I'm having trouble understanding the J-stringers for the aft fuselage. on DWG 18 they only show the end trimmed away (upper/inside flange cut-away) for the aft end of the 786B stringers. But it appears to me that to fit against the 706 bulhead the forward end of the B and C stringers will also have to be trimmed in a similar manner. Right now I can't get the tailcone assembly (711/712/779) onto the aft fuselage because the stringers are sticking too far out the back.
Also, it's not clear to me from Drawing 26 how the aft end of the 786C is supposed to fit (be trimmed) against the 712 bulkhead.
Help, anyone?
Also, it's not clear to me from Drawing 26 how the aft end of the 786C is supposed to fit (be trimmed) against the 712 bulkhead.
Help, anyone?