An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be

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(Refer to figure 61.) How should the 500-pound weight be shifted to balance the plank on the fulcrum?

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(Refer to figure 35.) What is the maximum amount of fuel that may be aboard the airplane on takeoff if loaded as follows?

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WEIGHT (LB.) MOM/1000
Empty weight 1,350 51.5
Pilot and front passenger 340 __
Rear passengers 310 __
Baggage 45 __
Oil, 8 qt __ __

 

(Refer to figure 35.) Calculate the moment of the airplane and determine which category is applicable.

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WEIGHT (LB.) MOM/1000
Empty weight 1,350 51.5
Pilot and front passenger 310 __
Rear passengers 96 __
Fuel, 38 gal __ __
Oil, 8 qt __ –0.2

 

(Refer to figures 33 and 34.) Upon landing, the front passenger (180 pounds) departs the airplane. A rear passenger (204 pounds) moves to the front passenger position. What effect does this have on the CG if the airplane weighed 2,690 pounds and the MOM/100 was 2,260 just prior to the passenger transfer?

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