6-6 Figure 6-10.  Sample moment limits versus weight envelope. 4,000 3,900 3,800 3,600 3,500 3,400 3,200 3,000 2,800 2,600 2,400 106  108  110  112  114  116  118 CG inches aft of datum Weight (lb) 3,900 4,600 4,50 0 4,400 4,30 0 4,200 4,100 4,000 3,800 3,700 3,600 3,500 3,400 3,100 3,300 3,20 0 3,000 2,900 2,800 2,700 2,600 Maximum zero fuel weight Moment/100 Envelope based on the following weight and CG limit data (landing gear down) Weight condition  FWD CG limit  Aft CG limit 3,900 pounds (max takeoff/landing)  110.6  117.5 3,250 pounds or less  106.6  Maximum takeoff and landing weight