Stability calculation


All the calculations of stability were made with the help of by Mr Bernd Trahmer of D.A..


Limits C601
Front by steering -0.151
Front by nose wheel -0.154
Back by stability

Shift by wing fuselage combination

Shift by engines Min. stability





Back limit 0.149
Back by nose wheel 0.220
M.A.C. 9.9-40%

An UHCA was born