Blank aircraft weight and balance revision form 2025

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All weight and balance data must be on board the airplane. Data must be entered accurately if software is used for calculating weight and balance. Aircraft are required to be under MTOW and MLW. An aircrafts center of gravity is required to be within the center of gravity limits at all times.
The Operating Limitations of the airplane must be on board. This includes, but is not limited to, placards and signs indicating limitations, gage indications (white arc, green arc on the Airspeed Indicator, etc.), and the Pilots Operating Handbook (aka the POH) or Flight Manual.
There are certain Federal Aviation Administration (FAA) regulations and requirements that must be kept in mind when operating an aircraft. These include: All weight and balance data must be on board the airplane. Data must be entered accurately if software is used for calculating weight and balance.
Remember that the weight and balance documentation is part of paperwork that must be on board at all times. It should show the empty weight, empty-weight CG, most forward and most rearward limits, and sample loadings.
It is vital to comply with weight and balance limits established for all aircraft. Operating above the maximum weight limitation compromises the structural integrity of the aircraft and can adversely affect performance. Stability and control are also affected by improper balance.
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Calculating Aircraft Weight and Balance Step 1: Find Your Aircrafts Empty Weight and Moment. Step 2: Find Weights of Everything Loaded. Step 3: Calculate the Moment for the Load. Step 4: Total Up the Weights and the Moments. Step 5: Determine If Center of Gravity Is Within Limits.
To determine the CG, divide the total moment by the total weight.

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