FAA Private Pilot Test Prep

Category - FAA Private Pilot

Refer to Figures 33 and 34 on pages 35 and 36.
What effect does a 35-gallon fuel burn (main tanks) have on the weight and balance if the airplane weighed 2,890 pounds and the MOM/100 was 2,452 at takeoff?
  1. 210 pounds less and the aircraft is still in limits
  2. 210 pounds more in weight and the aircraft is out of limits
  3. 210 pounds less and the aircraft is aft of the limits
  4. 210 pounds less and the aircraft is forward of limits
Explanation
Correct answer: C. 210 pounds less and the aircraft is aft of the limits. First calculate the burn of fuel- 35 gallons at 6 pounds per gallon = 210 pounds less. Now look at figure 33 under the fuel numbers: find 35 gallons which is 210 pounds which will change the CG by 158 according to the chart. Subtract the weight from the original weight 2890- 210= 2680. Then subtract the moment of 158 from the original moment of 2452 equals 2294. Now on figure 34 find the new weight of 2680. Look at the two moment numbers for that weight. The first number is the forward GC the second is aft CG. The aft CG for this weight is 2287, our number is now 2294, which mean we are now aft of the acceptable aft CG.
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