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At present, airlines use \u201cassumed mass\u201d \u2013 estimating the total weight of the passengers by using set figures. Typically each passenger is assumed to weigh 88kg. Airlines may use gender to refine this figure, allowing 93kg for men and 75kg for women.
Standard empty weight (GAMA)\u2014aircraft weight that consists of the airframe, engines, and all items of operating equipment that have fixed locations and are permanently installed in the aircraft, including fixed ballast, hydraulic fluid, unusable fuel, and full engine oil.
Maximum Takeoff and Landing Weights According the Cessna generic flight manual for the C-172S, normal category maximum takeoff and landing weight for a C-172S is 2,550 pounds.
At this speed, the airplane will stall before it pulls more than +3.8 g's. This is an important speed to know.
2:39 7:29 Cessna 172 - Weight and Balance Calculation - YouTube YouTube Start of suggested clip End of suggested clip And then subtract out the usable fuel you want to know where the datum is that's the reference.MoreAnd then subtract out the usable fuel you want to know where the datum is that's the reference. Point where you measure all the arms to the waypoints of the aircraft.
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CG limits\u2014the specified forward and aft points within which the CG must be located during flight. These limits are indicated on pertinent aircraft specifications. CG range\u2014the distance between the forward and aft CG limits indicated on pertinent aircraft specifications.
2:35 15:17 Calculating Weight and Balance - MzeroA Flight Training - YouTube YouTube Start of suggested clip End of suggested clip Wait times arm equals. Moment you will use this formula time and time again you'll use it in theMoreWait times arm equals. Moment you will use this formula time and time again you'll use it in the inverse.
Center of gravity (CG) is calculated as follows: Determine the weights and arms of all mass within the aircraft. Multiply weights by arms for all mass to calculate moments. Add the moments of all mass together. Divide the total moment by the total mass of the aircraft to give an overall arm.
Typically, an operator calculates takeoff weight by adding the operational empty weight (OEW) of the aircraft, the weight of the passenger, cargo payload, and the weight of fuel. The objective is to calculate the takeoff weight and CG of an aircraft as accurately as possible.
Basic Empty Weight: 1,680 lb. Useful Load: 878 lb. Full Fuel Payload: 560 lb.

c172 weight and balance sheet