[FONT="]In order to resolve a type registration issue over a Pitts S1 Im trying to research how its possible to tell an S-1 fuselage is a C or a D variant and also to form some view of its likely origin. Ive read through all the fuselage forum posts and gained the impression that differentiation is a little hit or miss as fuselages may have been modified over time.[/FONT]
[FONT="]As a starting point Ive pulled together the following:[/FONT]
[FONT="]Are there any fundamental differences in construction of a C or a D? For example is the tubing of a different wall thickness or does one variant have more tubes than the other?[/FONT]
[FONT="]I think Im correct in thinking that the D is an S fuselage fitted with the flat bottom wings and chronologically came after the roundwing S which was developed after the C. Was the S fuselage simply a late type C or was it changed in any way specifically for the S? Is the D fuselage exactly the same as an S built to the Aviat plans?[/FONT]
[FONT="]The differences Ive identified between C and D type fuselages include:[/FONT]
[FONT="]Pitch trim. The D has adjustable pitch trim whereas the C does not although some may have been retrofitted. Thus all Ds have weldments for a trim system and trim cable housing.[/FONT]
[FONT="]Elevator hinges. The D uses strap type elevator hinges rather than piano type hinges of the C. Again some Cs may have been retrofitted.[/FONT]
[FONT="]Fuselage length. The D fuselage is 3 longer than the C fuselage although later Cs also had this lengthened fuselage.[/FONT]
[FONT="]Elevator idler bearing. Ds have an idler bearing midpoint in the rear fuselage whereas Cs dont have this.[/FONT]
[FONT="]Brace at top of cabanes. Not sure about this as to whether theres any difference?[/FONT]
[FONT="]Are there any other distinguishing features between D and C fuselages?[/FONT]
[FONT="]Is it possible to distinguish a factory built fuselage frame from a homebuilt frame i.e. by the quality of the welding?[/FONT]
[FONT="]Id be very grateful for any input, corrections to the above.
Thanks to all in advance
[/FONT]
[FONT="]As a starting point Ive pulled together the following:[/FONT]
[FONT="]Are there any fundamental differences in construction of a C or a D? For example is the tubing of a different wall thickness or does one variant have more tubes than the other?[/FONT]
[FONT="]I think Im correct in thinking that the D is an S fuselage fitted with the flat bottom wings and chronologically came after the roundwing S which was developed after the C. Was the S fuselage simply a late type C or was it changed in any way specifically for the S? Is the D fuselage exactly the same as an S built to the Aviat plans?[/FONT]
[FONT="]The differences Ive identified between C and D type fuselages include:[/FONT]
[FONT="]Pitch trim. The D has adjustable pitch trim whereas the C does not although some may have been retrofitted. Thus all Ds have weldments for a trim system and trim cable housing.[/FONT]
[FONT="]Elevator hinges. The D uses strap type elevator hinges rather than piano type hinges of the C. Again some Cs may have been retrofitted.[/FONT]
[FONT="]Fuselage length. The D fuselage is 3 longer than the C fuselage although later Cs also had this lengthened fuselage.[/FONT]
[FONT="]Elevator idler bearing. Ds have an idler bearing midpoint in the rear fuselage whereas Cs dont have this.[/FONT]
[FONT="]Brace at top of cabanes. Not sure about this as to whether theres any difference?[/FONT]
[FONT="]Are there any other distinguishing features between D and C fuselages?[/FONT]
[FONT="]Is it possible to distinguish a factory built fuselage frame from a homebuilt frame i.e. by the quality of the welding?[/FONT]
[FONT="]Id be very grateful for any input, corrections to the above.
Thanks to all in advance
[/FONT]