W&B · Chapter 6
W&B 6-6
Page 6-6
This reproduces published FAA reference text for study. It does not replace the current official FAA publication or regulation.
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 4,500 4,400 4,300 4,200 4,100 4,000 3,800 3,700 3,600 3,500 3,400 3,100 3,300 3,200 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 106.6 117.5 Maximum takeoff and landing weight Figure 6-10. Sample moment limits versus weight envelope.
Retrieved from ecfr.gov on July 18, 2026.