III.5
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 |
0.215
-0.0146 -0.0016 -0.05 |
| Back limit | 0.149 |
| Back by nose wheel | 0.220 |
| M.A.C. | 9.9-40% |