which tie Fuselage Frame #4 to Fuselage Frame #5 do so properly, the parts were trial-fitted to these structures on the upper fuselage jig. This took place before all of the remanufactured pieces for Frame #4 were available, so the original, albeit corroded parts, were used as a temporary substitute.

The above images show several other upper fuselage ribs in the process of being trial fitted to the jig, so we thought our readers would enjoy seeing the following images describing that work with a little more detail. Great progress is clearly being made!