Posted for "Christopher Zavatson" <Christopher.Zavatson@udlp.com>:

Rob,
My approach was a little different.  It avoids the release and bond
step.  1.  Attached 3 bid lay up to inner fuselage side walls extending
straight up just beyond height of original flanges.
2.  Cut off old flanges
3.  Shaped vertical side wall extensions so that stab rests in correct
orientation at rear of original saddle.
4.  Added mid-bulkhead
5.  Bid lay up on interior and exterior side wall to stab joint with
small micro fillets.
6.  Added micro to exterior fillet to get final shape.
7.  Added bid tape over completed exterior fillet
8.  Installed aft tilted bulkhead

Chris Zavatson
N91CZ
360 std