Hi,
The longitudinal stiffeners (longeron/stringers) used in the rear fuselage of the B-17 refer to a Boeing specified extrusion and no plan appears to be included for such items.
The 3 key profiles are these:
BAC 1515-504
BAC 1515-506
BAC 1515-507
1. Does anyone know what the -504, -506, -507 represents please? A change in profile or perhaps just a change in material spec?
2. Does anyone know where I can obtain the accurate dimensions for these profiles? I see aerospace suppliers still refer to BAC numbers but few list the ones above - probably a discontinued line.
Thanks!
The longitudinal stiffeners (longeron/stringers) used in the rear fuselage of the B-17 refer to a Boeing specified extrusion and no plan appears to be included for such items.
The 3 key profiles are these:
BAC 1515-504
BAC 1515-506
BAC 1515-507
1. Does anyone know what the -504, -506, -507 represents please? A change in profile or perhaps just a change in material spec?
2. Does anyone know where I can obtain the accurate dimensions for these profiles? I see aerospace suppliers still refer to BAC numbers but few list the ones above - probably a discontinued line.
Thanks!