17,000 16,000 15,000 14,000 13,000 12,000 11,000 10,000 9,000 272  276 280  284  288  292  296  300  304 CG (inches aft of datum) Weight (lb) Maximum zero fuel weight Maximum takeoff weight 16,600 Maximum landing weight 16,000 Maximum zero fuel weight 14,000 Maximum takeoff weight Figure 9-46.  Weight and balance diagram. Determining the Changes in CG When  Passengers Are Shifted Using the loaded weight and CG of the Beech 1900, calculate  the change in CG when the passengers in rows 1 and 2 are  moved to rows 8 and 9.  [Figure 9-47]  Note that there is no  weight change, but the moment index has been increased by  1,155 pound-inches/100 to 44,294. The new CG is at fuselage  station 300.7.  [Figure 9-48] This type of problem is usually solved by using the following  two formulas. The total amount of weight shifted is 550  pounds (300 + 250) and both rows of passengers have moved  aft by 210 inches (410 – 200 and 440 – 230). The CG has  been shifted aft by 7.8 inches, and the new CG is at station  300.7.  [Figure 9-49] 9-16